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Aircraft Mechanic's Specifications Handbook
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Copyright © 1975 by Pittsburgh Institute of Aeronautics, Pittsburgh, Pennsylvania. All rights reserved. This book, or parts thereof, may not be reproduced in any form without permi$5ion of the publi5her5,
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TABLE OF CONTENTS SectIon One Aircraft Hardware Title Page No. ATA - Chapter/Section Numbering i-xv Quick Identification AN 1-19 NAS 20 -46 MS 47 - 79 AN Hardware Specifications 80 -126 Reference Tables and Conversion Factors Tables Twist Drills, Letter and Wire Gauge Sizes 128 American Standard (Tap, Pipe Threads) Dimensions in Inches
128
American Standard Screws (Coarse) Dimensions in Inches
129
American Standard Screws (Fine) Dimensions in Inches
130
Clearance
130
Drills for Machines Screws
"a"
Rings Specification
Numbers and Description
131 -133
Metric and Decimal Equivalents of Fractions (of one inch)
134 -136
Temperature Conversion Centrigrade and Fahrenheit Example Conversion
137 -144 144
Conversion Factors
145 -164
Torque Values for Nut-Bolt Combinations
165 -167
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Section Two Fastener Identification Title
Page
No.
Fastener Specifications
1
Maximum
1
Speeds (Hand-Fed Operations)
Blueprint Fastener Callouts Alphabetical Conventional
3
Code Listing
4 -5
Rivets
6 -10
Blind Rivets
11 -16
Bi-Metal Rivets
17
Lockbolts
18 -21
Hi-Lok Bolts
22 - 25
Blind Bolts
26 - 27
Taper-Lok Bolts
28 - 29
Rivet Oversize Chart
30 - 33
Tips for Good Quality Holes
34
Common
35
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Section Three Electrical Connector Identification
Title
Page
Contacts for Front Release Connectors"""""."""""
1
FZ & FY Electrical Connectors"""""""""."""""""""
2- 3
DCOOthrough DC08 Electrical Connectors""".""""
4-5
DC20 through DC28 Electrical Connectors.".""""".
6-7
48 Series Bayonet Type Electrical Connectors"""""
8-9
Deutsch Electrical Connectors"." .."
9 - 10
No.
Deutsch Fuel Boost Pump Connector"""."""""""".10 CAOOKEthrough CA3106KEElectrical Connectors"""."."."""""""""""""""""""""""""""""""""
11 - 12
Contacts for Rear Release Connectors""""""""."".13
- 14
DC30 through DC37 Electrical Connectors""""""".14
- 15
DC50 through DC57 Electrical Connectors""""""""",,15
- 16
DC60 through DC63 Electrical Connectors.""""".".".17 - 18 MIL-C-38999Electrical Connectors"""""""""""""".""."
19 - 20
Contacts for Rack & Panel (Rectangular) Connectors"".""""",,,,,,,,,,,,,.,,,,,,,,,,.,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,, 21 - 28
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Section One : Aircraft Hardware
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ATA-CHAPTERI SECTION NUMBERING 05 TIME LIMITS/MAINTENANCE CHECK 00 General 1 Time Limits 2 Operational Specifications 3 Mechanic Flight Approval 01 Line/Check 1 Post Flig ht 2 Through Flight 3 Line Check (Thru-Flight) 4 Line Check (Over-Night) 12
03 Engine/Systems Check 1 Engine Operation Check 2 Power Profile Check 3 Engine Powered Systems Check 04 Avionics/Electrical Check 1 Avionics/Electrical 2 Avionics 3 Electrical 05
06 Area/System Scheduled Checks hru (as for example 05-06-XX thru 05-83-XX 83 or 0506 thru 0583) NOTE (The second increment 06 thru 83 is as per the ATA chapter designation, the third increment, if used, is as per subchapter & sub-subchapter designations). '34
85 86 87 38 89
90 91 A Check 92 93 94 95 96
Intermediate/Midperiod/ Service Operational Chk
B Check C Check D Check E Check Phase Overhaul
97 98
99 Unscheduled Maintenance Checks (Should further coding be necessary,
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utilize a third increment and the designations as defined in Chapter 5 of the applicable AlC Maintenance Manual). 06 DIMENSIONS & AREAS 00 General 10 Fuselage 1 Dimensions 2 Stations 3 Zones 4 Access Panels 5 Service Clearances 20 Wing - Stations & Access 1 Dimensions 2 Stations 3 Zones 4 Access Panels 5 Service Clearances 30 Nacelle/Pylon - Stations & Access 1 Dimensions 2 Stations 3 Zones 4 Access Panels 5 Service Clearances 40 Tail Assembly - Stations & Access 1 Dimensions 2 Stations 3 Zones 4 Access Panels 5 Service Clearances 07 LIFTING & SHORING 00 General 10 Jacking 1 Jacking for Maintenance 2 Auxiliary Support 3 Support with Engine Removed 4 Lifting Damaged A/C 5 Lifting Damaged A/C with Jacks 6 Lifting Damaged A/C with Pneumatic Bags 7 Lifting Damaged A/C with Nose Gear Collapsed 20 Shoring 08 LEVELING & WEIGHING 00 General 10 Leveling 20 Weighing Procedures
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30 Weight
&
09 TOWING
3 Galley Units 60 Gaseous Service 1 Air 2 Nitrogen
Balance Data & TAXIING
00 General 10 Towing 20 Taxiing 30 Hand Signaling
3 4
00 General 01 Parking 1 Normal Parking 2 Prolonged Parking 3 Parking in High Winds 4 Parking with Engines Removed 20 Mooring
5 Oxygen 70 Tire Service 1 Inflation 75 Fire Extinguishers 80 Rain Repellent 90 Lubrication 1 Lubricants 2 Methods of Application 3 Charts
11 PLACARDS
14 EQUIPMENT
10 PARKING
& MOORING
AND MARKINGS
00 General 10 Exterior Color Schemes & Markings 20 Exterior Placards & Markings 30 Interior Placards & Markings NOTE: The NW Standard is to designate the ATA Chapter in which the placard falls for the subchapter number. E.G. A door placard would be numbered as 1152. 12 SERVICING
00 General 10 Refueling - Defueling 1 Refueling Procedure 2 Fuel Loading 3 Fire Hazards, Spills & Safety 4 Fuel Sump Draining 5 Ground Support Equipment 20 Oil Service 1 Engine Oil Servicing 2 Starter (Pneumatic) 3 Constant Speed Drive 4 Compressor (Air Conditioning) 5 APU 6 Nose Wheel Axle 30 Hydraulic Servicing 1 Aircraft Hydraulic Systems 2 Propeller System 3 Compressor (Air Conditioning) 40 Water Service 1 Potable Water 2 Nonpotable Water
OPERATION
00 General 10 Ground Operation Certification 1 Engine Operation/System Check 2 Support Equipment 20 Engine Operation/System Check (Runup) 1 Engine Operation 2 Systems Check 3 Aircraft Taxi 30 Discrepancy Analysis & Correction (Troubleshooting) 1 Engine (Including Power Profile) 2 Systems 3 Electrical 4 Electronics 15 TRAINING (REFERENCE PROGRAM MANUAL)
MAINTENANCE
00 General 10 All Personnel 1 Company Familiarization 2 Safety 3 Fire Prevention & Control 4 First Aid & CPR 5 SCEPTRE 6 FIMS 7 Aircraft Familiarization 20 Maintenance Initial 1 2
A & P R & E
30 Maintenance Differences 1 2
A & P R & E
3 Self help 40 Ground Service/Facilities 50 Cleaner 60 Stores 70 Pilots 80 Flight Attendant 90 Station Personnel
3 4
5 Batteries 50 Waste Service 1 Lavatories 2 Galley Containers 11
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7 Controls 8 Coils 30 Compressed Air 1 Compressor 2 Motor 3 Dryer 4 Controls 5 Piping 6 Valves (Also see 17-90-1) 7 System 40 Air Handling 1 Motors 2 Fans 3 Controls 4 Ducting 5 Coils 6 System 50 Emergency Power 1 Motor 2 Generator 3 Controls 4 Electrical 5 System 6 Emergency Lighting 60 Fire Protection 1 Tanks 2 Pumps 3 Hydrants 4 Portable Equipment 5 Valves (Also see 17-90-1) 6 Controls 7 Plumbing (Also see 17-90-2) 8 System 9 C02 Extinguishers 70 Servicing 1 Lighting 2 Water 3 Waste 4 Plumbing (Alse see 17-90-2) 5 Electrical 6 Doors 7 Dock levelers 8 Irrigation 9 Pneumatic Tube System 80 Lifting Equipment 1 Hoists 2 Jacks 3 Slings 4 Passenger Loading Bridges 90 Miscellaneous Equipment 1 Valves 2 Plumbing 3 Chemicals
16 GROUND SUPPORT EQUIPMENT 00 General 10 Fixed Refueling Equipment 1 Familiarization 2 Electrical 3 Pump 4 Motor 5 Filtration 6 Controls 20 Motorized Vehicles 1 Tug 2 Truck 3 Tractor 4 De-icer 5 Air Conditioner 6 Fork Lift 7 Loader 8 Fuel Truck 9 Hi Lift 30 Towed Vehicles 1 Bag Carts 2 Ground Heaters 3 De-icers 4 Air Starts 5 Hydraulic Mule 6 Tail/Wing Docks 40 External Ground Power 1 400 Cycle 2 28 VDC 50 60 70
80 90 Miscellaneous Equipment 17 FACiliTIES EQUIPMENT 00 General 10 Heating System 1 Boilers 2 Tanks 3 Pumps 4 Electrical 5 Plumbing (Also see 17-90-2) 6 Controls 7 Chemicals 8 Valves (Also see 17-90-1) 9 Coils 20 Air Conditioner 1 Chillers 2 Motors 3 Cooling Tower 4 Pumps 5 Plumbing (Also see 17-90-2) 6 Valves (Also see 17-90-1)
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20 STANDARD
PRACTICES
- AIRFRAME
5 Fueling/Defueling 6 De-icing/Anti-icing 7 Disinfect/Sanitize 8 Storage 70 Testing 1 Operational 2 Functional 3 System 4 Bite 5 Special 6
00 General 1 Shop Practices 2 Identification 3 Investigation 10 Cleaning 1 Chemical 2 Abrasive 3 Ultrasonic 4 Mechanical 5 Corrosion Removal 20 Inspection/Check 1 Visual 2 Detailed/Dimensional 3 Penetrant 4 Magnetic 5 Eddy Current 6 X-Ray/Holographic 7 Ultrasonic 8 Specific/Special 9 Boroscope 30 Correction/Repair 1 Welding/Brazing 2 Machine/Reaming/Blending 3 Stripping and Plating 4 Fiberglass/Plastic/Honeycomb/Epoxy 5 Plasma and Flame Spraying 6 Bonding and Molding 7 Heat Treating 8 Surface Treating 9 Machine Riveting & Flaring 40 Dissassembly/ Assembly 1 Disassembly/Open 2 Unit Removal 3 Disconnect/Loosen 4 Assembly/Close 5 Unit Installation 6 Reconnect/Tighten 7 Unassigned 8 Install Test Equipment 9 Install Support Equipment 50 Materials/Hardware 1 Fasteners 2 Cables 3 Pulleys 4 Tubing 5 Hoses 6 O-Rings 7 Decals/Placards 60 Servicing/Preserving 1 Servicing 2 Preserving 3 Depreserving 4 Lubricating
7
8 Pressurize/Depressurize 9 Leak Check 80 Processes 1 Fault Isolation 2 Adjusting/Aligning/Calibrating 3 Rigging 4 Balancing 90 Parts Manufacturing 21 AIR CONDITIONING
00 General 10 Compression 1 Eng.-Driven Air Compo System 2 Turbine Air Compo System
3
4 Related Controls 5 Related Indicating 6 Ventilation 20 Distribution 1 Ram Air System 2 Hot Air System 3 Bleed Air System 4 Cold Air System 5 Conditioning Air System 30 Pressurization Control 1 Sensing 2 Automatic Control 3 Manual Control 4 Emergency Control 5 Indicating 6 Pressure Relief 40 Heating 1 Combustion Heater System 2 Electric Heating 3 Cargo Compartment Heating 50 Cooling 1 Vapor Cycle 2 Heat Exchanger 3 Manual Control 4 Automatic Control 5 Indicating 6 Water Separation 7 Ram Air
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8 Air Cycle Machine 9 Equipment Cooling 60 Temperature Control 1 Sensing 2 Automatic Control 3 Manual Control 4 5 Indicating 70 Moisture/Air 1 2 3
Contaminant
30 Passenger Address & Entertainment 1 Passenger Address 2 Audio Entertainment 3 Video Entertainment 4 Portable Communications Control
5 Public Correspondence 40 Interphone 1 Flight 2 Service
Sensing Automatic Control Manual Control
2 3 4
10 Autopilot 1 Roll Control 2 Pitch Control 3 Yaw Control Engage Interlock Annunciation
6 7
Controlling Actuation
8 Indicating 9 Warning 20 Speed-Attitude 1 Sensing 2 Computing 3 Actuation
2 Display Panels 3 Control Computers 24 ELECTRIC POWER 00 General Correction
(Mach Trim)
10 Generator Drive (CSD) 1 Driving Mech and Disconnect 2 3 Control 4 Oil System 5 Indicating 20 AC Generation 1 Generator/ Alternator 2 Inverter & Control
1 Engaging 2 Amplification 3 Actuating 4 Warning 40 System Monitor
1 2 3
3 4
Cont. Reg. & Prot. Cross-tie
5 Indicating 6 Emergency Power 30 DC Generation 1 Generator
Indicating Aerondynamic Load Alleviating Sensing Computing Indicating Warning COMMUNICATIONS General HF
2 3 4
APU Generator System Cont. Reg. & Prot. Conversion
5 Indicating 6 Battery 7 Emergency Power 40 External Power
Transmit/Receive Control Antenna
1 2
20 VHF/UHF 1 2 3
Microphone Handsets Headsets
5 Speakers 60 Static Discharging 70 Audio Monitoring (CVR) 80 Integrated Automatic Tuning 1 Selector Panels
4 Indicating 5 Warning 30 Auto Throttle
1 50 1 2 3 4 23 00 10
(Airframe)
50 Audio Integrating 1 Control
4 Water Separation 5 Indicating 22 AUTO FLIGHT 00 General
4 5
Antenna Selcal ACARS
Satellite Communications Transmit/Receive Control
Coupling
3
Control
4 5 6
Indication & Warning AC Power DC Power
&
Protection
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50 Electrical Load Distribution 2 Wheel Wells 1 AC Busses 3 Tail 2 AC Protection 4 Battery 3 DC Busses 5 Hydraulic 4 DC Protection 6 Air Conditioning 5 Miscellaneous Electrical Items 80 Insulation 6 Ground Service 1 Flight Compartment 7 Flight Power Supply 2 Passenger Compartment 25 EQUIPMENT & FURNISHINGS 3 Cargo/Accessory Compartments 00 General 26 FIRE PROTECTION 10 Flight Compartment 00 General 1 Seating 10 Detection 1 Heat 2 Wall & Ceiling Furnishings 3 Floor Furnishing 2 Smoke 4 Tables 20 Extinguishing 5 Electrical Equipment Rack 1 Storage 6 Coat Compartment 2 Distribution 7 Miscellaneous Furnishings 3 Control 20 Passenger Compartment 4 Indicating 1 Seats & Leg Rests 5 Portable 30 Explosion Suppression 2 Wall & Ceiling Furnishings 3 Floor Furnishings 1 Indicating 4 Movable Partitions. Curtains 2 Extinguishing 5 Hat Racks. Passenger Service Units and 27 FLIGHT CONTROLS Berths 00 General 6 Stowage Compartments 10 Aileron and Tab Control 7 Misc. Furnishings/Publications 1 Aileron Manual Control 30 Buffet and Galley 2 Aileron Power Control 1 Buffet & Galley Structure 3 Aileron Tab Manual Control 4 Aileron Tab Power Control 2 Wall & Ceiling Furnishings 3 Floor Furnishings 5 Position Indicating 4 Ovens 6 Aileron Dampers 5 Mechanical Refrigerator 20 Rudder and Tab Control/Ruddervator 6 Coffee Makers 1 Rudder Manual Control 7 Waste Container 2 Rudder Power Control 8 Trolleys/Carriers 3 Rudder Tab Manual Control 40 Lavatories 4 Rudder Tab Power Control 1 Lavatory Structure 5 Position Indicating 2 Wall & Ceiling Furnishings 6 Rudder Dampers 3 Floor Furnishings 7 Rudder Limiters 4 Miscellaneous Furnishings 30 Elevator and Tab Control/Elevon 50 Cargo Compartments/ AG Spray Apparatus 1 Elevator Manual Control 1 Walls and Ceilings 2 Elevator Power Control 2 Floors and Bracing 3 Elevator Tab Manual Control 3 Restraining 4 Elevator Tab Power Control 4 Loading/Unloading Systems 5 Position Indicating 60 Emergency 6 Warning Systems 1 Evacuation 7 Elevator Dampers 2 Flotation 8 Elevator Limiters 3 First Air Equipment 40 Horizontal Stabilizer Control/Stabilator 4 Landing & Signal Flares 1 Manual Control 5 Emergency Megaphones 2 Power Actuation 70 Accessory Compartments 3 Alternate Trim Control 1 Avionics/Electrical 4 Drive System
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5 Indicating - Position and Motion 50 Flaps - Trailing Edge Control 1 Manual Control 2 Power Actuation 3 Bus System 4 Takeoff Warning 5 Indicating 60 Spoiler, Drag Devices and Variable Aerodynamic Fairings Control 1 Manual Control 2 Power Actuation 3 Spoiler Control 4 Warning Systems 5 Indicating 70 Gust Lock and Dampener Control 1 Manual 2 Power 80 Lift Augmenting Control 1 Manual Control 2 Power Actuation 3 Mechanical Activation 4 Warning Systems 5 Indicating 28 FUEL 00 General 10 Storage 1 Integral Storage 2 Bladder Storage 3 Aux Fuel Tanks (Removable) 4 Venting & Relief 5 Reservoir Feeding 20 Distribution/Drain Valves 1 Pumps & Valves 2 Supply Lines 3 Fuel & Defuel (include valves & adapters) 4 Control 5 Aux Fuel System (Removable) 30 Dump 40 Indicating (Not Engine) 1 Pressure 2 Quantity 3 Temperature 4 Fuel Level Indicator Sticks 29 HYDRAULIC POWER 00 General 10 Main 1 Storage 2 Power 3 Distribution 4 Regulation & Control 5 Filtration 20 Auxiliary 1 Electric Pump 2 Reversible Motor Pump
3 Distribution 4 Regulation & Control 5 Filtration 30 Indicating 1 Quantity 2 Pressure 3 Temperature 30 ICE AND RAIN PROTECTION 00 General 10 Airfoil 1 Wings 2 Stabilizers 3 Pylons 4 Controlling & Indication 5 Stroke Anti-ice 20 Air Intakes 1 Wings 2 Stabilizers 3 Fuselage 4 Power Plant 5 Controlling & Indication 30 Pitot and Static 1 Pitot Heat 2 Static Heat 3 TAT/RA T Probe Heat 4 Angle of Attack Vane Heat 5 Current Indication 6 Annunciation 40 Windows, Windshields & Doors 1 Windshield Anti-ice/ Anti-fog 2 Windshield Rain Repellent 3 Windshield Wipers 4 Windshield Washers 50 Antennas and Radomes 1 Electrical 2 Air 60 Propellers/Rotors 1 Electrical 2 Fluid 70 Water Lines 1 Water Service Panel Heat 2 Drain Mast Heat 3 Potable Water Heat 80 Detection 1 Sensing 2 Indicating 31 INDICATING/RECORDING SYSTEMS 00 General 10 Panels 1 Captain's Flight Inst. 2 First Officer's Flight Ins!. 3 Center Inst. 4 Overhead Panels 5 Pedestal & Consoles
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6 Cabin Attendant's 7 Miscellaneous Elect. & Service 20 Independent Instruments 1 Clocks 2 Inclinometer 30 Recorders 1 Flight Recorder 2 AIDS 40 Central Computers 1 EICAS 50 Central Warning System 1 Master Warning 2 Aural Warning 3 Annunciators 60 Central Display Systems 32 lANDING GEAR 00 General 10 Main Gear and Doors 1 Main Gear 2 Main Gear Latches 3 Main Gear Doors (Doors Attached to Gear\ 20 Nose Gear & Doors (Tail Gear) 1 Nose Gear/Tail Gear 2 Nose Gear Latches 3 Nose Gear Doors (Doors Attached to Gear) 30 Extension & Retraction/Level Switch 1 Mechanical 2 Hydraulic 3 Electrical 4 Main Gear Door Mechanisms 5 Nose Gear Door Mechanisms 6 Emergency Actuation Mechanisms 40 Wheel Assemblies and Brakes 1 Main Gear 2 Nose Gear 3 Temp/Press Indication 4 Brakes, Main and Nose 5 Brake Hydraulic Control 6 Anti-Skid 7 Emergency Brakes 8 Auto Brake 50 Steering 1 Mechanical Control System 2 Nose Gear Hydraulic Control 3 Supplementary Gear 60 Position & Warning/Ground Safety Switch 1 Main Gear 2 Nose Gear 3 Supplementary Gear 70 Supplementary Gear/Skis/Floats 1 Fuselage 2 Wing
3 Tail Skid 80 Service Clearances 33 LIGHTS 00 General 10 Flight Compartment & Annunciators 1 General Illumination 2 Panel Indirect Light 3 Panel Flood Lighting 4 Master Warning, Caution 20 Passenger Compartment 1 General Illumination 2 Passenger Warning 3 Reading Lights 4 Cabin Attendant Call System 5 Galley/Lavatory Area Lighting 30 Cargo & Service Compartments 1 Cargo Compartment 2 Wheel Well 3 Equipment Compartment 4 Service/Tail Areas 40 Exterior 1 Landing & Taxiing 2 Anti-Collision 3 Navigation 4 Floodlighting 50 Emergency Lighting 1 Fixed 2 Portable 3 Evacuation Slide Lighting 34 NAVIGATION 00 General 10 Flight Environment Data 1 Pitot and Static 2 Air Temperature & Thrust Limit 3 Rate of Climb 4 Airspeed 5 High Speed Warning 6 Altitude 7 Air Data Computers 8 Stall Warning 9 Speed Command 20 Attitude and Direction 1 Attitude Indication 2 Gyro Compass System 3 Magnetic Compass 4 Turn and Bank 5 Flight Director 6 Instrument Comparator 30 Landing & Taxi Aids 1 Localizer 2 Glideslope 3 Microwave Landing 4 Marker 5 Heads Up Display
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6 Radio Altimeter 40 Independent Position Determining 1 Inertial Guidance System 2 Weather Radar 3 Doppler 4 Ground Proximity Warning 5 Air Collision Avoidance 50 Dependent Position Determining 1 DME/TACAN 2 Transponder 7
3 4 LORAN 5 VOR 6 7
8 60 1 2
3
ADF Global Positioning System OMEGA Flight Management Computing Course Computer Data Computer Control Display Unit Warning Annunciator
4 35 OXYGEN
00 General 10 Crew 1 Storage & Regulation 2 Controls & Valves 3 Distribution 4 Indicating 20 Passenger 1 Storage & Regulation 2 Controls & Valves 3 Distribution 4 Indicating 30 Portable 1 Crew 2 Passenger 36 PNEUMATIC 00 General
10 Distribution 1 Powerplanti APU Generation 2 Wing 3 Fuselage 4 Control 20 Indicating 1 Pressure 2 Temperature 3 Warning 37 VACUUM
00 General 10 Distribution 1 Powerplant 2 Wing 3 Fuselage
4 Control 20 Indicating 1 Pressure 2 Quantity 3 Temperature 38 WATER/WASTE
00 General 10 Potable 1 Storage 2 Distribution 3 Indicaiton 4 Temperature Control 20 Wash 1 Storage 2 Distribution 3 Indication 4 Heating 30 Waste Disposal 1 Wash Basins & Drains 2 Water Closets/Flush/Storage 40 Air Supply 1 Distribution 2 Control 39 ELECTRICAL/ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS
00 General 10 Instrument & Control Panels 20 Electrical & Electronic Equipment Racks 30 Electrical & Electronic Junction Boxes 40 Multipurpose Electronic Components 50 Integrated Circuits 60 Printed Circuit Card Assemblies 45 CENTRAL
MAINTENANCE
SYSTEM
(CMS)
50 thru 59 60 thru 69 70 thru 89
General CMS Aircraft General CMS Airframe Systems CMS CMS Structures CMS Propellers CMS Powerplant
49 AIRBORNE
AUXILIARY
00 5 thru 19 20 thru 44 45
POWER
00 General 1 APU Change 10 Powerplant 1 Cowling 2 Mounts 3 Fireseals 4 Attach Fittings 5 Electrical Harness 6 Air Intakes 7 Engine Drains 20 Engine 1 Reduction Gear & Shaft Section
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2 Air Inlet Section 3 Compressor Section 4 Combustion Section 5 Turbine Section 6 Accessory Drives 7 By-pass Section 30 Engine Fuel and Control 1 Distribution 2 Controlling 3 Indicating 40 Ignition/Starting 1 Electrical Power Supply 2 Distribution 3 Switching 4 Cranking 50 Air 1 Engine Anti-icing 2 Accessory Cooling 3 Compressor Bleed Control 4 Indicating 60 Engine Controls 1 Power Control 2 Emergency Shutdown 70 Indicating 1 Power 2 Temperature 3 Analyzers 4 Integrated Inst. Systems 80 Exhaust 1 Collector/Nozzle 2 Noise Suppressor 3 Unassigned 4 Supplementary Air 90 Oil 1 Storage 2 Distribution 3 Indication 51 STRUCTURES/STANDARD
3 Insulation, Lining 4 Integral Steps, Ramps Handrails, Fittings 20 Emergency Exit 1 Emergency Exits 2 Emergency Exit Doors 30 Cargo/Baggage 1 Baggage 2 Baggage Door Actuation 3 Cargo (Cargo A/C Only) 4 Cargo Door Actuation (Cargo A/C Only) 40 Service 1 Galley 2 Elect./Electrical Compartment 3 Hydraulic Compartment 4 Accessory Compartment 5 Air Conditioning Compartment 6 Fluid Service 7 APU 8 Tail Cone 50 Fixed Interior 1 Flight Compartment 2 Lavatory 3 Galley 4 Cargo Compartment 5 Avionics Compartment 6 Coatroom 60 Entrance Stairs 1 Structure 2 Control 70 Door Warning 1 Indicating 80 Landing Gear (Doors Attached to Airframe Structure) (See Chapter 32 Also) 1 Structure 2 Latch/Handle/Control Mechanism 3 Fittings Aerodynamic Smoothness PRACTICES
53 FUSELAGE
00 General 10 Investigation, Cleanup and Aerodynamic Smoothness 20 Processes 30 Materials 40 Fasteners 50 Support of Airplane for Repair and Alignment Check Procedures 60 Control-Surface Balancing 70 Repairs
00 General 10 Main Frame 1 Frames 2 Bulkheads 3 Formers 4 Longerons/Stringers 5 Keels 6 Opening Frames 20 Auxiliary Structures 1 Floors 2 Internal Mounting Structures 3 Internal Stair5 4 Fixed Partitions 30 Plate/Skin 1 Skin
52 DOORS
00 General 10 Passenger/Crew 1 Structure 2 Latch/Handle/Control
Mechanisms
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2 Doublers 3 Access Covers 40 Attach Fittings 1 Wings 2 Stabilizers 3 Landing Gear 4 Bulkhead & Stringer 5 Door Hinges 6 Equipment 7 Powerplant ,0 Aerodynamic Fairings 1 Nose 2 Wing 3 Tail 4 Stabilizer 60 Strokes
locations will then be defined by manufacturing joints or other suitable demarcation in sequence from front to rear). 55 STABILIZERS
00 General 10 Horizontal Stabilizers/Stabilator 1 Main Spars/Ribs 2 Auxiliary Structure 3 Plates/Skin 4 Fairings 5 Access Covers 20 Elevators/Elevon 1 Main Spars/Ribs 2 Auxiliary Structure 3 Plates/Skin 4 Fairing 5 Control Tab 6 Geared Tab 7 Balance Devices 30 Vertical Stabilizers 1 Main Spars/Ribs 2 Auxiliary Structure 3 Plates/Skin 4 Fairings 5 Access Covers 40 Rudder/Ruddervator 1 Main Spars/Ribs 2 Auxiliary Structure 3 Plates/Skin 4 LE & TE Fairings 5 Trim/Control Tab 6 Balance Devices 50 Attach Fittings 1 Horizontal Stabilizer 2 Elevator and Tab 3 Vertical Stabilizer 4 Rudder and Tab
(Some A/C may have the complete fuse,age structure grouped together with assignment by section. The section locations will then be defined by manufacturing joints or other suitable demarcation in sequence from front to rear). "4 NACELLES/PYLONS J General 10 Main Frame 1 Frames ~ Bulkheads & Firewall J Longerons/Stringers 4 Spars/Drag Struts 5 Keels Opening Frames ~O Auxiliary Structures 1 Leading Edge 2 Trailing Edge J Tip 30 Plates/Skin 1 Skin '2 Doublers 3 Access Covers 4 Heat Shields (Not Firewalls) 40 Attach Fittings 1 Wing 2 Powerplant 3 Thrust Reverse/Sound Suppressor 4 Landing Gear J Fillets/Fairings 1 Wing 2 Powerplant
56 WINDOWS
00 General 10 Flight Compartment 1 Windshield Assemblies 2 Fixed Window Assembly 3 Movable Window Assembly & Mechanisms 20 Passenger Compartment 1 Window Assembly/Structure 2 Window Assembly/Non-Structure 30 Door 1 Window Assemblies 40 Inspection & Observation 1 Window Assemblies 2 Observation Viewers 3 Wheelwell Viewing 4 Astrodome
(Some A/C may have the complete Nacelle/Pylon structure grouped together with assignment by section. The section Xl
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57 WINGS
00 General 10 Main Frame 1 Spars 2 Ribs/Bulkheads 3 Longerons/Stringers 4 Opening Frames 5 Center Wing Box 20 Auxiliary Structure 1 Leading Edge and Tip 2 Trailing Edge 3 Fuel Tank Aux Structure 4 Cell Backing Boards 30 Plates/Skin 1 Skin 2 Doublers 3 Access Covers 40 Attach Fittings 1 Fuselage 2 Nacelle/Pylon 3 Landing Gear 4 Bulkheads and Stringer 5 Control Surfaces 6 Equipment 50 Flight Surfaces 1 Ailerons 2 Aileron Tabs 3 Trailing Edge Flaps 4 Leading Edge Slats 5 Spoilers 6 Balance Devices 60 STANDARD
PRACTICES
- PROPELLER
00 General 61 PROPELLERS
00 General 1 Prop Change 10 Propeller Assembly 1 Blades 2 Hub 3 Deicing 4 Fairing 20 Controlling 1 Governor 2 Feath./Reversing 3 Manual 30 Braking 1 Actuation 40 Indicating 1 Switch/Lights 70 STANDARD
PRACTICES
00 General 1 Shop Practices 2 Identification 3 Investigation
-
ENGINE
10 Cleaning 1 Chemical 2 Abrasive 3 Ultrasonic 4 Mechanical 5 Corrosion Removal 20 Insp/Check 1 Visual 2 Detailed/Dimensional 3 Penetrant 4 Magnetic 5 Eddy Current 6 X-Ray/Holographic 7 Ultrasonic 8 Specific/Special 9 Boroscope 30 Correction/Repair 1 Welding/Brazing 2 Machine/Reaming/Blending 3 Stripping and Plating 4 Fiberglass/Plastic/Honycomb/Epoxy 5 Plasma and Flame Spraying 6 Bonding and Molding 7 Heat Treating 8 Surface Treating 9 Machine Riviting & Flaring 40 Disassembly/Assembly 1 Disassembly/Open 2 Unit Removal 3 Disconnect/Loosen 4 Assembly/Close 5 Unit Installation 6 Reconnect/Tighten 7 Install Test Equipment 8 Install Support Equipment 50 Materials/Hardware 1 Fasteners 2 Cables 3 Pulleys 4 Tubing 5 Hoses 6 O-Rings 7 Decals/Placards 60 Servicing/Preserving 1 Servicing 2 Preserving 3 Depreserving 4 Lubricating 5 Fueling/Defueling 6 De-icing/Anti-icing 7 Disinfect/Sanitize 8 Storage 70 Testing 1 Operational
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2 3 4 5 6
Functional System Bite Special
7
8 Pressure 9 Leak 80 Processes 1 Fault Isolation 2 Adjusting/Aligning/Calibrating 3 Rigging 4 Balancing 90 Parts Manufacturing 71 POWER PLANT GENERAL
-5 Failures -6 Maintenance -7 Service Evaluation -8 Engine Emissions and Noise -9 Mise Turbine 10 Reduction Gear and Shaft Section 1 Rotating 2 Cases 3 Lubricating 4 Accessory Drives 20 Air Inlet Section 1 Front Accessory Drive Group 2 Guide Vanes 3 Fan Inlet Group 30 Compressor Section 1 Froont Cases 2 Lower Pressure Cases (Stators) 3 Low (N1) Compressor Rotor 4 Compressor Intermediate Group 5 High Pressure Cases (Stators) 6 High (N2) Compressor Rotor 7 Diffuser Group 8 Diffuser Outer Fan Ducts 40 Combustion Section 1 Combustion Section 50 Turbine Section 1 Turbine Nozzle Group 2 High (N2) Turbine 3 Low (N1) Turbine 4 Exhaust Case Section 5 Fan and Exhaust (Mixer) Section 60 Accessory Drives 1 Internal 2 External 70 By-pass Section 1 Fan Discharge Section
00 General 1 Engine Change 10 Cowling 1 Intake Cowling 2 Fixed Cowling 3 Movable Cowling 4 Pylon Aprons 20 Mounts 1 Main Structure 2 Vibration Dampeners 3 Support Fittings 30 Fireseals/Shrouds 1 Fireseals 40 Attach Fittings 1 Attach Fittings 50 Electrical Harness 1 Electrical Harnesses 60 Air Intakes 1 Nose Ring Cowls 2 Engine Air Inlet Duct 3 Oil Cooler Inlet Duct 80 4 Nose Fairing 90 Conversions 5 Scoops 72 ENGINE (RECIPROCATING) 6 Compo Fan Cowls 00 General 7 Buried Ducting 8 Actuators, Wiring, Controls Linkages, 10 Front Section 20 Power Section Doors, Etc.) 30 Cylinder Section 9 Warning System & Position Indicators 40 Supercharger Section 70 Engine Drains 50 Lubrication 1 Lines/Manifolds 2 Vents 73 ENGINE FUEL AND CONTROL 3 Tanks 00 General 10 Distribution 72 ENGINE (TURBINE/TURBOPROP) 00 General 1 Plumbing 2 Valves & Controls -1 Procurement 3 Fuel De-Icing -2 Performance (Monitoring) 4 FiIters -3 Operations -4 Overhaul 20 Controlling
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1 Automatic 2 Manual 30 Indicating 1 Flow 2 Temperature 3 Pressure 74 IGNITION 00 General 10 Elect. Power Supply 1 Exciters 2
20 Distribution 1 Harnesses 2 Ign iters 30 Switching 1 Direct 2 Remote 75 AIR 00 General 10 Engine Anti-icing 1 Valves, Regulators 2 Ducting 20 Accessory Cooling 1 Distribution 2 Controlling 30 Compressor Bleed Control 1 Automatic 2 Manual 40 Indicating 1 Pressure 2 Control Position 3 Temperature 76 ENGINE CONTROLS 00 General 10 Power Control 1 Mechanical 2 Electrical 3 Pneumatic 4 Hydraulic 20 Emergency Shutdown 1 Manual 2 Automatic 77 ENGINE INDICATING 00 General 10 Power 1 Pressure Radio 2 Speed 3 Thrust/Torque 20 Temperature 1 Inlet 2 Exhaust Indication 3 Thermocouple System 30 Analyzers 1 Vibration
2 Ignition 40 Integrated Engine Instrument Systems 1 Transmitters 2 Receivers 3 Computers 78 EXHAUST 00 General 10 Collector/Nozzle 1 Rings 2 Ducts 3 Nozzles 20 Noise Suppressor 1 Baffles/Shields 30 Thrust Reverser 1 Clamshells 2 Actuation 3 Control System 4 Indicating & Warning 40 Supplementary Air 1 Tertiary Air Doors 2 Indicating & Warning 79 OIL 00 General 10 Storage 1 Tanks 20 Distribution 1 Plumbing 2 Pumps, Valves & Coolers 3 Filters 30 Indication 1 Quantity 2 Pressure 3 Temperature 4 Detectors 80 STARTING 00 General 10 Cranking 1 Starter 2 Valves & Controls 81 TURBINES (RECIPROCATING EN G) 00 General 10 Power Recovery 20 Turbo-Supercharger 82 WATER INJECTION 00 General 10 Storage 1 Tanks 20 Distribution 1 Plumbing 2 Pumps/Valves 30 Dumping & Purging 1 Plumbing 2 Control
xiv
40 Indicating 1 Pressure 2 Quantity 3 Temperature 83 ACCESSORY
GEAR BOXES
00 General o Drive Shaft Section 1 Shafts 2 Torquemeters ~OGear Box Section 1 Drive Gears 2 Reduction Gears 3 Seals 4 Lubrication :11 CHARTS
00 General 10 Control Cables '0 Flex Hoses 30 Tubing 40 Conduit & Wiring 1 Junction Box Locations 2 Disconnect Plugs 3 Spare Wiring 99 Miscellaneous
xv Aircraft Technical Book Company
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Quick Identification
Aircraft Technical Book Company
800-780-4115
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•
• 1--1
•• 1--1
AN 3 thru AN 20 Hex Head Bolt Steel & Stainless Steel
125,000 psi Min. T.S. Aluminum 62,000 psi Min. T.S.
e
AN 73 thru AN 81 Hex Head Bolt
I
w--
--
_
125,000 psi Min. T.S.
AN 173 thru AN 186 Hex Head Bolt, Close Tal. Shank Alloy & Stainless Steel & Aluminum
AN Screw, 500 Mach. thru AN Fillister 501 Head, Slotted Carbon Steel, CRES, Brass
•• .~ e
AN 502 thru AN 503
___ W
_. _.
Screw,Steel Mach. Drilled Fillister, Alloy 125,000 psi Min. lS .
Slotted
AN 505 Screw, Mach. Flat Head 82° Carbon Steel, Brass, CRES Alum.
AN 507 Screw, Mach. Flat Head 100° Carbon Steel, CRES, Brass, Alum.; Slotted & Recessed AN 509
AN
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8
510
Screw, Mach. Flat Head 82° Carbon Steel, CRES, Brass, Alum.; Recessed
••
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AN 515 and AN 520 Carbon Mach. Screw, Steel, Round Brass, Head CRES, Alum.; Recessed
Screw, Mach. Washer Head Steel, Alum.; Slotted & Recessed AN 525 AN 526
1
"
Carbon Mach. Screw, Steel, Truss CRES,Head Alum.; Recessed AN 530
4~ .....,
Thread Cutting, Round Head, Spaced Thd., Recessed, CarbonThread or CRES Steel or Screw, Tapping, Forming AN 531
•I ~ ,~
•_1
Thread Tapping, Screw, Cutting, 82° Thread Flat Forming Head, Spaced or Thd., Recessed, Carbon or CRES Steel
Hex Head Bolt Alloy & CRES Steel AN 101001 thru AN 108200 125,000 psi Min. T.S.
:.1. Screw, Mach. Flat Head 100° Alloy Steel, Alum., CRES; Recessed
Aircraft Technical Book Company
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~
Z
1-AN36
•
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AN3-AN20 Close tolerance MS24566 I
=
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Bol t-aircraft AN210 AN 173-186 Pulley, anti-friction
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AN4'2-AN49
AN219
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Bolt-eye AN73-AN81
MS2219 I Pulley-groove, ~ secondary control, aircraft I ANnO MS20220
Bolt-machine,
drilled
I Pulley
ANIOO
AN221 MS20221
C~) c::J ...... -.-.- -.
Thimble,
wire-cable
Pulley, AN227-6
AN 115-116 I
Sh.ckl,,· anchor
I
~
• wire rope and~
AN130-170
Butlon (["ten."
~
snap and curtain)
~
ANn7-7
II Turnbuckle
groove, heavy duty
II
I· cfu-=~
assemblies 2
Aircraft Technical Book Company
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AN 227-8 and curtain) AN227-10
urtain) 27-9 227-15
AN 253
-
~
AN250 AN 240 with washers AN230 Grommets Eyelet-lacing
@~ I ~Hinges,
~
curtain) ~ fastenersand snap
Socket (fasteners and curtain)
snap
assemblies
& parts
Pin-hinge
AN227-16
AN254
Plate (fasteners snap and curtain)
Screw, thumb necked
AN227-21
AN255
Hex Base
thru -26
Screw, external. relieved body
Stud
AN229
AN256
Fasteners Inter!. slide
Nut, self-lock right angle plate
o 88
3 Aircraft Technical Book Company
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05 Nut, plain, Nuts, castellated hex. Fittings, lubrication non-structural ejoint cap plain universal, Plain~
01U
@ @ ©
AN341~ ~~~ AN270-27 ~~plain, I AN276 Nut, ~ wing Nut-check Nut, plain, hex, AN257
n-s, fine coarse thr. n-s, thread
e
~
@
Nut, plain, Nut, plain, hex., hex., AN 320 AN316 AN345 335 AN350 AN 340
@
Nut-cas tie shear
4 Aircraft Technical Book Company
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F king nut 5500 plate, F unters., Pin-cotter ,mped engine nut-plate, 06 Nut, self-locking, 250° F ~ elf-locking,
b~ @~
en,i•• , ,\ott.d@
~
~
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AN355 D Q countersunk 1000,~ 5500 F. ~ ~ CountersunkAN362 AN364 363 AN ~ Nut-plate, non ~
lIJ
Pin-flat head AN365 AN373 AN AN380 386 & 381 AN 366 AN392 thru AN385 100°, 250° F AN406 Pin, plain taper counters., 250° F Threaded taper pin ,..
aw
©
~
5 Aircraft Technical Book Company
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aHoy minum Alloy - ss, Brazier ,ock monel Head,thread cutting 0426 . 56 27 41 ad 30 26 ~csk. 1000 head 16 safety
AN470 -IAN486 c::::D0 solid-universal head, ~Screw-tapping, AN41S ~ ~ Ri ve t, MS20470 steel, al. aHoy monel, copper
c::DO
c:=::D@ c:::D0 c:=tJ®
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Clevis-rod end adj. Rod end-threaded AN 490 504 AN481 Clevi s-rod end, AN al. ANS02 aI.head &aHoy ANS03 ANSOO ANSO Ifine driHed, coarse Screw-machine,· hd. Scre w-machin e &fill. rod.& head, macho thread fillister
~
~~
~
6 Aircraft Technical Book Company
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-'3 ..c@
d, 1000 ew-machine, round head 507 508 515 506 510 509 & AN520thread forming or d, ~ ~ nd head ew machine, typo ew-machine, flat~ ~ ow-tnpping,
.a@ ~
AN505 820 coarse
Screw-tapping, thread Screw-tapping, ~~
Drive round.head Screw-washer headhead, cutting, 82° flat hd.head820 buttonhe ad flat thread cutting, AN AN525 53 Iscrew, rod. hd. AN535 AN530 Screw-wood, round AN526 AN 545 AN 550 Screw-wood,
c:r@ ~~ Screw-machine
~
7 Aircraft Technical Book Company
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rod minal-wire rope stud all End, swaging N663 N658 tubeswaging support, N665 B0ail End, 664 clevis, lII~nm_u"O ( ~~ ork end
OJ (l
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Clamp-plain, (~ AN565 ~(~ ~ fluted loop socket typefork swaging, end ClamploopAN666 AN667 ~
r.-v
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type bonding rope, ~studend AN742 AN669 AN741 Terminal-wire AN668 Bracket-support clamp Terminal-swaging, eye AN737 AN743 Clamp-hose Clamp-tube
0
~~
AN 735
~
8 Aircraft Technical Book Company
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T
-flared tube and tip e-assembly el fitting, flanged 77~ 776 74 Elbow, ~ 450 ~tube Tee-flared ~ w-universal 900
l:QJ
AN753 AN771 AN763 AN775
d
Nipple
a 4D
0
Tee AN779 AN781 AN784 AN785 AN778 AN780 AN783 Coupling-union Nipple-union Tee-flared tube
~ ~
~
~
9 Aircraft Technical Book Company
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Elbow-union high pressure Nut, union Nipple-flared tube, AN800 Cap-air valve, AN807
a.\:]
~ ~ ~
I AN786III w/buckhead
~
I onrun
•
01ife
Nut-coupling tube Union-flared AN809 AN818 Valve, AN81S stem AN817 AN816 AN813 !AN814 Nut-coupling pipe & thread Bleeder Plug I~I
(IJ)
~
I
I
10 Aircraft Technical Book Company
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N822 N821 N824 N823 820 ee
~ ~
I
AN819
dJ ro
~~~ Elbow, 450 450 Elbow,
,T+••
Tee Tee AN839 AN833 AN832 AN827 AN 826 Elbow AN834 AN837 Cros s 900 Union-fl ared tube
~
~
II Aircraft Technical Book Company
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Nipple-pipe thr. Plugs ~ Gasket-metal hose to Ring-hydraulic 450 900 900
•
F{ct~ 831
~ m¢:1P ~~~ ~
AN840
Gasket-copper
Bushing AN901 AN900 AN894 AN902 Coupling-pip e thr. AN905-909 AN910 AN911
~
~
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12
Aircraft Technical Book Company
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Reducer N914 N918 oss-into N91S bow 900 pipe N913 N917 bow 450 shing-reducer
t:8 [gJ CBJ
•
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AN912
Washer-lock, Grommet-plastic
Plug AN924 Cap assembly Nut-flared tube AN929 AN93S AN932 AN933 AN919 Plug AN931 spring
g11 ©P
13
Aircraft Technical Book Company
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AN936
Washer-tooth
0
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lock
AN960
I
@
AN96 1
AN937
Cross Internal Screw Thread
W"h«-O,'
@
W"h«-O""eo"kal (Brass,
@
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AN938
AN970
Tee Internal Screw Thread
Washer-flat, wood
AN939
AN975
Elbow, 900 Internal Screw Thread
Washer-flat
AN941
AN995
@
Lock Wire Elbow, 450 Internal Screw Thread AN944
AN996
Fittings, lubrication
Clip
AN950~55
AN 3039
Washer-ball socket, ball seat
Light assembly
o
14
Aircraft Technical Book Company
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0
~® m, CD
AN3066 AN 3062 AN3050
duit . conduit dui t 450
conduit 450
3056 306 3054 30 58I 3053
AN3060
ule-flexible Nut-coupling, rule-rigid ~ pling-
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Coupling-e1ec. Elbow-electrical Seal Assembly
~
Elbow-electrical conduit 900 electrical conduit coupling AN Nut-plain, hex. AN3068 AN3063 Box3064 connector, AN3067 conduit 900 conduit Receptacle-fuel
AN3117
~
15 Aircraft Technical Book Company
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•
Gasket h Q(IJ slide St,,'e 229 0n 196-3199 170 Packing-V ring ~ ator-limi t w Assembly
~D
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~ • ICTube AN4024 Assembly AN6003 t00 0 0c;J ur: ~ 0Ijp=IJ AN3169 • ~
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@~
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~
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16
Aircraft Technical Book Company
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aulic 231 249 246 232 230 aul ic 227 strip ing-O ring, ket-O ring, g-hydraulic, per, rod,
~~.
,.:. AN6226 \,
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low pre ssure Hose Assembly, AN8002-2 gasket back-up AN629 AN6270 1mount AN6290 AN8013 Shock, AN8008 universal fitting AN6289 (Rubber) Washer, insulator Packing-preformed
'i\~"~>J'"
'
~
17
Aircraft Technical Book Company
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AN 10 100 1- 10 1900
AN 107301-108200
Bolt-hex., head
Bolt hex. dri lied head, (six holes), corrosion resistant
~
steel,
AN 10190 1-102800
AN 115401-115600
Bol t-hex., drided shank, steel
Screws-flat fIll. head, steel, .190-.375
AN 102801-103700
AN 115601-115800
.
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Boll-d"lI,d h
~
(one hole) , steel ex. he~
Drilled shank Screw f~ head, steel, .190-.375
AN 10370 1-104600
AN 115801-116150
Boll-d"lIod h ~~ ",,' • ( SIX . holes) ox. h'~ ,
Screw-flat fill. head, steel, .190-.375
AN 10460 1-105500
ANI 16901-117080
Boll-hox. hood co·rroslOn resistant '
cq
AN 105501-106400
~
fill. head, steel
AN 12150 1-121550
Bolt-hox. hood. d" ~ shank, corrosion
Screw-oval
steel
st.
resistant
Nut-plain steel
steel
AN 121551-121600
AN 10640 1- 107300
~ Bolt-hex., drilled head, (one hole), corrosion resistant
or cres.
st.
I Nut-castel.,
hex.
18
Aircraft Technical Book Company
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0~
steel, inconel 23020-123119 -solid 23151-123750 22576-122600 24951-125550 Gasket al. asbestos 23851-124050 D
at head steel clevi s paoking, 0 ring, er-plain
UTI (Q)
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AN 121601-121925 0I@ ~ ~inconel steel, 1000 head, drilled, steel, ctsk. drilled .190-.625 & undrille d TITI I Ri vet-solid universal \,,::;} Plug, straight thread
Bolt-socket head, 6-hole Stud-straight, .250-.625, Pin-lock, AN 150401-150450 steel, brass shear slotted 125951-130774 150501-170900 drilled & undrilled AN 125551-125700 125901-125950 15020 1-150400 Stud-stepped, head, steel steel AN 148551-149350 Nut-hex.,
check &
19 Aircraft Technical Book Company
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I•
1_ II•• t NAS 514
I~
.'
95,000 psi Min. S.S. __ I Full 100° Threaded. Flush Head AlloyBolt Steel 75,000 125,000 Mach. psi psiMin. Min. 100° T.S. 95.000 Hex T.S. Flat Head psi Head Bolt Min. S.S.220 thru NAS 224 I Screw, Internal Full Threaded. Wrenching Alloy Bolt Steel __ I Stainless Steel NAS __ Bolt NAS 563-572 464 ~_ I 100° Flush1 Head NAS 501 333 thru NAS thru NAS 1020 NAS 1103 thru NAS NAS340 1120 NAS 517 NAS1003 600 thru thru NAS 606 NAS 144 NAS 158
t1••• _. I_II
Aircraft Technical Book Company
•• _I• • I._1
Hex Head Bolt 160.000 psi T.S. S.S. 140,000 95,000 psi Min. 160.000 psi Min. Min. T.S. Hex Head Bolt Screw. Mach. Pan Head. Phillips, Hex Head Bolt
800-780-4115
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Red End alloy steel inuous, al. alloy, steel -iner SSO S40 S42 S4-S S43 SIS-16Bushing-flanged,
ings, cers-screw
~© (~~~
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(
~)
21 Aircraft Technical Book Company
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\
1
./ -& - -~--; - - - - - Bolt-1000, -" ( ,-NAS363 Control Rod Control Rod, plain tol erance, hi-s close trength NAS354 thru NAS362 Control Rod.& ,n~NAS364 NAS312 thru NAS320 NAS333 NAS340 ~ 'J --, ) m.b.~ WImI/~ steel, ~ NASI44 })Wl thru NASI58 , ........ " Control Rod, OllJlU\Jll ~ ••al. alloy ~ NAS365 ~ I d, coarse ~ '--9 tube twotype assy., threaded 1t type 1 & 11 terminal s Clevis-engine controlriveted, swaged phillips recessed ethru , ~-~\ends rod, steel type 1 terminals ~~~~~e~n: l-W-12 tubeassy. ___ ------~~'R"''''] tube assembly, C.bl, A"ombly, internalthru S302 thru NAS310 ~1 wrenching, S220 NAS237 S183-184 NAS 179
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22 Aircraft Technical Book Company
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NAS366 Control Rod & tu b e assy. " welded. 2 threaded
NAS397-398 ~""\
•\'~ •
\.> Clamp-ratchet, one & three piece
\J)mB
\,~. ends
.:n.~""\
NAS424
NAS36 7 Control Rod & welded, \ 1 thre~ded tub, & clevi send \-
•
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N AS4 27
NAS377
Pulley-flight
Coupling - tube steel, al. alloy
_~
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Pin-pulley guard, steel, al. alloy
control
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NAS428
NAS384-385
~~~®
Screw-oval head, phillips recessed 100°, 82°, steel
Bolt-adjusting, crowned hex. hd.
NAS387-388
NAS434-435
Screw-ma h' ~~ 1000 , 820c. steel me, oval hd .,
Clamp-loop type, sheet metal nu t
\:!/
NAS390-39I
NAS436-437
Washer, finishing
Clamp-harness, wire bundle
NAS395-396
NAS442
Nut - U type
Latch-flush
type
23
Aircraft Technical Book Company
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L11
offset Nut-self-lock ing, 450 446 447-448 451 444-445 49 sleeve, steel button plate, ~ lat typetype plain anchor nut, anchor
O
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NAS443u
~~
~~ ~ ~ Bolt-shear, ~
Nut, instrument Ring-locking ~Shim-
Washer-tab close head flat type head NAS456-457 moun t&tolerance NAS487 Rivet-blind, NAS454-455 Rivnut-lOOo NAS463 csnk. N AS464 NAS452-453 al. alloy
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@
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24 Aircraft Technical Book Company
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NASSI7
NASSOO
Shim-anchor nut, csnk. N ASSO I
•
NASS28
DO
Coli ar-hi-strength hi-shear rivet
Bolt-hex. head, drilled & undrilled NASS08
•
Screw-lOOo flat head, close tol. 160,000 PSI
N ASS32
Guard switch toggle Ri ve t-uni vers al head, monel
three position
N ASS09
N ASS37
Nut-drilled
Bushing-plain, ij press fit, undersize in side di a.
NASSI3
NASS38
ij--mo
Washer-rod end, locking, steel
Bushing, flanged, press fit undersized J.D. N ASS48
NASSI4
~@ Screw-machine, 1000 flat hd., fully threaded, al. steel
Screw-lOOo flat head, type B tapping
N ASSI6
NASS49
Washer-flat, resin fiber
Pi tting-lubricator 118 in. drive, flush type 2S Aircraft Technical Book Company
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©
cod end mmet-split, 552 Screw-machine, 553 554 555 Tee-universal 1000 ~ -uni versal w-uni versal w-universal ~
~® ~O r
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~ ~ NAS55 I ~~ Pin-spring, elec. equipment ~~ ij ~ heavy duty IIIIIIIIIIII mountmg 26 NAS558 Bolt-full thread, ~ N AS557 I Pin, r~ar ~ Key-squilre,
Aircraft Technical Book Company
I
slotted and coiled, NAS559 NAS560 N AS561 NAS563 thru 572 NAS574 NAS573 fully identified head structural, hi-temp Lock-rod end Clamp Assembly, ~
800-780-4115
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0
0
ips recessed, full thr., steel el,connector steel elf-locking, drilled head S608-609 S600 606 S591 S617 S583 thru thru 596 590 u1I.lIillllu~ w-hex. -self locking,~
I
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wrench, NAS577-578~ Bolt-twelve point external lock. (for wire rope) N AS607 Washer-flat,
~@ .~~ ~@
I
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(Q) Fork-turnbuckle, Fork-turn buckle reduced Hooklocking, short, support, 160,000 0.0. (for bearing) PSIclip clip elec. equip. Screw-pan hd.clamp thr. ~644 NAS645 NAS622 Eye End-turnbuckle, clip locking NAS620 NAS623 NAS624 thru NAS646 ~NAS647 180,000 ID .. PSI
~
27 Aircraft Technical Book Company
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atternal close toleranceti.ti.alloy alloy ad, close p hd., lock (fortolerance pin) AS651 ng-retainer, ing-re tai ner,
AS670
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locking, two small I NAS682-683 I height, F, F Bolt-hex. head, N AS67pattern I5500 NAS680-68 close tolerance, Ilug ti. alloy NAS686 NAS679 NAS673 thru 6788000 locking, self-locking one lug NAS684-685 I Nut-plate, self. N AS648 Nut-plain, ~ hex., ~ lockin~ two IuS. fioatms Nut-plate, corner, Ilow I ~ NAS663 ~ 668Nut-self-locking, NAS 669 thru
I
Nut-plate, self- Nu'•• I'''.
~
I
'elf-IUCkin~
28 Aircraft Technical Book Company
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N AS687
NAS811
Nut-plate ~.self-Iocki~g , one lug
Cap-protective, flarele s s
;'
N AS8 12
NAS688 thru 69S~RP ~ Nut Assembly, self-locking, gang channel
Cap-protective flared
NAS696
NAS813
Nut-plate, self-locking,
Cap-protecti ve, electric conn.
one lug, miniature
NAS697
co
NAS814
~ Nut-plate, self.locking, two lug, miniature
Cap-protective, flared fi tting
NAS698
Nut-plate, comer self-locking, miniature NAS704
~
NAS81S
0
thru 709
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Terminal-stud, turret types, brass
Plug-protective, fl ared
NAS720
N AS816
- - -- --
Screw-pan head, assembled
(------18
Cap or Plug protecti ve
29 Aircraft Technical Book Company
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m 9
CO 00 ~O~b ~V ~
NAS817 ~ self-locking, ~ tings ctricheadconn. x. I Nut-platn. ~~ "IfNut-pI ate, gular & low ht. Nut-plate. Nut-plate, " ASI021-NASI022 AS 1003thru thruNut-plate, 1020 AS818 AS945 947 AS819 right angle, 30 AS820 Nut-platn, CO,"". Nut-plate, self~ self-locking, ug-protecti ve, lf-locking lared p-protective Nut-hex., ap-protective, ug-protective, Cap-protecti nged fi tting ve,
Aircraft Technical Book Company
9
NASI029-NAS 1030 self-locking NAS 1033floating floating, self-locking NAS 1027-N NAS 1025-NAS 1026 one one lug, NASI031 lug, two AS lug 1028 NASI032 self-locking, locking, two lug locking, one lug two lug, floating ~~ I NAS1023-NAS1024
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HAS 1047
NASI034 thru I041~ Nut Assembly, ~ self-locking, gang channel
Turnbuckle Assy.
NASI042
Shackle-anchor, round pin NASI043
Shackle-chain, screw pin NASI044
Shackle-chain, round pin
Sling Link, welded
NASI045
NASI050
Thimble-he avy wire cable
Grab Hook, direct eye
NAS 1046
NASI 05 I
(~
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Safety Hook, snap, direct eye
Clip, wire rope
NASI052
SHook
31 Aircraft Technical Book Company
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a
~ @ © €J6 ~
NASI053 ulder nut 1000 flush head uding head o Hr.i,,~nvE ~~ e[:FOPE SI061 Set Screw-hex. NASI054 I055 I056-1057 acer lock-spring flat hd., ~ ~Bolt-l00o Washer-hi-temp. I Sue om••• et-hi-shear ,
10
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1IIIIIIII
warning
~@ ICollar-lockbolt NASI090 NASI089 NASI083 socket, self-lock. NAS 1080 titanium alloy 1081
FLIGHT
NAS 1067
Hook-chain S NASI091
N.t-plate. ,elf-loeki ••• ~ one lug, miniature
Streamer-assembly
NAS 1068
Nut-plate, floating, self- locking, two lug, miniature 32 Aircraft Technical Book Company
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hd. fulI thr. 120 fulI thr. torq.-set thread, torq.-set full thread hss, shear head, al. alloy SIIOI SII02 S 1100 1098 S I1099 097 IUWIIIIIlIIlIllUt] lum~~~ .IUIIUIW{]
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Screw-machine,
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33
Aircraft Technical Book Company
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-flatDevice fill hd., ng universal head hread, self-locking =:J hread, self-locking ock., g, fulltorq.-set thread 1193 miniature o m8J)
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34 Aircraft Technical Book Company
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HAS1211-1213
HAS 1222
Fitting-tie down, strap end; strap
Insert, helical
HASI216
coil
HAS 1223 thru 1235
III~UI~llIilJl1I~ijD ([)
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Bolt-self locking, hex. head 2500 F
HAS 1217
HAS 1236
Screw-pan hd. hi-torque, short thr.
DCID
Bolt-universal, tube-end, f1areless
HASI218
HAS 1237
Screw-pan hd. hi-torque, short thr.
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HAS 1219 HAS 1238
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35 Aircraft Technical Book Company
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q .I~ q @II
sss Rivet-solid flush head el O.S. hi-torque 251 1241 242 Bolt, her-flat
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Type 8
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36 Aircraft Technical Book Company
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"roar 0 0 i 9 --- --~@
head g,lushlow hei ght ar pinthru 1296Screw-shoulder, Bolt-shoulder, 1297 1292 291 1299 1298 b Screw, flat head -shoulder,
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recess
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37 Aircraft Technical Book Company
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NAS 1353 thru
NASI397
1366
Pin-quick release, positive locking, double acting
Clamp-loop, nylon
NAS 1368
NAS 1398
Grommet-fli p-type, plastic
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NAS 1394
NAS 1407
Insert-threaded, metal. It. wght. reg. & self-locking
1406
Pin-spring, coiled
NASI395
NAS 1408-1409
Insertthreaded metal,
Nut-hexagonal,
heavy duty, regular & self-locking
self-locking, regular hei ght, coarse & fine thr. 38
Aircraft Technical Book Company
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q
ng all.head, steel pull aded ng head, steel type, steel r- 1436 head,thru pull 1442 type,Pin-swage steel SI454 SI423 S 1414 thru ~1422 swage lock, pro~~hex., plain, thin kbolt-shear 1000
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pull type, steel 1456 thru 1462 NAS 1474 Pin-swage truding NASI473 head, lock, pull protype,rivet steelspacing NAS cap 1464 reduced 1000 head, NASI475 thru 1482 two floating, lug, head, pull type, steel ~NAS
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39 Aircraft Technical Book Company
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+~
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ll type, al. type, alloy steel ead, stump ut-plate, Knobs-hand ad, AS 1503 1496 thru 1532 1510 1502 ASI525thru ASI516 ASI515 1522 Pin-swage oy ad, stump type, IIIIIUIIIIIIIsteel Washer, ~ n-swage lock, pron-swage n, swage lock, lock, protru~ 1000 ~
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flush hd., 1200 F tension, stump type, alum. head, tension, stump type, alum. Screw-pan thread,I1556 1200 hd., full 1579 thru 1562 Bolt-shear panF NASI578 NASI546 NASI553 1552 NASI535thru 1542 NAS 580 tension, pull type, alum
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lock, 1000 hd~
lock, protrud~
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40 Aircraft Technical Book Company
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rivet, 1200 head, 1200 int, external hr., 1200 F FFwrenching 1587 1585 82 er-1200 -l,200oF, F,
1586
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shear Washer-sea)ing rivet, 1200 ~ F NASI584 NAS 1583
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preformed .0312 O.S. Bol t-shear hex. 1628 NAS1611-1612 head, 1200 torq-set Fhead, 1598 NASI630 1634 1620 short thr., NAS 1603 1610 Screw-flush Screw-machine, 1000 flat preformed NASI588 NAS 1593 thru thru 1596hd., Screw-machine, pan.
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Pack ing-O Packing ri ng, 0~ ring, I N AS 158 1-(Q) IJ® IJ@ ~(3)
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41
Aircraft Technical Book Company
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NASI63S
NASI711
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Strap-retaining, ~ cushioned, rectangular
NAS 1636
N AS 1712 Washer-key dual tab
NAS 1640 Washer-lock, non-magnetic
o
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NAS 1713
Clamp-loop,
NAS 1669 thru 1674 Fastener-blind,
cushioned,
into threaded ext. sleeve,
center mounting
NAS 1714
Clamp-loop, protruding & flush hd., self-locking
cushioned. elongated
NAS 1677
NASI71S Clamp-loop, cushioned
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two piece 1710 Clamp Assembly,
~
cushioned, saddle
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NASI716
V
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42 Aircraft Technical Book Company
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q
uding head, ti-alloybulbed ti-alloy head, ti-alloy ti-alloy locked spindle, 2306 906 thru 1916 2206 2210 806 1816 2105 2112 2005 thru 2310 2012 d. hd., ti-alloy ~ -hi-shear, (1I111I1111j1111~ (j11l111111111i1~ -hi-shear, , blind, @:n!~
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43 Aircraft Technical Book Company
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n
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NAS4703 thru 4716 NAS3103 thru 3110 s, long cres thru 3305 recess, cres. stl. long thr., st!. ,recess, short thr., alloytitanium stl. long alloy thr. reces s, short thr., alloy ti tani urn 4304 thru thru 4316 4204 4216 4400 4416 4104 4116 3203 BoltBolt-lOOo Bolt-WOo 3210 1000 head, reduced, tri-wing tri-wing Bol t-V strap type Ilt!IU hook iamuIu ,1)( iI1hI ~ V type
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44 Aircraft Technical Book Company
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NAS5200 thru 5206
s, thr., cres. s.s, s. thr •• •• titanium alloy full thr., alloy stl. short thr titanium s, full fullthru thr., titanium ing 5400 5406 5700 5706 5500 thru 5806 5506 800 5600 5606 5300 5306 wing thru -wing ng .UIUIIIIIII(] IBlgIBJI~Ub~ II1muunw~\'(]
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NAS6100 6103 NAS5900 5903 NAS6203 6220 Bol NAS6403 NAS6500 t-hex, recess, head, thru thru 6506 short tri-wing Screw-lOOo oval6420 hd., full thr., u 1I1Il\~1\111~@ ~@ a.1~lJIIlhll~@ .ml~uw~ @
thread, titanium Screw-hex. head, tri-wing Bolt-hex.cres. head, short recess, NAS600 full thru thr., 6003 alloy stl, cres. Screw-hex. recess, full head, thr., titanium tri-wing alloy steel tri-wing recess. NAS6303 full thru thr., 6320 cres. thread,
U ~@ @
45 Aircraft Technical Book Company
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NAS6604 thru 6620
recess, full thr., thread, cres. titanium alloy steelcres. head, tri-wing NAS6804 6820 NAS6704 thru 6904 NAS6900 6720 Bolt-hex. Bolt-hexScrew-pan head, Bol~hex. head, long long ~
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46 Aircraft Technical Book Company
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MS 9039 MS9033 35188thru thruMS MS 35203 Brass, Alum., CRES; Plain, Cadmium Steel, or Pan Head Machine Screw, Cross Recess: Flat Head Machine Screw, Slotted: Steel, Brass, Alum., Slotted: CRES: Plain, • Passivated __ 1 MS 35459 thru MS 35461 ICA __ I 12 Point Bolt Steel Anodized or MS 9157 thru MS 9163 125,000 psi ~Min. T.S.CRES: Zinc Brass, Plated; Alum., Phosphate, CRES: Plain,Black Cadmium Oxide, orHead Steel, or Zinc Brass, Plated; Alum., Plain, Black Cadmium Oxide, Fillister Machine Screw, Drilled, (@) __Phosphate, Pan Head Machine Screw, Slotted: Steel, __ MS 9088 thru MS 9094 and20073 MS 35262 MS thru MS 20074
~
Aircraft Technical Book Company
MS 35455 thru MS 35458 and CRES, Phosphate uncoated, Treated Cadmium or Passivated, or Zinc Plated: etc. Black Socket Oxide, Head Anodized Cap Screws, or Passivated Alloy Steel and Cadmium or Zinz Plated: Phosphate, Anodized or Passivated Zinc Plated: Phosphate, Black Oxide, MS 35263 35221 thru MS 35236 MS thru MS 35278 MS 35237 thru MS 35251
800-780-4115
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MS90 17
MS3367
Strap-cable, adjustable,
~1I11I1I11111~
Bushing Screw, slotted
plastic
MS90 18
MS3368
Strap-cable, ~~ adjustable, plastic,
0
MS9012 Ring, external, Retaining berylium copper MS90 13
Retaining Ring, external, steel MS90 14
Retaining Ring, internal, steel
Insert-18-1.5MM Aviation Spark Plug helical
identificat.
MS9020
Paoking-p"fonned,
0 0
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ring- Fitting
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MS9016
MS9033
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0~ 0~
Boss Gaskets
MS9021
o
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@
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Bolt-machine 12 pt head, 130,000 PSI Min. T.S.
48 Aircraft Technical Book Company
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t. washer head,plate drilled olt-machine, eel, hex. aring cadmium retainingdouble S9081 S9068 S9058 IJI~ S9048 acking-O ring
hing, back-up
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MS9101
thrU910d
49 Aircraft Technical Book Company
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MS9 136
MS9157 thru 9163 Bolt-steel,
12 pt. 11II~~1r
Gasket, type XII, XIV A & B, XVII A & B
hd., black oxide 125,000 PSI Min T.S.
MS9137
MS9164
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Gasket, type XIII
Pin-straight, steel, headless, oversize MS9165 thru 9168
MS9138 Gasket type XIV C & D
Bracket-90o
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angle,
AMS 6350
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MS9169 thru 9175 Bolt-steel,
12 pt.
•
Gasket, type XVI, XVII C, D, E, F
drilled hd. black oxide 125.000 PSI Min. T.S.
MS9141-9142
MS9176
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o ring, creSt
Plug- expansion, tapered
MS9144
MS9177-9178
Gasket type XX
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head, creSt
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MS9146 thru 9152 Bolt-steel,
MS9183 thru 9186
12 pt.
head, cad. plate 125,000 PSI Min T.S.
•
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Screw-machine, steel, drilled 12 pt. hd., cad. plate
50 Aircraft Technical Book Company
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• []
AMS 5504 Bracket-90o angle, x.hd.,head, cres. fused nickel cad. plate, drilled black oxide ad, diffused nickel cad. plate S9189 thru thru 9199 9192 S9197 rew-dbl. hex. ut-plain, hex., S9202 thru 9205 steel, 12
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£".I.s
. , bearing ret. cres. heat resistant Wire-steel, heat &18000 corrosiF on cres. AMS 7211 resi stant, safety 5510 MS9276 1800 lockring MS9224 MS9228 thru 9231 Bolt-12 pt. head, MS9274 rubber, 7272 MS9226 Washer-key, cres. AMS MS924 I AMS MS9245 Pin-cotter,
~
51 Aircraft Technical Book Company
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-
AMS slotted hex.black head7233 AMS 6322 oxide univ. flush 5646 hd., AMS Rivet-solid MS9303 9312 MS9314-9315 MS9292 thru 9302 MS9313 Cap-assembly, Cap-tube, [ MS9316-9317 Stud~~ hd.,~ e,Screw-machine, screw-machine,~ drilled hd.,C
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MS928 1 thru 9291 Nut-cas tell ated Nut-plain hex., wrenching, drilled & undrilled. MS93 18 Clamp-loop type,
Pack;ng-o dng,
A-2866350 head, AMS AMS &7233 5510 rubber, AMS 7272 cushioned, cres. MS9358-9359 MS93 MS9320-9321 MS9356-9357 19 MS9355 hex., A-286 MS9349 thru 9352& aluminum r aluminum Clamp-loop Washer-flat, type, T
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~
52 Aircraft Technical Book Company
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MS9360 Packmg-
Nut-plain hex. drilled, A-286
preformed MS93~5 thru o ring & seal
MS936 1-9362
93880
MS9389
Nut-plain hex. check, A-286
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MS9363-9364
MS9390
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AMS 5510 multo tube, ~~ detachable cushion
MS9371 thru 9376
MS9392
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MS9394 Strap-ret., multo tube, AMS 5510 detachable cushion,
Coupling tube brazing, AMS 5646
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53 Aircraft Technical Book Company
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ap, AMS 5510 ew-mach., steel S 6322, x. hd., thru 1 hol9402 e S9397 S9403 S9438-9439 vet-solid,thru universal ug-mach. thread S9405 ug-mach. thread S9432 9437 9404
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AMS 6304 AMS 6304 ~o MS9395 \IIIIII4UjI ~ 01 Washer-flat, Ferrule-brazing steel Ball-bearing AMS 6304 Pin-s traigh t, CSK. diffused nickle CAD, Rivet-solid 1000 AMS 5735 ~chamfered chamfered CAD pl. Bolt-mach. steel, Bolt-mach. steel,
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tube AMS fi tting, AMS 5646 AMS or AMS AMS7235 6485 hd. 5735 flush 6437 head, AMS 7445 MS946 MS9482 I nickel MS9483 MS9449 thru 9459 MS9460 Hex. hd., 3 holes MS9440 9448 diffused CAD, MS9462 thru 9468 diffused nickle CAD, hex. head
54 Aircraft Technical Book Company
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322 CAD3-tube, hex. multiple 2-tube, AMS 3839 ull shank, AMShead 5731 multiple AMS 3839 ex. hd., 15132 hole, full shank ock, AMS AMS MS9486 MS9498 thru 9508 MS9516 thru 9526 MS9515 ~ ~ Ring back-up ~ 0
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AMS 5510 , WWIIII •• Bolt-mach Bolt-mach., steel AMS wash. hd. drilled PD shank Bolt-mach., db!. hex ext. AMS 5731 silver plated MS9563 PD 9571 shank, AMS connection, MS9527 CRES. 9537 Washer-flat, Bracket-flat, AMS 6350 MS9549 MS9554 9562 Bolt-mach., wash. MS9572 hd. drilled, dbl. 9580 hex. AMS ext. 5731 5731 CAD MS955 MS9553 pl.hd., 1-9552 &thru CRES AMS 5510 MS9484 0Nut-hex, boss 0) dbl. hex. ext. . (0 6322 CAD 1 hole hex. hd. ."'hIUl mallt' IIIWUUIIII MS9487 MS9514 thru 9497
~
55 Aircraft Technical Book Company
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•• h«.key,
d ~O (fu ~@
WasherAMS dbl. 5510 hex. ext. MS9680 thru 9683 cup, lock CRES MS9684 IIIIIIIIIIIII H~II~II Bolt-mach. hd., cupwasher locked, AMS MS9694 6304 diffused 9702 CAD wash. hd., AMS 5708 CRES MS9685 AMS thru 5731 9693 Bolt-~QlI~1II mach., full shank, titanium AMS 4967 MS9649 9652 ext. wash. Bol t-mach., MS964 IPD 9648 steel AMS 6322 CAD Bolt-mach., hex. 9679 hd.nickle dbl. hex. 1MS9676 hole, shank, steel ~liI~ hd., cupwasher locked, MS958 I titanium IIIQ\QIIlU AMS 4967 full shank hex hd. 1 hole, dbl. hex. Bolt-mach., Bolt-mach., IIllIIWIII MS9622 thru ~~ 9630
IIJ~ ~@ (liI@ ~~ DO 111111111111
x. hd. hole, D shank, tititanium tanium AMS 4967 hd. 61&holes MS 5510 AMS 6350 CAD pI. ext. wash. llx. 9603 AMS 5731 00 locking 9599 l CRES. shank, AMS 4967 hex. hd. RES S9600 S9583 thru thru 9591 S9582 S9592 acket,AMS 9005504 angle, S9631 thru 9639 olt-mach., @}1I.\w/u~. ol t-m ach., asher-key, crew-mach.,
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@
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56 Aircraft Technical Book Company
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wash. hd.,AMS drilled, AMS 6322 5708 CAD itanium 4967 AMS 5737 CRES & AMS MS9748 9756 MS9757 thru 9765 MS9766-MS97 67 MS9739 9747 MS9712 thru 9720 MS9730 thru 9738 Bol t-mach. Bolt-mach. Bolt-mach •• Bolt-mach • Bolt-mach., Bolt-mach., Nut-dbl. bl. hex. hex. ext.
• S0@
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Bolt-hex. hd., macho 5525 &full 5737 CSK CRES AMS Bolt-mach., 3650. seal hex. hd. 1 5643 AMS 3650, O-ring full shank, AMS 5643 AMS 3617, Seal MS977 I AMS MS9768 MS9770 MS9781 9791 MS9792 MS9772 thru 9802 MS9773 hole. shank, AMS AMS 3617, O-ring
MS9703 thruAMS 9711 l)1@) drilled. PD wash. AMS 5643 hd. PD shank, CRES ~ drilled, AMS titanium AMS 4967 shank, CRES 5643 wash. hd. PD shank. drilled. 5708 SILVER PLATE
paCk;og-p
57 Aircraft Technical Book Company
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-- V
mfered CRES, AMS 5640 agement, steel AMS drilled , full shank, 5643 agement steel
ole, 1PD shank, ded, AMS 5616 984 9834 thru 9840 9842 9848 AMS 5643 9827 9833
ma~
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AMS 5646 CRES AMS 5510 Nut-plain, hex., brazing, AMS 5646 ext. hd., AMS 5616 MS988 1AMS MS9879 MS9882 Bolt-mach., dbl. drilled, 6322, CAD MS9880 wash. Bolt-mach., MS9901 hd., AMS dbl. 5616 hex. drilled ext.plate 6322,wash. CAD plate MS9892 thru 9900 MS9883 thru 9891
Nut-plain, hox., AMS@
58 Aircraft Technical Book Company
800-780-4115
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0@
h, hd., hd., sh. hd full shank. steel spanner-end h. drilled, full steel shank steel hdl,•• PD PD shank, shank, AMS 7279 O-ring lt-mach, g-macho thrd. t-mach., t-mach., -spanner •• nut, CRES AMS lt-mach 1)1 5646 9912 thru 9920
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drilled, AMS 4121 AMS 7273, AMS 7273, seal 3668, sesurface al MS9956 (hydraulic) MS9967 MS9954 MS9970 MS9955 MS9966 AMS 3668, 0O-ring ring Plug-mach. thrd. Fittings-lubricat. ~check MS9902 1)1@ (lJI@ 6322 CAD drilled CAD AMS slots, 6322 cupwasher locked. AMS 6322 ~ MS9921 thru 9929 p,e!.nned MS9930 MS995 Packi."p,e!.,med 9938 MS9939 thru 9946 MS9952I thru MSI5001 thru ~ Packi••• Pack;•••••,.!.'med Packi•••••'e!.nned
~ 15006 Packin•.••,.!.'med
~~ ~
59 Aircraft Technical Book Company
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I:
i ~it
stenitic corr. res. steel silicone ivet-tubular, ut-plain, hex. 1000 ivet-tubular, check Washer-fiat, «tnn"~\ -1"""""\11
ad, copper SI6198 S S 16199 15795
MS 16536 S 16535 hting,-Iubdcat.
0
10
0 @
, I 'fd @ 11 0
exterior, inverted Ring-retaining, MS 16203 Ring-retaining, ~
Ring-retaining, ~~ 15721 MS 15720 thru Ring ~~ retaining, .001 over normal size
"
exterior, basic nominal size Pin-straight, headless interior, inverted interior, tubular, basic Pin-spring, 16562 MS 16627 16555slotted MS headless MS 16556 16624 .0002 over MSI6625 MS 16626 Pin-s traigh t,
60 Aircraft Technical Book Company
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MS 16628
Ring-retaining, exterior, bowed MS 16629
Ring-retaining, interior, bowed
MS 16630
Ring-retaining, exterior, beveled
MS 16631
Ring-retaining, interior beveled
o o o o
MS 16842
@
Clamp-wi" ,opa. saddled single grip, steel MS 16995
~(Q)
Screw-cap, socket head hex., corr. resisting steel UNC-3A MS 16996
-==-1 (Q) Screw-cap, socket head, hex., corr. resisting steel UNF-3A MS 16997
~(Q) Screw-cap, socket head, hex., alloy steel CAD UNC-3A
MS 16632
MS 16998
Ring-retaining, exterior, cresent
Screw-cap, socket head, hex., alloy steel, CAD UNF-3A
MS 16633
MS 17160
~(Q)
Clip-spring tens.
MS 16634
MS 17413
Ring-retaining, ext. bowed ICE"
:aJ. ..
Ring-re taining, exterior "E"
Packm rubber ••• o-nng ~aronnad
..
0~ I
61 Aircraft Technical Book Company
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@~ --@ r.-~
tle, regular hex. regular & thin 00, regular monel 0° hI.ht.,CRES steel,
t-self-locking, -t-self-locking, 17821 ap-cable,
.-
steel
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17828 17825-/7826 17984 thru 17990 17822 17829-17830
)
,.,s-bearing Screw, --- "-Ball . Set MSI7811 ...
cup-fIa t-cone p ts., positive lock ~ Strap.cable, ~
~
~ ~:-<~
,...
~
self-locking, CJllllilll1dllllllllllli IIJ:.III-I for MS27212 18035 pan identificat. plastic MS MSI8212 18034 18029 Screw-machine, fiat steel &plastic-nylon stainless Cover-assembly MSI8211 head, adjustable, plastic Strap-cable, MS 18063 19059 thru 18068 19064 head, plastic-nylon
~§ 8U!{58
62 Aircraft Technical Book Company
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square 0033 thru 9069-19070 0004 thru 20046 20024 0002 her-key, ~ er-plain,round, 0001 plain, r-bearing 9067-19068 hi-strength e-extruded secondary
00®
~Or:r
Key-machine, 10 ~ I ~r_~ MSKSI 19065 Pin-hinge 160 &Fcoarse drilled hd., fine hex. head, 12000 Shackle-wire ~~ thr. Pulley-groove, Pulley-groove, Pulluy...,«" flight
I\\i=Ccontrol @ aircraft
- lA' O@ ~
MS20253 MS2022 1 thrucontrol, MS20073-20074 MS20065 20068 aircraft heavy duty, MS20115 MS20220 MS20219 rope Bolt-machine, aircraft, control, aircraft
63 Aircraft Technical Book Company
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MS20426
Hinge-continuous MS20257
Rivet-solid, csk 1000, al. alloy
~ ~~
MS20427
MS20270-2027I
q~
Joint-univer ~ light & h eavysal,duty plain ,~
Rivet-solid steel , as monel ' csk,, copper 100°
MS2034I
\:!!:P
MS20470
Nut-el ectrical, plain, hex.
Rivet-solid, universal head, al. alloy MS20500
MS20364
Flexloc Nut, selflocking, 1200° F
Nut, self-locking, 250° F, thin
MS2050 I Nut-plate, selflocking, two lug
MS20365 MS20600 Nut-s° el f-Iocking, 250 F, regular
UI
n
D-"·""""·"~·
Rivet-blind, pull stem, protruding head MS20392
MS2060 I
Pin-straight, headed, drilled
Rivet-blind, pull stem, 100°, flush head
0'
II
I}."
.
64 Aircraft Technical Book Company
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,al uninsulated I' flush head and 1000 sal hd., fork univ. end Sleeve-flared ive End-swaging, nd 604-20605 shank :::(] ", . . ,",un. Double shank T erminal-s wagin g, 664 solid. monel &( pipe thread 900 End-swaging,
cQ C=D
0(W cj) /?
Elbow-flared tube ~ air 11 MS208 Elbow-pipe to-- .,--=-~ tube 45019 valve swaging, TerminalTerminalMS20667 eye end swaging, III IJnI MS20602-20603 ~ Cap, high-pres sure steel, ss, brass, copper MS20823 tube fitting q"""""",un", MS20668 MS208 13 ~ MS20822
.~
MS20663
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..
-:::-
~~
65 Aircraft Technical Book Company
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MS20825
Tee-pipe
MS21047-21048
Nut-self-locking plate, two lug, low ht.
to tube
MS20826
Tee-pipe
MS21049-21 050
Nut-self-locking plate, two lug, 1000 csk, low ht.
to tube
MS21025
MS21051-21052
Nut-cas tellated bearing retaining
Nut-self-locking, plate, one lug, low ht.
MS21040 Nut-self-Iockin light weight
MS21053-21054 g, Nut-self-locking, plate, one lug, 1000 csk
MS21042-21043
MS21055-21 056
Nut-self-locking, reduced ht., ring base
Nut-self-locking, plate, corner, low ht.
MS21044
Nut-,elf-loc"'n., hex©
MS21057-21058
~
Nut-'elf-luc"'n.,
regular ht, nylon insert
plate,
MS21045-21 046
MS21059-21060
NUHe!f-toc"'n.,hex@ reg. ht., all metal
W
~
corner, 1000 csk.
Nut-self-locking, ~~ plate, two lug, floating, low ht.
66 Aircraft Technical Book Company
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~
reduced rivet spacing dtwo rivet spacing insert ug, e two lug, lug. nylon nylon insert plate, lf-locking, plate, 077 insert 071-21072 073-21 074 hex., nylon e lf-locking, plate, ,, rw\...::..., f-locking, plate,
-"lf-!ouk'n., p,at,
bcJJ ©~ ~@
Gang ~~ Channel, ~ MS21061-21062 . Nut-self-locking Nut-self-locking, reduced rivet spacing, one lug,corner, nylon insert insert ~ plate, plate, nylon MS21078rivet spacing, reduced MS2107S-21076 MS21069-21 070
floating, low ht. s reces Gang Channel MS21080 MS21081 plate,spacing, MS21079 Nut-self-locking, MS21083 MS21090 MS2108621087 pan head, cros sed Screw-self-lock, low ht., reduced MS2 1088-2 1089 corner, nylon ins.rivet
~
~ ~
67 Aircraft Technical Book Company
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@
-
flat hd., steel, recessed CRES steel head ush & Protrud. hd. A-28655 head, cross 208 er, 1096-21097 098-21099 1140-21141 207 1094-21095
helical
.
--
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MS21254 ~ 11111.' MS21091~Cthru 21093
~@ :;: a@ ~@
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I I
turnbuckle, CRES steelrope Turn buckle Body, Eye End-turnbuckle, clip locking ext. MS21251 wrenching MS21252 Clevis turnbuckle, MS21250 MS21256 End, Bolt-12 pt.,forclip MS21255 clip locking, for locking pin MS21253 Clevi sEnd-turnbuckle, clip lock, bearing clip locking, for wire Eye End-turnbuckle, Clip-locking,
(§)
IIIIII!IIII H6U+IIII
COil-
68 Aircraft Technical Book Company
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•
fastener, stud-clip ing stud washerIJlock Terminal-wire ext. head 259
261 260 262
Woodruff, er-key, ~ 277 thru 21285
3i~ ~@
MS21266
~
0-I
CI'mo-loop
IICI]@
PII?
I
II clinch Stud-snap slide ..thru " ! I h & tubingII MS21286 MS21318 21294 Screw-self-lock, Screw-drive, round MS21322-21323 MS21295 into wrenching MS21324 MS21331 thru 21326 for pipe, conduit cable Screw-machine, dbl. hex.Style 3 ~
I.
11& cushioned Strap-retaInIng, two aNut-plain, e, MS21258 2.~ drilled ext. U washer head into wrenching head, Type ~ ~'-t~
I~~
MS21314-21315A
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MS21332
Fastener
MS21903
snapslide Union-flareless tube, 3~ bulkhead & universal
01
MS21904
~ ~
,
Clamp-loop, MS21333-21334/?
plain & cushioned
ss
MS2190S
MS21340
Nut-plain, electrical,
Elbow-flarele tube 900
0
Tee-flareles tube
hex. thin, wire holes
MS21342
s
MS21906
Set Screw-fluted ~ socket, cup and flat point
Cross-flareless tube
©
MS21900
MS21907
Adapter-flarele ss to AN flared tube
Elbow-bulkhead universal 450 flareless
MS21901
MS21908
01
Adapter-universal to AN flared tube Adapterfl areles s tube for 3"g bulkhead
Elbow-bulkhe ad universal 900 flareless
MS21902
MS21909
Union-flareless tube
tube
Tee-bulkhead & universal, flareless
tube
tube
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, MS21910
MS21917
I
Nut-sleeve coupling, flareless flarele s s tub~ , lOt. . thrd
~Tee-bulkhead MS21911
.
~ . on side
MS21919 "
I flareless
tub' e, mt. . thrd - .
~Tee-bulkhead MS21912
T
~
CI.mp-cu.hionod, support,
..
~.~:.""
'~
'Q
--::::..:.Ie -
loop type, aircraft
MS2 1920
. on run
Clamp-hose Tee-flarele -~ bulkhead onssrun tube, with"
-W- -.
MS21913
MS21921
Plug-flareless tube
Nut-sleeve coupling, flareless
MS21914
Cap-pressure seal, flareless tube fitting
o
MS21922
I Sleeve-coupl flareless
ing,
MS2191S
MS21923
Bushing-screw thrd. expander, flareles s tube connection
bulkhead universal
MS21916
MS21924
Reduce-ex tern al thread, flareless tube
Union-Oareless tube, bulkhead and universal
Adapter-flarele
ss tube,
and to flared tube
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pan 820 Oat head, ey-control, eless low &profile & 820tube, fIat head ow-900 univ., ow-900 univ. 210 24587 246 15-24618 thread cutting 24566 24585 21926 w-tapping, ng-helical, pter-tube ng-helical, ~~
[OJ (Dr) ,,®
MS24679-24680 =--~~ cross recessed Type A ~high Screw-tapping, Type & low 'u Pin-cotter Type FB ~ MS21925 Screw-tapping, ~crown anti-friction Screw-tapping, hd hd., •• flat, fIat, drilled csk.
G@
MS24586
c;)
a~
MS246 19-24622 MS24627 -24630 MS24623-24630 pan & 820 820 flat head, MS24665 pan & flat head & 24671 Nut-plain cap, MS24667 MS24673 thru 24678 Screw-cap socket phillips recessed, Screw-cap socket cross recessed Type BFor BT
B::I © IT® ,,@ Tfc±)
72 Aircraft Technical Book Company
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MS24690
4692
C 0
MS25083 MS25\7\
electric, bonding
Jumper-assembly, ~
Pin-tapered plain
»
d
Nipple-electrical
MS24693
MS25226
~@
Screw-machine, flat csk. Head, 1000 cros s reces s
Link-terminal connecting
MS24694
MS25227
(]@
(0
Strip-mounting, nut insulating
MS25036
MS2528\
~.
07
Lo
Screw-machine, csk fiat hd., 1000 cross recess, structural
#
Tenninal-Iug, crimp style, insulated
Clamp-loop, plastic, wire-support
MS2508\
MS27039
Washer-key
@
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GiU\\\\1()
Screw-machine, pan hd., structural, cross recessed
MS25082
MS27040
Nut-plain, thin, hex., electrical
Nut-plain square
@
@]O
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ntersunk open Washer-fini shing, end IIclosed vi s-rod& end, round ~~ sher-fini -plain, shing, ut-stamped 27130-27131 27151 Washer-slotted 27129 27111
I
I CS @ (@ © DB
plain, ~round MS27051 MS28740 Fitting End,'" Clamp-loop Nut-spanner, turnbuckle Hose Assembly ~ I Clevi Terminal-board, MS27 128~s-rod-end, I Washer-flat, ~ ~ 74 ~~~~ ~ MS27120
---1
~
Aircraft Technical Book Company
@
MS27405 I MS27183 MS272 12 MS27955 assembly MS27975-27976 hydraulic I adjusting MS28741
~~~
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MS28889
MS28772
0~ O~ 0 O~
Valve-air, high pressure
DPa~king.p"'o
0
820 flat hd.
ng up, teflon 8782-28783 8778 chain 8777
Retainer, packing backup
~
MS28932
Felt Strip, packing
I MS35206-35219 MS28775 O~ Screw-machine ~ recessed, MS28776 Packing-O-ring 75cross Hook-filler cap Screw-machine,
,h".hydmnlic, ~~ p".pi"on md~ Cking_p,,'n
Aircraft Technical Book Company
~®
~@
~
~~
MS29523 MS2956I O-ring MS35 190-35203 MS295 12-295 13brass, steel, brass, alum. recessed, steel, pan head, cross
aluminum
Packln g-preformed,
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,lled d. SS steel, 35337-35340 5265-25278 5333-35334 her-lock, her-lock, flat
8
Gromme t-rubber Screw-machin brass. alum. e, internal
@}
@©;
· . ·· ,, ~ t MS35223-35234 hd., slotted, steel Nut-slotted headless, tapered groove Nut-plain hex. hex. Nut-plain ~~ hex. flat MS35239-35243 Screw-wood,
\.~.- .....•.•
Screw-wood, flat head, & roundcross hd., recessed slotted MS35489-35490 MS35494-35495 MS35692 MS35690-35691 MS35492-35493 MS35671-356 79 MS35649-35650 Pin-grooved, \l:t7~ (Q) ~'0" CW\UU~c:8 ~
~~ MS35335-35336 MS35425-35426
@
@
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# 0
hex. socket
er & asbestos clevis, sher-lock, 1000
35842 35769 35914 358 10 Pin-spring, 35821-35831 5790 mp-hose, rt-screw,
ge-cnnlinnnua ket-metalic
MS35756 SS & steel
10
-. B@ ~(t) -@ ~(±) @ ~(f)
1\0 ~ Screw-machine, pan~ tubular coiled Set Screwpan flat head, hd., cross recessed head, cross recessed ~ cross recessed Pin-spring, ~ ~
~
half-dog, -51958 cone, type flat, AD, cup pt. MS51861 MS39086 MS51862 MS51923 MS51959-51960 MS51017-51047 MS51957 Screw-tapping, Screw-mzchine, Screw-tapping, type AD,
~(f) ~
I
77 Aircraft Technical Book Company
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ijO .fL1h"
cone point tener-blind, hitt,t, Fas head oval po in t 1975 1967-5 1973-5 1972 1974 ij plain, hex.&11BICJIJ crew, hex.
~© @ ~©
0-~ 4A © I@ @
coil-coarse thread 12 point MS90064 MS90353 MS 122900-122939 pull type, captive protrud washer ing head O-ring MS90415 MS 122026-122075 122076-122275 MS90354 hi-strength, Fastener-blind, Insert-helical MS5 1963-5 QUit 1966 Nut-self-locking, Washer-lock spring socket, half-dog point strength, pull type, 1000~ flush hd. Clamp-loop MS5 1987 1976-5 1917 MS51981-51982 ~ Pack-preformed,
c:::t)
I
~
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SS steelsteel grade retaining bearing retaining single rt-helical bearing
~O
-~
••• @ O( O~ @(
MS 124651-124850 ~ Nut-spanner
Washer-key, ~1, single Nut-spanner, Ball-precision Washer-key, Pin-spring, Ball-grade
MS172321-172370
MS 150451-150500 17220 17140 1-172235 117 1900 MSI7227 1-172320 MS 172236-172270 134351-134400
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AN HARDWARE SPECIFICATIONS
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SOL TS
AN3-20 AN21-36
• On AN9-6 only X : 7/32 4
+"h~+xll~+Jl~+J
LEH~h
,
t-
LENGTH
I
c.
Add ~D" betore dash No. tor al.alloy bolt Plain dash No. denotes steel bolt
~
-1=--------9
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. --------
-..•. -
WADJt FOR S TEEL nAn
MARK FOR CRES MARIt POR At.ALLOY
~
cotterwith pin hole Add "H" betore daeh No. tor bolt Add "A" atter dash No. tor bolt without drilled head and without cotter pin hole Example: AN7-7 : 7/16 dia. steel bolt 31/32 long AN7C7 = dia. steel crestor bolt 31/.32 Add "C" betore dash No. crss boltlong ANB-7A : 7/16 1/2 d1a. bolt 31/32 long, without cotter pin hole
Add "A" atter dash No. tor bolt without cotter pin hole
"""'D"""~
. =ft-
--'$' - ~;:1Tl ~
LENGTH
Example: AN21-111
= 16 steel bolt, 29/32 long with cotter pin hole AN2B-lIiA : 1/2 dia. steel bolt, 591611 long without Dotter pin hole
~
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BOLTS
AN42-49 AN73-81
1/8 •. x 11'A t
xll~ + x Add "A" after dash No. for bolts w1thout cotter p1n hole Example: AN46-5 = 3/8 .teel eye Bolt 45/64 long for 3/8 p1n AN46-5A = 3/8 .teel eye Bolt 45/64 long w1thout cotter p1n hole
-t _~ IDENTI~ICATION
coarse f1ne thread
thread)
r_~~
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TURNBUCKLE
~+
FITTING
AN155 ANI61
+
---=
L
~--'-.--~--
"s"
-
=
~:_--
--
-
"h" ,.'"~o.
denotes 1shong ort barrel barrel after dash NO. denotes
"C"
Example: AN155-Bs AN155-8L
= =
I
Barrel, Barrel,
L
short, #6-40 tnternal thread long, #6-40 tnternal thread
~I
£3-====( ~~ ~~~i~~~LS
=
AN161-22RS AN161-22LL AN161-22RL
=•
Fork,
short -
J~8b.
thread
1/4-28 L.B. R.B. thread thread Fork, short long --1/4-28 = Fork, long - 1/4-28 R.B. thread
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TURNBUCKLE EYES
ANJ65 ANI70
dash Mo. denotes
100&
Example: AN165-22S = short eye 1/4 -28 thread AM165-22L = long eye 1/4 -28 thread
THREAD
~ -2111~2I11i16-2
_
11'-28 L.B. thread AHl70-22RS = short e.,e 11\-28 R.B. thread AJIl70-22LL • 100& e.,e 11\-28 L.B. thread AJI170-22.RL= = short long e7e eye 11\-28 R.B. thread
tAHlJO_22LS
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a
HINGES
I :~":::"
I~
1'+ P ~
I~ '~6 '~
r(TYPE"HY"
l--r WIDTH
If
, :
+
OPEN
1-
(TYPE"UX" HALF HINOELOOP ON R IOHT END FCI\ TYPE "H" HALF HINGE)
HINOE
AN251 AN252 AN253
'J-:~~'" I
HALF HINOE)
I
PIN
";
- EXTRUDED
(AL. ALLOY)
I
~
1 ~50 11 2~O 11.2~0 2.~ Flr.t dash No. denote •• ize of hlnge
$
--
.I
r "':
and hundredth •. Plain dssh No. denote. al. alloy. Add "e" before rtr.t da'h No. for ere. first dash Add "H", "HX", or "HY" before Second denote. length No. for da.h half No. hinge wlthout pin. in inehe. Example: AN251-0-800 = hinge, al. alloy 1-1/16 wide x 8.00 long wlth ere. pin AN251-CO-800 = hlnge, ere., 1-1/16 wide x 8.00 long with ere. pin.
DIM. DASH NO.
:
First dash No. denote •• ize of hinge.
I~
r=:t~~ ~ -tseeond -
B
..l.
Add "A" after fir.t da.h No. for anodized finish first dash No. to obtain Add "H" "HXIt, or "BY" before type "Brl, "HX", or "HY" half hinge without pins Exalllple: dash No. denote. in lnohe.hlnge and anodized, hundredth. AN252-4A625 = Size II typelength "H" eOlllplete 6.25 long AJl252H4A625 = .ize 4 type "H" half hinge anodize 6.25 long AN252H4-625 • tTPe "H" half hinge unanodized 6.25 long AN252HX4A1Q50 = slze 4, type nUX" half hinge, anodized 10.50 long
.J.a2 !!.
Fir.t da.h No. denote •• ize of pin Second dash No. denote. length in inches and hundredths Example: AN253-l-625 = ere. pin .063 dia., 6.25 inches long
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NUTS
AN310
AN315 AN320
AN316
steel nut Pla 1n dash No. denotes dash NO. for al. alloy nut Add "c" before dash No. for cor. Res. STL. nut - Example: AN310-5 = steel nut, 5/16-24 thread Add "D" before AN31OD5 = al. alloy nut, 5/16-24 thread
~
718- 14
7
I
Add "D" before
¥
-~-
-
,
t}
I 8
dash No. for at.
14
12
I 9 alloy
nut
1'8- 2
Pla1n dash No. denotes steel nut ~'"_ Add "R" after dash No. for R .R. thread -Example: AN315-7L = nut, steel 7/16-20, L.R. thread Add "L" after dash al. No. alloy for L.R. threadR .R. thread 18 AN315D7R = nut, 7/16-20,
1-14 16 174-
12
20
16 ---,-N ---:? 4
-L
,
-
$-, F ,
(+
/
-
I
-
-g ~
"L"
after
dash
-Example: AN316-4L = nut, steel, 1/4-28, L.R. thread "R" after dash AN316-4R = nut, steel, 1/4-28 R.R. thread
-Pla Add 1n"D" dash before No. Example: AN320-4 = nut, steel, 1/4-28 thread AN320D4 = nut, al. alloy, 1/4-28 thread
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NUTS
AN335 AN345
AN340 AN350
Plain dash No. denotes steel nut Add "B" before dash No. for brass nut Example: AN335-4 AN335B4
nut, steel, 1/4-20 thread nut, brass, 1/4-20 thread
/14- 28
THREAD
416
ores nut
nut
QhV
2 steel nut, 68-32 thread = brass nut, 68-32 thread
I
87 Aircraft Technical Book Company
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NUTS
-20 ----
1 t>-20 1 6-14 -11 11 NUMBERS - 0 DASH
AN362 AN363
AN364 AN365
AN366 AN367
.~~
!'YL "'~"" ... ~""
'"''
l61U R'I??OOR 1'11'1 101" lU No. 'II:! denotea l611 R'I R 'I? ? ,0AN363. oR-8101 In'O? '\1 I1?O IO'l? lR ?U '>11:! a?o 10" '\11:! IO"? LI:! 1216 LI:j U"O U?O L02'+ 102 20 -1 11:!12 1 I:!l 2 daah -'12 -1:1 -28 -12 6'12 102 2012 6?U 102'1 10'1 aIR 6?U 10'12 20 102 20 102'1 1216 .?U 0 LU1" t>~2 2 1011 1.21.0 12 1011 .:1 18 13 l21 1:1 6'12 !O 2012 I'll OJIO 8 0 6 AN36r; t>
~4
;~
~
~
~
2
820
363
)
Add Add
"a" "C"
before before
dash dash
No. No.
for for
brass self lOCking locking cres self
nut onon ANAN363 nut 362
• •
AN 365 AN363
Add "D" dash No. all01 self locking nut onon AN366 AN364, • AN365 Add "D" before before dash No. for for al. al. alloy plain plate nut AN 367 Add "DY" before dash No. for al. alloy self locking plate nut on AN366 • AN367 Add "F" before dash No. for steel self locking plate nut on AN362, AN366 • AN367 Add "wC" before dash No. for cres self locking plate nut for use b1 welding on AN362, AN366, • AN367 Exam~les: AN362F1032 AN362WCIQ32 AN363B428
• '10-32 steel self lOCking plate nut = '10-32 cres self locking plate nut for • 1/4-28 self locking brass nut
AN363C428 AN364-428 AN364D428 AN365-'I28 AN365D428 AN366-428 AN366DF'I28
= self cres nutthin nut = 1/4-28 steel, locking self locking = 1/11-28 al. alloy self locking thin nut = 1/4-28 steel self locking nut • 1/4-28
al.
alloy self locking nut steel plate nut locking al. alloy plate
= 1/4-28 plain = 1/4-28 self
use
b1
welding
nut
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PINS - COTTER
AN380
r
l
AN380 AN381
PIN - ConER
LENGTH
©={
rUNEVEN
.1
PRONGS OPTIONAL
Plain dash No. denotes low carbon steel Add ·C" before first dash No. for crea Example: AN38OC2-2 • pin 1/16 (2/32) d1&., 1/2-(2/11) long, cres "'N380-2-2 = pin, 1/16 (2/32) dia., 1/2 (2~) long, steel Second dash No. = length in quarters of an inch except -1 • 3/8 in. First dash No. = d1&. in thirty-seconds of an inch
AN381 PIN - COTTER
CCRES)
DU. EXUlplel "'N381-2-10 • pin, 1/16 (2/32) d1&., 5/8 (10/16) inch long, cres Second dash No. = length in sixteentha of an inch Firat daah No. = d1&. in thirt,-aeconda of an inch
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R IVETS
AN426 AN427 AN430
AN43S AN441 AN442
AN4S6 AN470
ALUMINUM ALLOY
I
ALUMINUM ALLOY ALUMINUM ALLOY) (ALUMINUM ALLOY)
{AUjMI
~15161~~
~'
,'"•••.•. I
1100 (A) PLAIN
•'
"
2117T (AD) DIMPLED
•
~
,
5056 (B) RAISED CROSS
-@-' -@-' ,I T
RAISED
2024T (DD) DOUBLE DASH
" .••
2017T (D) RAISED TEAT
Add code before first dash No. for material F1rst dash No. denotes diameter of rivet in thirty-seconds Second dash No. denotes length of rivet in sixteenths Example: AN426A3-12 = 1100 aluminum rivet, 3/32 d1a., 12/16 long AN426B3-12 • _ al. alloy rivet, 3/32 d1a., 12/16 long AN426AD3-12 = 2111-1 a1. alloy rivet, 3/32 d1a., 12/16 long AN426DD3-12 = 2OZ~I al. alloy rivet, 3/32 d1a., 12/16 long AN426D3-12 = 2017-T3 al. alloy rivet, 3/32 d1a., 12/16 long
For NO. Add Add
6 I 8 I 10 I AN427 & AN435: Add "C" before for cad. plate, OZ" before second dash No. for "Un before second dash No. for
12 J 14 second dash zinc plate, unplated.
RAISED TRIANGLE (pCJ\ MONEL ONLY) First dash No. denotes d1a. of rivet in thirty-seconds Second dash No. denotes length of rivet in sixteenths Plain dash No. denotes steel rivet, cad. or zinc plated (AN427 only) Add "M" before first dash No. for ~onel rivet Add "CO before first dash No. for copper rivet Add "P" before first dash No. for cres rivet Example: AN27-2-2 = 1000 csk head steel rivet 2/32 d1a., 2/16 long, plated AN435M2-2 = round head ~onel rivet 2/32 d1a., 2/16 long AN441C2-2 • flat head copper rivet 2/32 d1a., 2/16 long AN441-2-2P • flat head steel rivet, plated, 2/32 d1a., 2/16 long
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SCREWS
-FILLISTER
HEADS-
AN500 AN50!
AN502 AN503
3/8-16
SrzE
616
A
screw, 66-32 thread, 1/2 long screw, 66-32 thread, 1/2 long, screw 66-32
thd, 1/2 long,
5/16-18 516 First dash No. denotes size of screw Second dash No. denotes length in siXteenths Example: AN502-8-10 c steel screw, 68-36 thd, 5/8(10/16) long AN503-8-l0 • steel screw, 68-32 t~d, 5/8(10/16) long
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SCREWS-MACHINE
AN504 AN505 AN506
1/11-20 416
second dash No. tor recessed head Exaaple, "115011-11'"•• 14"'0. carbon steel .lotted head ecr ••• 11/16 long "1I5011c11-4 •• 111·110cree slotted head .cr ••• 11/16 lone
11\-20 1116 First dash No. denotes eue or ecr ••• Second dash No. d.not •• l.nsth in sixteenth. Plain daeh No. d.not •• carbon st •• l "dd ·C· betore tirst dash No. tor ore. (dotted h.ad scr •••• on17 Add "II" b.tor. e.cond dash No. tor r.c •••• d h.ad acrewa
Exaaple, "11506-.-11• 4/16 lons 14-110 carbon .t.al All506c•.•• = 14"'0 cr ••• lotted
.cr ••••• lotted h.ad h.ad .cr ••• 11/16 lGIII
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SCREWS
AN50] AN509
440
-$-
~I---
1/16
Pirst dash No. denotes
- C-- -
size of screw
--+- Add "a" before first No. Add"R" before second dash dash No. for for brass recessed head S~==~~==~-Plain dash No. denotes carbon steel Second dash No. denotes length in sixteenths ~ AN507-448-8 = N4 slotted head carbon steel screw I ~ LENGTH ~ Examples: 1/2 (8/16) long AN507-448RB = #4 recessed head carbon steel screw
~II
1/2 (8/16) long AN507B448-8 slotted head brass screw 1/2 (8/~6) long
NO. SECOND DASH NO. + ,"'2 Pirst dash No. denotes size of -
11= --E3-
__
I~
Add "p" before first dash No. for plateddash bronze Plain No. screw denotes carbon steel
"m
unplated bronze screw
Add before Add "DD" before t1rst dash dash No. No. for for al. OZ" a11O)' screwfirst MARKINO PCR BRONZE Add "R" before second dash No. tor KING pCJ\ STEEL . Example: receued head screw AN509-10-12 = 110 slotted head steel screw 25/32 long AN509PIo-12 • 110 slotted head plated bronze screw 25/32 long AN509Z10-12 • #10 slotted head unplated bronze screw 25/32 long AN509-1OR12 = #10 recessed head steel screw 25/32 long LENGTH
~
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SCREWS-MACHINE
ANSIO ANSIS ANS20
First dash No. denotes size of screw Second dash No. denotes length in sixteenths Plain dash No. denotes carbon steel Add nBII before first dash No. for brass Add "c" before first dash No. for cres Add "DD" before first dash No. for a1. alloy Add "RI1 before second dash No. for recessed head Examples: AN510.4-8 = #4 carbon steel screw, 1/2 18/16\ long, slotted head AN51OB4R8 = #4 brass screw 1/2 18/16 I long, recessed head
-e==-=:- -=!~ARKING
FCR CRES ~ LENGTH~
First dash No. denotes size of screw Second dash No. denotes length in sixteenths Plain dash No. denotes carbon steel Add "B" before first dash No. for brass Add "c" before first dash No. for cres Add "DD" before first dash No. for al. alloy Add ''R'' before second dash No. for recessed head Example: AN515-4-8 = #4 carbon steel screw 1/2 (8/16) long slotted head
~ DASH NO.
~ARKING
-8--~ FOR CRES ~ LENOTH
-j
First dash No. denotes size of screw Second dash No. denotes length in sixteenths Plain dash No. denotes carbon steel Add "B" before first dash No. for brass Add "C" before first dash No. for cres Add "DD" before first dash No. for a1. alloy Add "R" before second dash No. for recessed head Example: AN520-10-8 = #10 carbon steel slotted head screw AN52OCIOR-8 = #10 brass recessed head screw, 1/2 18/16) long
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SCREWS
AN525 AN526
1,1\-28 416 First dash No. denotes size of sorew Second dash No. denotes length in sixteenths plain dash No. denotes steel screw Add "D" before first dash No. for al. allO)" screw Add "R" before second dash No. for reoessed head screw Example: AN525-10-6 a 110-32 slotted head steel sorew. 3IB (6/16) long. 1/32 grip AN525D10-6 110-32 long. slotted al. allO)" screw. 3/8 = 16/16) 1/32head grip' AN525-1CR6 = #10-32 recessed head steel screw. 3/8 (6/161 long. 1/32 grip
COARSE TIID FINE TIID. DASH NO.
~ FCR CRES
~~-=t~
First dash No. denotes size of screw Second dash No. denotes length in sixteenths Plain dash No. denotes steel screw Add "CO before tirst dash No. tor cres screw Add "DD" before first daah No. tor ale allO)" screw Add "R' before second dash No. for reoessed head (steel 0017) Example: AN526-632-4 = #6-32 slotted head ateel sorew 4/16 long AN526D~32-4 = #6-32 slotted head ale allO)' screw. 4/16 AII526c632-1i= '1/16 long = AH526-632R4 acrew. 4/16
long #6-32 slotted bead crea sorew. #6-32 r~ ••ed bead ateel long
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AN530 AN531 AN535
SCREWS
S
1114
14 First dash No. denotes size of screw Second dash No. denotes length in sixteenths
Add "Rn before screw
-----
-B== -- ---J f- LENGTH ~
Example: AN530-6-6 AN530-6R6
second dash No. for recessed
=
116
=
116
head
slotted head steel screw, 3/8 long recessed head steel screw, 3/8 long
AN SIZE
1114
14 First dash No. denotes size of screw Second dash No. denotes length in sixteenths Add 'R" before second dash No. for recessed head Example: AN531-6-6 AN531-6R6
-E3==-~~_J f--
LENGTH
= 116 slotted head steel screw, 3/8 long = #6 recessed head steel screw, 3/8 long
~
SIZE
#14
DASH
14 First dash No. denotes size of screw Second dash No. denotes length in sixteenths Example: AN535-2-2
= steel screw, size #2, 2/16 long
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SCREWS
~
~
NO ••
2
4
AN545 AN550 AN565
6
8
10
1
14
1
12
14
16
First dash No. denotes size of screw Second dash No. denotes length in eighths Plain dash No. denotes steel Add "B" before first dash No. for brass Add "R" before second dash No. for recessed head
~
L ~t L::J LENGTH
~
Example: AN545-l0-l0 = 610 slotted head steel screw, 1-1/4 (10/8) long AN545B10-10 = 610 slotted head brass screw, 1-1/% (10/8) long
616
16 First dash No. denotes size of screw Second dash No. denotes length in eights Plain dash No. denotes steel
~
I
L~3
LENGTH
Add 3
"B" before first dash No. for brass
~~:~:
"N550-l0-l0 = 610 slotted head steel screw, l-lft! (10/8) long AN55C1!lO-10 = "10 slotted head brass screw, 1-1/11 before (10/81 long second dash No. for recessed head
SIZE DASH NO.
r1rst dash No. far t7P" "II" first dash No. far tn>e "c" first dash No. far tn>e "D" second dash No. far hex socket
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(FOR SWAGING)
TERMINALS
AN663 AN664 AN666
AN 663 TERMINAL
- DOUBLE SHANK BALL END CABLE
6
DASH NO.
~ CABLE S I'lE
Add "e" before
dash No. for cor.
res.
steel
term 1na 1 Example:
'I647/32 ,616 <; .846 .500 ,730 87 .384 .962 3/32 3/16 1/8 5/32 114
.268 1/16 2 AN 664 TERMINAL
AN66.3-6 6/32 dla. = termtnal, cable
non-cor.
AN663C6 = terml"al, 6/32 d la. cable
cor. res. steel,
res.
steel,
- SINGLE SHANK BALL END CABLE
DASH NO
Add "CO before dash No, for cor. res, steel terminal Example: AN664-6 = terminal, 6/32 dla. cable AN664c6 = terminal, 6/32 dla. cable
non-cor, res, steel, cor, res. steel,
4
4-28 3/32
I
LENGTH
C
E-~-=--+-~ ---------Exampl ••
1/8 ~
5/32
~4 7/32 Plain dash Nos. for for cor. res. steel terminals Add "P" for non-cor. res. steel terminal Add R.H. or L.H. after dash Nos. for right or left hand threaded terminals
3/16
I
~
AN666-6R.H. = terminal, cor. res. stl., 3/16(6/32) dla. cable, R.H. threads
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(FOR SWAGING)
TERMINALS-
AN667 AN668 AN669
DASH NO. CABLE SIZE liD" DIA F
.093
G
Dash Nos. are for cor. rea. steel termtnala
---
ttl -
'. OO=-.:::-=.:::.:::.:::.::_-~
~~~-f+~
~ - --
~
+ '/ "D' /
Add ''F'' before dash No. for carbon steel termlnals Example: AN667-6 = termlnal, cor. res. steel, 6/32 dla. cable, fork end AN667F6 = termlnal, carbon steel 6/32 dla. cable, fork end
AN
3
2
DASH NO. "D" DIA. CABLE SIZE
I
1/16
I
3/~3-,,2-,----,,~
t ~ -
~------Ei1::..=..:: ---:::------
termlnals Addsteel "P" before dash No. for carbon EX~~~8:6 = termlnal, cor. res. steel, 6/32 dla. cable, eye end AN668F6 = termlnal, carbon steel, ;)a~~r:,;~~~l:re for cor. 6/32 dla. cable, eye res. end steel
-
D"
DASH NO TIffiEAD
CABLE SIZE
1 Dash Nos. are for cor. res. steel termlnals Add "P" before dash No. for carbon steel termlnals Add R.H. or L.H. after dash No. for rlght or left hand threads
Example: AN66gFL6R.H.
= long termlnal,
carbon steel, 6/32 dla. cable, R.H. threads
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CLAM PS
AN
735 CLAMP
-
LOOP
AN735 AN737
TYPE
BONDING
to
R.
1
---..c "faSh No. ~
denotes
I Dash inNos. sixteenths are for Add "D" before dash al. alloy clamp
inside d i••• steel cl••• ps MI. for
Example: AN735-2 = steel clamp .125 (2/16) inside diameter AN735D56 = al. alloy clamp 3.500 (56/16) inside dia.
AN 737 CLAMP
- HOSE
Dash No. denotes insIde dIameter In thIrt7-seconds
Example: AN737-34 = single sIze sIze clamp clamp opens opens to 1-1/16 (34/32) (46/32) inside diameter AN737-46-56 = multiple from 1-7/16 InsIde dIameter to 1-3~ (56/32) InsIde diameter
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CLAMPS
AN741 AN742
DASH NO liD I' DIA
designates
one half clamp (for type B) I Add
"E'1
liD"
,
I
'. -
,
alloy Add "H" before a1. alloy dash No. for 52S al. alloy Add "p" after steel dash No. for plated clamp
t
(~-
I.
Add liT" before
[J);-' TYPE
TYPE B
A
dash
No.
for
"a"
type
clamp Example: AN741-6p
=
clamp, type "A", steel
plated AN741D6 = clamp,
type
"A", al.
alloy
24S
AN
SU~
2
8
Add
liD"
No. for Add
before
al.
dash
alloy
"e" after dash
No. for
cush ton
clamp.
Pla 1n dash No. denotes
PLAIN CLAMP
steel
CUSHIONCLAMP
Example: AN742D8 dtameter platn clamp, clamp, al. steel alloy .500 .500 (8/16)(8/16) tnstdetnstde dtameter AN742-8 == platn tnstde dtameter AN742D8c = cushton clamp, al. alloy .375<3/8) .375 (3/8) tnstde dtameter AN742-8c = cushton clamp, steel
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TEE - FLARED TUBE
AN783 AN784
TUBE O.D. THREAD DASH NO.
Plain dash denotes steel Add "D" before dash No. for at. alloy Example: AN783-4 = tee, steel, 1/4 tube O.D. AN783D4 = tee, al. alloy, 1/4 tube O.D.
INTERNAL THREAD ON RUN
denotes .teel da.h No. for al. Example: AN784.4 AN784D4
= =
tee, .teel, 1/4 tube O.D. tee, al. alloy, 1/4 tube O.D.
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TUBE FITTtNGS
DASH
AN804 AN807
NO.
Add "D" before dash No. for a1. alloy Platn dash No. denotes steel
Example: ANB04 -6 = tee, steel, 3/8 (6/16) tube D.D. AN804D6 = tee, a1. all oy, 3/8 (6/16) tube D .D.
Platn dash No. denotes copper alloy Add '~" after dash No. for al. alloy
i
Example: ANB07-B : =adapter, alloy,, (81l6) (B/16) tubeD.D. D.D. ANB07-BD adapter, copperalloy, tube
al.
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TUBE FITTINGS
AN815 AN816
-..~
eel Plain"D" Add dash after No. for No 'dash denotes st al • alloy Example: AN815-6 = = union, •• steel AN815-6D union, 3/8 3/8 (6/16) (6/16) tube tube O.D O.D., al. alloy
-e~~ - ----
'I
-
Add "II" after dash No. for copper alloy Add "D" after dash No. for al. alloy
+Plain
t
Example: AN816-4 = nipple, tube O.D. to 1/8 dash No. denotes steel pi~ thread, steel tube O.D. to 1/8 AN816-4B = nipple,
t
t
pi~thread. cop~ alla" AN816-4D = nipple. tube O.D. to 1/8 pipe thread. al. alloy
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FITTINGS
TUBE
1
1 3A
2
8-12 1713-12 27'Lt-1212 ~2-12
~1
-
--
AN819
1 1/2
-$--n f-
AN818
20
24
28
32
Platn dash No. denotes steel Add. "DII after dash No. for a1. alloy Example: AN 818-4 = nut for l/Lt tube O.D., steel AN 818-4D = nut for l/Lt tube O.D., a1. alloy
, ~
12 .255 1 .193 10 8 16 .631 1.006 1/2 .380 .318 5/8 3/Lt 4 lA 3/16 .505 .756 6 .130 1/8 2 5/16 3/8 TUBING
AN 81q SLEEVE
- COUPLING
O.D.
~& B
_
2 2.014 ~
32
Platn dash No. denotes steel Add "D" after dash No. for al. alloy ~O No. for al. bronze Add "Z" after dash
Example: AN819-5 = sleeve, 5/16 tube O.D., steel AN819-8D = sleeve, 1/2 tube O.D. alum. alloy AN819-5Z = sleeve, 5116 tube O.D. alum. bronze
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AN82! AN822
TUBE FITTINGS
THREAD DASH NO.
2 steel for al. alloy
Example: AN821-11 ••elbow, 1/4 tube O.D., steel AN821-IID = elbow, 1/4 tube O.D., al. alloy
Plaln dash No. denotes steel Add "D" after dash No. for al. alloy Add "B" after dash No. for copper alloy
Example: ~ I,
and 1/8 plpe thread, steel AN822-4 = elbow, ~ tube 0.D. AN822-4D = elbow, & 1/8 plpe thread, tube al. a.D. alloy
!
AN822-4B tube O.Dt & 1/8 plpe= elbow, thread, ~copper al oy
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TUBE FITTINGS
'.',
AN823 AN824
,
,.' I
I :
Example: AN823-4 AN823-4B AN823-4D
Plain dash No. denotes steel Add "D" after dash No. for al. alloy Add ~" after dash No. for copper alloy
= elbow, ~ tube O.D. • = elbow,
t
& 1/8 pipe thread, steel & 1/8 pipe thread, copper alloy al. alloy
tube D.D. O.D.
Plain dash No. denotes steel Add ~. after dash No. tor al. alloy
Examtlle: AN824-4 = tee, ~ tube D.D., steel AN824-4D • tee, • tube O.D., al. alloy
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TUBE FITTINGS
AN825 AN826
Example: AN825-4 = tee 1/4 tube O.D. & l~ pipe thread, steel AN825-4D = tee 1/4 tube O.D. & 1/8 pipe thread, alum. alloy AN825-4B = tee 1/4 tube O.D. & 1/8 pipe thread, copper alloy
2 AN 826 TEE - FLARED TUBE WITH PIPE THREAD ON RUN 16-12 tJ.6-24 1/8 8 1 2~6-1; 31/8 1 -16 1/8 <; 1 0 16 1/8 'V'16-20 5/16 1.116-12 1/2 3/4 3/16 9/16-1£ 4 5/8 /8-14 1/4 3/8 61 1/2-20 /8-24 1/2 ,,A 11 1/8 ~6-12 3/8 TUBING
O.D.
Plain dash No. denotes Add "D" after dash No. Add "B" after dash No.
Example: AN826-4 = tee 1/4 tube O.D. & 1/8 pipe thread, steel AN826-4n = tee 1/4 tube O.D. & 1/8 pipe thread, alum. alloy AN826-4B = tee 1/4 tube O.D. & 1/8 pipe thread, copper alloy
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TUBE FITTINGS
AN827 AN832 AN833
!...H.:.12 11
~ plain dash No. denotes Add "n" after dash No. Example: AN827-11 = cro88, 11'% tube O.D.,
steel
1
TUBING O.
5/16-12
THREAD
16
DASH NO. 11'%
@-
8 -12
I
I
20 211 28 Plain dash No. denotes steel Add "D" after dash No. for al. all OJ Exalllple : = steel union, 11'% tube O.D. AN832-11
Plain dash No. denotes steel Add "D" after dash No. for al. aUO)' Example: AN833-_ • steel elbow, l~ tube O.D. AN833--» • al. allO)' elbo., l~ tube O.D.
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FITTINGS- TUBE*iOSE
AN834 AN83? AN838
Plain dash No. denotes Add "D" atter dash No. tor al. alloy Example: ANB34·4 = tee, 1~ O.D. tube, steel ANB34·4D = tee, 1/4 O.D. tube, al. alloy
Pla in dash No.
~~~o~~~ :~~:;
11
dash No. tor al. aUoy Example:
Plain daah No. denotes copper alloy Add "D" after dash No. tor al. alloy Example: ANB3B-4
= elbow, 1~
O.D. tube,
oopper aUoy ANB38-4D = elbow, 1/4 O.D. tube, al. aUoy
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HOSE FITTINGS
AN839 AN842
AN 839 ELBOW- HOSET TUBING O.D. HOSE I.D THR EAD
DASHNO.
Platn da.h No. denote. copper alloy Add "D" after da.h No. for al. alloy Example: AN839-4 = elbow, ,} tube, O.D. copper alloy AN839-4D = elbow, ; tube, O.D., al. alloy
HOSE I.D PIPE THD. DASHNO
Platn da.h No. denote. copper alloy Add "D" after da.h No. for al. alloy Example: AN842-4 = elbow, ~ (4/16) I.D. Ho.e, copper alloy AN842-4D = elbow, ~ (4/16) I.D. ho.e, al. alloy
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HOSE FITTINGS
AN844 AN846
PIPETHD DASHNO. P1atn dash No. denotes copper alloy Add "D" after dash No. for a1. alloy Example: ANB44-4 = elbOW, ANB44-4D = elbow,
to
hose I.D., copper alloy I.D., alum. alloy
4 hose
P1atn dash No. denotes copper alloy Add "D" after dash No. for a1. alloy Example: ANB46-4 = elbow, ~ hose I.D •• copper alloy ANB46-4D = elbow, 4 hose I.D •• alum. alloy
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HOSE FITTINGS
120 29/16-18 16 24 1110 lA 4 81lA; 6,/8 7/16-20 3;11-16 11\.6-12 n6-12 0;/8 1/2 7i3 -12 -12 1,}4 ltJ 117/8-14
AN848 AN849
AN 848 ELBOW- HOSE BULKHEAD900
HOSE I D
Platn dash No. denotes copper Add "D" after dash No. for a1.
alloy alloy
Example: AN848-6 = elbow, 3/8 (6/16) hose I.D., copeer alloy AN848-6D - elbow, 3/8 (6/16) hose I.D., a1. alloy
111
HOSE LD
~6-12
16
---00= ------
- ------ -----
::.::-
~
+ I r,z" ~~ '
~".,. Example:
Add "p" after
1 ~-12
20
dash No. for al. alloy
,••, ,•• ,•••,••••,,"""'<0
AN849-6 = = connector, connector, AN489-6D
3/8 alloy 3/8 (6/16) (6/16) hose hose I.D., I.D., copper al. alloy
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BUSHING-
SCREW REDUCERTHRfAD
AN893
"'''''''ADEDEND 7. 11/4 7, B A 6-20 ·<;/16 <;/8 11/16-12 THR EAD 1c; 6-12 <;/8 11_1? ')/16 C;"1;_1? 3/8 ')/ 11/16-20 111 11/2 TUBEO.D. ~-J45/16 5/8 5/16 5/16-12 ,/8 'R c;/R 1/2 3/4 1,,/11; <;/16-12 "/R ,7' 1/16-12 ,6-20 h~ h? Jh 1-7/64 1/2 7/16 3;4 7/R-14 1/2-20 13/16 15/8 <;/8 1/2 -20 ')/ 5/8 578 15/8 OVERALL 1-1/64 7/16-20 3;4 1/8-14 15/16 86-20 16-1? -12 1125/32 15/16-12 1;4 11/b4 1<;/16 1/16-12 19/16-18 <;J 31/32 27732 ,1 1;4 1IIh 1/8 3/8 7/R c;/R -16 ,/8 8 -14 7/1'\ 3/8 3/4 ,,/8 11/64 17/R "118 9/16-18 <7/64 11;4 111>'1 21/32 0/16-18 < 8 17/8-14 3;4 Ih -11; AN80'1 BUSHING- SCREW THREAD REDUCER 3/4 ,.,/P. 7/9-14 1/16-12 ,1/32 13/lb ,,/1'\ c;/iI 1<2 ,IIh c;/R 7/R -12 _1? _1? 1/8-111 1/2-20 3/3 <1/<2 ll~ '11/<2 1')/16-12 o.l.R D~~
Plain dash No. denotes steel Add "D" after dash No. for al. alloy Example:
AN893-4 = bushing, steel AN893-4Da bushing, AI. 10110}'
4
to 3;4 tube O.D•• ~ to 3111tube O.D.,
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BUSH ING-
AN894
SCREW THREAD EXPANDER
,
INTERNALLY THREADED END ALL OVER -4 -12 -<; .116 -8 ./Ii ,<;/64 B "116-12 -10 -16 l/1i -6 ·4 _11 1/4 1/2 ,/Ii ,;\I 1.;\1-16 ~~ ,,116-12 /&.h ul16 EXTDlNALLY THREADED END -2 -. _4 ,,/1;; ,h A ~At 3/8 1/8 15/8 -5 7116-20 7/8-14 1/2-20 3/8-24 7116-20 ,./8-24 ~At_, /1 1/64 7/64 h_o" ;;_?n 1116-12 TIm" 5/16 3/16 00 .1113/16 13116 /8 At ;; D. 5/8 tiT> 1<;/8 TUBE 21/4 3/4 5/16-12 -1613/8 1,At /8 7/811,5/8 3;\1-161 2221/64 1/2-20 ,.,1 9116-18 3/4 3/8 19/64 19/611 25/64 59/64 21/32 U/64 ,1116-12 '!'HR"AT> /? 1/2 1/4 5/8-12 <;/8-12 ./8 ,/8 ./8 7/8 3/8 ./8 5/16-245/8 5/16-24u/16 3/16 1/8 1/2 -2111;\1 .,-->'<;/64 Q116-18 /1 7/8-14 9/16-18 ./Ii 7/8-14 ;;_'On 5/8 1,,/8 Q/16-18 11/16-12 1116-12 3/1i ./Ii "<;116 116 7/8-14 ,/Ii 1./64 1'!'HREAT> -16 "/8-12 11,,/8 11/8 1/8 121h2 41/64 13116 43/64 1;\1 1,,/8 7/8-141 7/8 5/8 AN 8Q4 BUSHING- SCREIITHREAD EXPANnDl •••
DASH
Plain da.h No. denote •• teel Add "D" before flr.t da.h No. for a1. a11"7 Example: AN8g4-10-6 : bU.hlng, 5/8 to 3/8 O.D.
tub., steel
AN8g11m0-6 • bu.hlng, tube, alum. aU"7
5/8 to 3/8 O.D.
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PIPE FITTINGS
AN910 AN911 AN912
1 1;11 10
PIPE THREAD DASH NUMBER Plain dash No. denotes copper alloy Add "D" after dash No. for al. alloy
-BB-- ~ ~~
Example: AN910-4 = coupling, 1/2 pipe thread, copper alloy AN910-4D = coupling, 1/2 pipe thread, al. alloy
11/4 10
or No. for al. alloy Example: AN911-4 = nipple, 1/2 pipe thread,
bronze or brs8B
AN911-4D = nipple, 1/2 pipe thread, al. alloy
1 3;11
10
=~-~-
=~--
1
1
1/2 3/8 11 12
Plain dash No. denotes copper alloy Add "D" after dash No. for al. alloy Example: AN912-4 = reducer, from 1/2 external pipe thread to 3/8 internal pipe thread, copper alloy AN912-4D = reducer, from 1/2 external pipe thread to 3/8 internal pipe thread, al. alloy
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PIPE FITTINGS
AN914 AN915
AN
PIPE THREAD
1 1;4
DASH NUMBDI
10
Plai~ daeh de~otee copper alloy Add "D" after dash No. for al. alloy Example: AN914-4 alloy AN914-4D
900 elbow,
= =
900 elbow,
t
pipe thread, copper
t
pipe thread, al. all07
PIPE THREAD DASH NUMBDI
Plain daah No. denotea copper alloy Add "D" after daeh No. for al. alloy Example: AN915-4 = 450 elbow, copper alloy AN915-4D = 450 elbow, alloy
l
pipe thread,
t
pipe thread, al.
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PIPE FITTINGS
AN916 AN917 AN918
ELB(I\I
1/11
l~ 10
Plain dash No. denotes copper alloy Add "D" atter dash No. tor al.all07 Example: AN916-6 = elbow. 3/11 pipe thread. copper all07 AN916-6D = elbow. 3/11 pipe thread. al. alloy
1 1/11
10
Plain dash No. denotes copper alloy Add "D" atter dash No. tor al. alloy Example: AN917-6 = tee. 3/11 pipe thread. copper alloy AN917-6D = tee. 3/4 pipe thread. al. alloy
l~ 10
PIPE THREAD DASH
NUMBER
Plain dash No. denotes copper alloy Add "D" atter dash No. tor al. alloy Example: AN918-6 alloy AN918-6D alloy
= cron,
3/4 pipe thread,
copper
= orees, 3/11pipe thread, ai.
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TUBE FITTINGS
7NUMBER 28 2, 24 "38Q 26 17 422 27 1" 16 12 21 18 2'; 10 11 14 12 6013 19 20
AN919
,
'>.111 21/l6-12 'B >. -16 7J END 0;/16-12 0;11.6-12 TUBE0 DSMALL 13;11 '>./R 'I0; ,I 23 3LARGE 11/2 13/8-24 1/2 11;11 1/4 711.6-20 ,) 1/2-20 3/4 "17/8-14 OJ ';/16-12 , 083/4 51 61/4 B-24 6-18 15/16 1'>./8 575/16-24 '>./8 5/l6-12 2718-14 16-24 R 2QJ -20 -16 7/8-14 518 'I'''''E THREAD 3/8 D 3189/16-18 16-20 6-20'>./16 7/l6-20 7/16-20 11/4 318-24 3J11-16 9/16-18 3/4-16 7/16-20 11/2-20 5/8-12 17/R-14 '>./R-241/8 7/8-12 5/8-12 1/16-12 1/16-12 5/16 3/16 1/8 5/lb-12 1/16-12 ANQ1QREDUCER-EXTERNAL 7/8-14 111.6-12 111.6-12 ';/8 518 3/16 THREAD FLARED TUBE 11;11 5Ja-12 1;11 5/16 11/'1 318 l/2 DASH
Plain dash No. denotes steel Add "D" after dash No. for al. allOJ -
-
-.ExamPle:
+
7
AN919-5 = reducer. 3/8 to 3/16 tube o.n., steel AH919-5n = reducer, 3/8 to 3/16 tUbe o.n •• Al. AHo)'
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TUBE FITTINGS
AN924 AN925
TUBE O.D
-
I I I I
-D I
:.
--Plain dash No. denotes steel Add "D" after dash No. for al. allo7 Example: AN924.4 • steel nut, tube O.D., 7/16-20 thread AN924.4D = al. alloy nut, ~ tube O.D •• 7/16-20 thread
t
ateel for al. all", Example: AN925-6 = cross, 3/8 tube O.D., steel AN925·6D • cross, 3/8 tube O.D., a1. alloy
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TUBE
FITTINGS
AN926 AN927 AN928
plain dash No. denotes steel Add "D" after dash No. for sl. alloy Example: AN926-6 ••tee, 3/8 tube O.D" steel AN926-6D = tee, 3/8 tube O.D., al. alloy
Plain dash No, denotes steel Add "D" after dash No. for al. alloy Example: AN927-6 ••900 elbow, 3/8 tube O.D., steel AN927-6D = 900 elbow, 3/8 tube O.D., al. alloy
Plain dash No. denotes steel Add "D" after dash No. for al. al107 Example: AN928-6 ••450 AN928-6D ••450 elbow, elbow, 3/8 3/8 tube tube O.D., O.D. steel al. alloy
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GROMMET -ELASTIC
"
16 _1'" 20 0--<; ,_?n _,? 28 10 2-26 56 0;2 ;_0 22 -40 1-44 "A 26 7n111 11 1_' -12 -1"'. -10 1' .• 8-20 ,;,;
AN931
, ,,
I"h,,
0; ,/'1 7<;/'8 611/16 '4 11/11 71<; oA6 1/4 J,3111 11, 17 11/16 <¥l6 <;/1 5/1 11 1113/16 <; 1~ 7/ -vi 6221<; I" 79/16 111.1 /1 711 '1.1 4271,,)1-6 3112 3/8 12.""19/l1 218<;/8 7?2216I, 613. 5/ o;/; 77. 53 "770; 1. 51 811/8 '16 8116 1/2 17 7/1 5/8 1, 0;, 67. ,,8 0;. 0;, 'l6<; 36If10;', /1 1212 65/1t 33/8 9/l1 17/16 51 11/8 ,,8 55/'8 1/4 7/16 11/4 ,/8 75/8 2,; 9,,1.6 ,/8 1/'8 1825/11 '8 611 39, 7/1 5/8 59/1 3/1 1',16 62 7, 11 0;,8 1, 31/2 111;1.6 1<;/16 37"IV 106 1/16 1~ 1612100;', ,,8 111'4 <;. 3/8 ~6 318 iV 5/8 1/8 162'8 13/16 "7/'8 9/ 6." 17. 5/2
R /III'V': 1<. 1<. K H 7/1~ 7 Eun 7J ." gilt '';: MOU ,,; ." ,At 'A 11 r~AI .". Ii 1<. ." 6~.". ~At ." /A -7 'lE 6'4'A 3/8 QJ D <;, ,11. .,,/1 3/4
Add "A" before first dash No. far grommets with 1/8 groove width Add "B"" n "" " .... 3/16" " Add Itel' " " "1/11 second Add ''W " " web tYDe grommet " "sp1tt'~ " Add "s" Example: AN931-6-10 = grommet with 3/8
I.D., 51'8
groove die. and 1/16 groove width
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PIPE
PLUGS
AN932 AN933
1 1;4
8
---~"" ---,
I I I I I IT
I II - --.{..) ___ J
PIa In dash No. Add "u" ber ore plated steel Add "D" berore aUoy Add "C" berore
denotes plated steel rlrst dash No. ror unrlrst dash No. ror al. rlrst dash No. ror
A~~P~:~ ~~;:e rirst
dash No. ror
magnesium
Example: AN932-2=1/8 AN932U2 = l~Ripe pipe thread threadplated unplated steelsteel plug plug AN932D2 = 1/8 pipe thread al. aUoy plug AN932C2 = 1/11 pipe thread copper aUoy plug AN932M2 = 1/8 pipe thread magnesium plug
Plain dash No. denotes ateel Add ~" berore daah No. tor copper allqJ Add "D" berore dash No. ror al. al107
/..--,I
--
'''---.•.
.•..•
ExaIIIple: AN933-6 • plug, 3/\ pipe thread, steel AN933B6 • plug, 3/4 pipe thread, copper aU07 AN933D6 ••plug, 3/11 pipe thread, a1. aU07
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WASHER-
iii
1110 112 18 114 #6 1;11 5/16 7/16 3/8 1/2 5/8 3 #5 9/16
nASH
2468'I 416 REGULARSERIES 10 1016 716 516 616 816 1216 Q16
MEDIUM
AN935
SPRI NG LOCI<
SIZE 2L LIGHT 416L 4L 6L 616L 8L 1016L 1216L 716L 816L 101, SERIES '\L 516L Q16L BOLT "'1<""S
IJI
---$--+ Plain dash No. denotes Itesl lock washer Add "B" bet ore dash No. tor phosphor bronze Example: AN935-10 = steel lock washer tor '10 bolt, regular AN935-1CL = steel lock washer tor #10 bolt, 11ght AN935B1CL a bronze lock washer tor '10 bolt, 11ght
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WASHER-LOCK
AN936
1016 5/8
INTERNAL
TEE'l'H
EXTERNAL
TEE'l'H
COUNTERSUNK
TEETH
"A" before dash NO. designates internal teeth washer "B" before dash No. designates external teeth washer "c" before dash Mn. designates countersunk teeth washer No letter after dash Mo. designates steel washer "B" after dash No. designates bronze washer
Example: AN936A416 z steel washer, internal teeth, for bolt AN936A416B = bronze washer, internal teeth, for ~ bolt
t
J
AN936B416 bolt AN936B416B = =steel bronzewasher, washer,external externalteeth, teeth,for f ~ bolt AN936c416B = bronze washer, countersunk teeth, for • bolt AN936c416 = steel washer, countersunk, teeth, for bolt
t
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WASHER- PLAIN -
Jill #10 1/4. 116 6.125 #8 .125 .250 .203 14 1211 .188 3-Jil4 Jil4 #6 .312 .175 .375 .234 .312 8.149 #10 .174 .438 .203 13 .625 416 7Jil5 .438 .265 .375 .50C 14.140 0-0; .078 .094 .500 .109 IRnr.'I'
AN960
AN 960 WASHER- PLAIN
St"1E
STEEL ALUM CRES BRASS AL. ALL COPPER
P
- T1-3 A CU B -II D C -7IA)..316 CODE -101\)-10. 'A'; 1121i11tI4OMI 3~ -IOTO-IONI -10'10-lOIII SERlE.! M~ n~~ -5 -'I to -8 • 14TO-12-101\)_ TO-8 i-IOTO-10M -3TO-4OI6 3-3 TO-8 'A" ~104OIfJ T04OI6 n!J.o iZiiT040le e" nQ1 e" 10TO-516 IRe" ~to-8 iI2I6 T04OI .001 06e; .-101n.4lWl n,,, n!J.?
Add "p" before dash Nos.for Add "L" after dash Nos. for
al. and al. light series
"T" THICKNESS
alloy to obtain washers
anodized
washers
Ex8lllple: regular series, steel ANC)60-716 = washer for 7/16 bolt, ANC)600\lOL• washer for #10 bolt, light aeries unanodized a1uminUIII ANC)60PA1OL= washer for #10 bolt, light series anodized aluminum ANC)6OC10= washer for *10 bolt, regular series, cor. res. steel AN96OCU7• washer for #8 bolt, copper
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REFERENCE TABLES
and CONVERSION
FACTORS
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A
-
TWIST DRillS-lETTER .... 27 .. ..... Size. Wire Inch Drill .295 .404 .302 Diem. Drill Inch 0.368 0.281 0.413 .272 .290 .277 .358 .348 .238 .339 .242 .397 .316 .386 .1820 .0960 0310 14 41 .2210 .1850 .1360 .0465 13 40 0.228028 0.1770 .2130 .2090 .1960 .1990 0.1405 0.0890 0.0280 0.0520 .1890 .1695 .1800 .1065 .0820 .1285 .0995 .1100 .0370 .0380 .0145 25 24 18 12 15 17 79 44 78 36 63 45 72 57 66 42 69 71 35 62 58 51 39 31 498716 311 43 70 0.1910 0.1590 0.1015 0.0760 .1935 .1660 .1040 0.323 0.257 .0730 .0360 .0240 .0225 0.234 Diom. 20 .250 22 23 .377 19 .266 .246 10 .332 .261 46 47 76 73 37 59 50 32 ..Diom. 26 75 53 48 3618Drill 65 .1440 54 0.204033 0.1130 .2010 0.0400 .1110 34 61 60 68 .0980 .0320 67 29 56 .1730 .1200 .0935 :1495 .0635 .1520 .0860 .0670 .0430 .0330 .0292 .0250 .0260 .0420 .0160 52 30 55 .2055 0.1470 0.0595 0.0135 0.0350 0.0210 .1160 .1570 .1540 .0700 .0785 .0810 .1610 .0410 .0180 .0200 77 64 49 74 21 52Inch 80 .0550 Wire Goge .0390
p
AND WIRE GAUGE SIZES
AMERICAN STANDARD TAPER PIPE THREADS Dimensions in Inches Size
Outside moll Dio. Inch Joint End St·d.Wt. Effective Threo Thick. Drill d ofDio. 0.540 0.840 0.675 0.405 1.050 0.113 0.140 0.546 0.109 0.068 0.091 0.707 Threod. 0.145 0.683 0.724 81.200 515/16 7Size 32 0.402 0.088 0.534 0.264 0.408 4.500 0.133 0.237 1.300 Length 3.500 0.7 0.154 23 of Engoge. per 3.241 Top Pipe 57 16 for 4.000 0.226 1.250 0.701 0.334 1.488 27 18 14 18 14 Vlinor Tight 8of 2.875 1.138 4.234 0.433 0.911 0.568 1.660 9/16 11 1/2 1.727 1.144 1.315 1.900 2.375 3/4 3/8 1/2 11/16 1/4 11 133/4 41/4 2.199 1/2 1/2 19/32 1/16 3.738 2.620 110.216 1/8 23/32 3:z0.203 11 5/1 1/4 1/2
Woll
1,%'16 lX32 1 2X32
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AMERICAN STANDARD SCREWS Coarse Thread Series Dimensions in Inches Number or Decimal Diameter Minor 3.0000 .5000 3.1752 .6250 .5000 1.1572 1.0322 .5069 423911 120 25 F 1.0000 1.1250 4.0000 3.2500 3.0000 0.5625 0.1380 0.2500 .5000 .7500 .8750 .2500 .3750 0.0730 0.2010 .7500 0.1065 0.0595 ..4375 .3125 2.1752 .3750 2.1057 .7500 .16.40 .1900 .2160 .0860 .0990 .1250 .1120 .2570 64 .3.4.47 32 41 40 .1770 .1495 .1015 0.9394 .0785 .0890 .1360 .4252 3.0876 .3376 .6752 .123.4 0.1850 .2.403 ..4252 .1619 1.7113 .07.4.4 .0855 .1088 .2835 ..4902 .6201 0.0629 .2938 0.508.4 1.0644 ..4001 ..4500 .5660 .7307 .8028 .8376 .1585 .2667 2.9252 0.1177 .1.437 0.2175 .276.4 .1629 .0958 .0925 .3917 0.0527 1.8557 .9613 47 43 31 16 53 37 .1359 .0700 0.0974 .5876 .0628 .0719 .0795 0..45.42 .6850 .1889 .33.44 .2500 .9188 .8376 .2500 1.7812 1.1094 .5000 16 50 .7500 91/2 4U Diameter per 11 2.0000 0.9844 .3125 0.4844 .7500 13 2.0312 .5312 •.4219 10 12 .8750 .6562 .7656 .29 .3437 .2187 .5625 .2500 .5000 67536 41/2 2.3680 21/2 156 49/64 17/32 27/64 324 17/64 33/4 9/16 31/64 1/32 314 63/64 1/4 1/4 23/4 21/32 7/1 1Pitch 7/32 5/16 11/32 25/32 41/2 Major Identification
Baoic •• Tap Diamete Drill Sizeo
Size
ds
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AMERICAN STANDARD SCREWS Fine Thread Series Dimensions in Inches Decima Pitch 72 36 .3750 32 .1590 .1820 42 45 Diameter Malar Minar Diameter or 0.5625 1.0000 0.0600 0.2500 1.1250 0.1250 0.2130 44 456 64 40 .5000 .2500 .8750 .7500 .6250 80 0.10~0 .~375 .0990 .1380 .16~0 .1900 .2160 .3125 .0860 •1120 .0730 14 .2720 2.3320 •.0700 .1360 .0935 .0820 .0595 .1130 20 1.0167 0.0~38 .0657 .087~ .0985 .1055 .1460 .3917 .1417 .2667 .3209 0.~903 .709~ .~675 .5528 .5889 .3725 .~050 .0759 .0550 0.1102 .1218 .1697 ..258~ 0.2036 0.2268 .285~ .8125 .5781 •37/64 1928 33 53 50 29 21 14 Q .2969 1Size 37 31 20 2. 0.0~69 24 18 14 16 .06~0 0.0955 .~~59 1.0709 .1959 .7822 .8286 0.526~ .66811 .~350 0.0519 .08~9 .0758 .1279 .1~9~ .1696 .3~79 .9375 .6875 .3906 .~531 .9536 1.0~69 12 .1719 .~219 per 11/16 19/64 10.5156 1.9072 27/64 11/64 15/16 3/64 29/64 13/16 25/64 3/64 33/64 Identification
Ba.1e TapDiameters Drill Size.
Number
CLEARANCE DRILLS FOR MACHINE SCREWS 48 .3230 2Drill 29 1Drill 0.1160 0.1285 0.0700 0.0635 37 30 27 52 43 32 .0960 .1360 .1100 .0760 .0810 ~6 35 25 50 30 0.3970 0.2010 0.1960 18 .2280 .2210 .2570 .2660 .3320 .1770 91~~O f.5312 P~1 .5156 16 Q H 7X Decimal Decimal Siu .1695 ..1~95 15/32 10~0 1285 0890 .~687 .4531 Size 0.3860 W 33/64 29/6~ 17/32 Equiv. Equiv.
free fit
Clo.e fit
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O-RINGS MILITARY SPECIFICATION INDEX SEAL·FLUID CONNECTION, 7271. for SEAL·"O" RING, AMS 7271 - fluids Synthetic rubber back-up ring for use with AN 6290, MS AMS 9020, MS O·Ring GASKET - torings STRAIGHT THREAD TUBE FITTING, RING, These rings are from MIL·P-5516B MIL-P·5516B _650rings +160°F. are in hydraulic systems using MIL-H-5606 back-up for AN 6230 O-Rings. er back-up for AN 6227 O-Rings. in hydrocarbon fuels from perma_400 to +300°F.
HYDRAULIC BACK-UP. FITTING, GASKET for from fuel _550 to NUMBER AN·R-22 applications AMS SPECIFICATION AMS -O-Rings 7274C 7270E O-Rings 3651B foreating use a!1d lubriMIL·G-5510A AN-R-22 AN-R-22 PACKING, PREFORMED -+300°F. AMS 7274, "0" RING straight thread tubeinoilengine fitting bosspropellor with _400 togaskets from DESCRIPTION thru SEAL-"O" RING, AMS 7270 - O-Rings for use AN 124050 AN 123950 thru AMS(See 7271B for rotating shafts. Teflon equivalents are 7271BMS B 28782 Iv used. used. (See MS 28783 DRAWING and MS 28774), Teflon equivalents are generally nently dots asand identified designated MS 28774). with in theone latest blue and 5516 two generalyellow 28778, hydrocarbon MS 29512, fuels from NAS _550 617, and toQPL +250°F. NAS 1612 0ded by MS 28777. BOSS. Rings. Superseded Dash numbers hy MS correspond, 28778. release. AN 6246 6244 Class AN AN 123851 123951 RING RING, -BACK·UP, HYDRAULIC HYDRAULIC BOSS GASKET PACKING CONNECTION BACK-UP BACK-UPLeather Leath· Teflon MS 9058 6230B AN 6227B GASKET, O-RING, HYDRAULIC O-Rings for use AN 6291 AN 6290 MS 9021 MS 9020
PACKING, O-RING, HYDRAULIC -
O-Rings
for use
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O-RINGS MILITARY
SPECIFICATION
INDEX
(CONTINUED)
PACKING. PREFORMED·AMS 3304. RING.Shock For PACKING. _65° to +275°F hydraulic systems. PACKING. "0" RING. SHOCK STRUT. For use in"0" RING Leather back-up ring for use with MS 28778 systems pel' 1\lIL-H-5606. Tempprature range of }'ings for use with AN 6230B O-Rings. Dash HYDRAULIC PREFORMEDVALVE. hack-up rings HIGH strut for use air with valve AN adaptor gasket. O-Rings. GASKET SINGLE PACKING MIL·R·5521 PACKING. PRESSURE AIR numbers BACK·UP. MIL-R·8791B MIL·G·551OA MIL·P-25732A FITTING. correspond. TURN. BACK·UP. PREFORMED -For RUBBER. AMS 7272 correspond. MIL·R·8791B MIL·R·879lB 28784 & MS 29513 SPECIFICATION NUMBER forMS rings use with Teflon back-up Teflon O-Rings. MIL-H-5606 fluids from _65° to +160°F. Identi"0" For RING. air and gases .554 diester ± _70° .005 synthetic ID to xequiva+450°F. .070 lubricants ±6227B .003 Static W. from sealClass B Class B DESCRIPTION MIL:P-55l6B AMS 7272 fica tion: one blue and two yellow dots. AF MS 47A1562) 28772 AMS 3304C DRAWING LUOROETHYLENE. cumference. Dash with one blue dot. _40° to +325°F. numbers material is _650 to +212°F. Identification: Nonnumbers correspond. O-Rings. lents are generally used. (See MS 90581. This 28784. FITTING specification These BOSS. rings O-Ring replaces are for permanently +160°F MIL-P-18017 hydraulic identified and fluid MS MS 28782 permanent ing only. blue stripe. 1/32" wide. around cir28778 MS28775 28783 MS 24690 MS PACKING. STRAIGHTTEFLON. THREAD Teflon TUBE RETAINER.PREFORMED. PACKING. BACK·UP. MIL·P·55l6B MS 9241 RING. RING. GASKET. TEFLON. Teflon back-up PACKING.BACK·UP. PREFORMED. HYDRAULIC. +275°F. "0" MS 9068
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O-RINGS MILITARY
SPECIFICATION
INOEX
(CONTINUED)
PACKING, PREFORMED, STRAIGHT THREAD TUBE MIL·P-5516B PACKING, 1\IIL-F-5616 or 1\IIL-F-5624 fuels from _65° to O-RING, HYDRAULIC, 275°F. Cancelled. SupersedESTER RESISTANT (_65° +(lash FITTING low FLANGES). MIL·P·5315A dots. Dash Identification: 5616 number and1\IIL-F-5624 3TO isuse One an160°F). exception blue fuels and from to two this _65° yelType IED, correspond. These rings are permanently identiLUBRICANT MIL-R-7362B MIL-P-18017 ESTER PACKING, from _65° RESISTANT. PHOSPHATE to+275'F. from For Use MIL-L-7808 NAS 617 for fluids tube fit- to +200°F. HYDROCARBON SYNTHETIC FUEL ELECTRICAL PHOSPHATE RESISTANT SPECIFICATION MIL·P·5315A AMS NUMBER OIL USE. FOR "0" for 3209 connectors RING, SYNTHETIC, BOSS, BOSS, PREFORM PREFORMED, PREFORMED FITTING, RING, O-RING, Supersedes AF 934 but numbers do O-Ring RESISTANT. gasket O-Ring for with MIL-L-6387 or (-65° TO + RE160°F). Dash numbers correspond tonot DESCRIPTION Class Ielectrical MS 28778. MIL-L-7808 Grade DRAWING 50 These fluids _65° tocorrespond. +275°F. +250°F. ou tel' circumference. specification fied TU BE with FITTING, two and red BOSS. and isfrom per one O-Rings MIL-R-5847, green for dot, MIL-F as Class shown -5572, IIb, in ANT. O-Ring for use Composition in Class MIL-F-5572, the eo ting +200°F. MIL-Fby latest gaskets. 1\IS QPL 28775. red 5315 rings stripe, Dash release. are numbers 1/32" ioentified wide, with around a nonthe NAS 1612 B fJ permanent MS 29513 AF 934) (Supersedes MS 29512 PACKING GASKET - "0" FUEL RESISTANT, THREAD MS 90064 PACKING, MIL·R·7362B GASKETS, (ROUND, FOR USE STRAIGHT WITH WAVEGUIDE GASKET-TUBE MSNAS 28784 1613 NAS 1613
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METRIC
AND DECIMAL
EQUIVALENTS
OF FRACTIONS (of one inch) nun.
0.234375 15/64 0.171875 0.296875 0.28125 0.21875 0.34375 0.3125 5/16 11/32 0.2517/64 23/64 19/64 21/64 0.015625 0.140625 0.328125 0.359375 0.265625 1/4 3/8 0.1875 0.375 9/32 0.078125 0.046875 0.03125 0.109375 9/64 0.203125 0.15625 3/160.125 5/32 13/64 11/64 7/32 0.0625 1/16 1/32 3/64 5/64 0.09375 1/8 3/32 7/64 1/64
inches
I
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METRIC
AND DECIMAL
EQUIVALENTS
OF FRACTIONS (of one inch) mm.
0.421875 0.390625 0.453125 0.484375 0.4375 0.703125 0.734375 0.71875 0.671875 0.6875 0.640625 0.65625 0.546875 0.578125 0.515625 1/2 33/64 0.40625 0.53125 7/16 13/32 25/64 0.46875 11/16 0.609375 0.59375 0.625 19/32 39/64 9/16 17/32 0.5 3/4 15/32 29/64 45/64 47/64 43/64 5/80.5625 21/32 41/64 35/64 37/64 31/64 27/64 23/32 0.75 I
inches
135
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METRIC
AND DECIMAL
EQUIVALENTS
OF FRACTIONS
mm.
(of one inch) 0.984375 1" 0.953125 0.765625 0.828125 0.84375 0.921875 0.9375 0.890625 0.859375 0.90625 0.78125 0.96875 7/8 0.8125 0.875 27/32 55/64 0.796875 15/16 31/32 29/32 25/32 61/64 57/64 13/16 51/64 53/64 59/64 1.0 49/64 63/64
inches
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--
5 1 4.0 84.2 2.2 82.4 1.7 8 87.8 86.0 9.6 8 0 2C. 3 5.0+--41.0 37.4 32.0 32 + -148.0 -12.8 1.1 0.0 -100 11 10 12 13 14 18 21 24 27 25 26 28 14.0 25 35 45 7 15 9 40 20 55 6 70 65 60 2 80 95 90 5 4 1 2 10 3 48.2 44.6 -103.0 -112.0 -130.0 -139.0 -14.4 53.6 69.8 66.2 64.4 62.6 19 15 16 17 20 13.0 94.0 31.0 40.0 22.0 76.0 67.0 58.0 30 7.2 50 75 85 35.6 33.8 23.0 30.2 5.6 77.0 78.8 80.6 30 29 3.9 73.4 46.4 42.8 -121.0 -12.2 -11.1 -13.9 68.0 55.4 60.8 50.0 51.8 57.2 59.0 85.0 49.0 8.9 6.7 6.1 39.2 0.6 71.6 75.2 31 3.3 2.8 5.0 Deg. -13.3 -10.6 -10.0 -11.7 8.3 7.8 9.4 4.4 137
Deg.
CENTIGRADE C. of. oroC.
of. Deg. oroC. TEMPERATURE F.
- FAHRENHEIT
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28.3 27.2 32.2 31.1 27.8 29.4 30.0 26.1 31.1 30.6 28.9 26.7 22.2 22.8 20.6 21.1 21. 7 20.0 18.9 18.3 17.2 17.8 131. 0 125.6 122.0 120.2 Ill. 123.8 24.4 25.0 25.6 78 2 107.6 23.3 102.2 68 19.4 16.7 138.2 136.4 129.2 87 134.6 127.4 132.8 118.4 116.6 77 109.4 114.8 113.0 23.9 75 72 74 105.8 104.0 70 71 69 100.4 67 98.6 96.8 93.2 95.0 63 64 62 88 59 86 57 56 82 84 53 170.6 81 52 163.4 161. 165.2 167.0 73 76 80 45 6 158.0 156.2 159.8 41 152.6 154.4 66 37 65 145.4 147.2 35 143.6 140.0 91.4 190.4 181. 188.6 179.6 186. 83 58 55 54 4 8C. of. Deg. 185.0 177 85 .8 168.8 174.2 172.4 176.0 79 48 49 44 47 51 50 46 43 42 39 40 150.8 38 149.0 36 34 194.0 90 61 33 183.2 89 192.2 Deg. C. 141.8 of. Deg. 60 oroC. or °C .F. 138
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Deg.
III
61. 62.8 63.3 62.2 56.1 55.0 64.4 61.1 60.6 53.3 54.4 53.9 59.4 57.2 56.7 55.6 57.8 60.0 122 52.2 51.1 52.8 127 58.9 58.3 146 120 121 50.0 123 124 126 51.7 125 128 131 246.2 242.6 294.8 147 148 144 119 117 237.2 115 114 48.9 91 197.6 235.4 233.6 231. 49.4 140 112 8 92 199.4 50.6 251.6 204.8 208.4 260.6 95 96 97 98 210.2 212.0 215.6 213.8 130 129 100 101 102 230.0 228.2 282.2 134 132 135 136 137 104 105 103 110 240.8 293.0 298.4 145 118 116 239.0 289.4 143 195.8 287.6 285.8 284.0 142 141 113 249.8 248.0 93 201. 2106 206.6 258.8 253.4 255.2 257.0 99 266.0 264.2 262.4 217.4 219.2 224.6 226.4 221. 222.8 275. 276.8 278.6 280.4 267.8 273.2 269.6 271. 133 139 138 107 108 109 0 4 244.4 291. 296.6 2C. of. Deg. C. 203.0 ° 63.9 F. Deg. 00794 rOC. oroC. F F.
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Deg.
C.
307.4 311. 0 336.2 338.0 339.8 392.0 390.2 386.6 388.4 347.0 341. 345.2 343.4 334.4 325.4 332.6 330.8 327.2 329.0 95.0 89.4 399.2 397.4 395.6 379.4 381.2 323 393.8 384.8 375.8 377.6 383.0 .6 321. 87.8 374.0 8 C. 316.4 318.2 320.0 86.1 366.8 368.6 370.4 372.2 309.2 312.8 314.6 305.6 84.4 359.6 361.4 357.8 363.2 365.0 302.0 303.8 82.2 81.7 354.2 300.2 178 350.6 96.7 402.8 or 93.3 198 199 200 171 95.6 94.4 91. 90.0 194 202 204 203 172 76 88.3 191 196 192 195 201 190 86.7 187 188 160 85.6 85.0 82.8 83.3 184 182 185 181 153 180 179 356.0 155 151 352.4 206 401.0 92.8 92.2 169 170 197 93.9 88.9 91.1 90.6 193 175 173 174 164 167 165 166 168 163 162 161 87.2 189 186 158 159 83.9 183 154 156 157 152 150 81.1 149 348.8 205 177 Deg. of. 176 or °c . F 96.1 Deg.
Deg.
F.
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Deg.
536.0 520 490 560 550 440 530 450 510 420 420.8 422.6 424.4 390 400 410 430 480 380 340 330 320 310 300 554.0 563.0 298.9 1058 455.0 437.0 446.0 464.0 518.0 527.0 540 460 470 500 275 270 240 428.0 426.2 482.0 250 350 370 360 207 304.4 570 1076 290 295 545.0 285 509.0 280 265 473.0 491. 500.0 220 245 255 260 0.2 210 208 of. or °c 293.3 271.1 1022 282.2 276.7 265.6 260.0 225 235 417.2 419.0 218 216 217 411. 413 415.4 .6 8 410.0 408.2 406.4 590 148.9 580 1040 243.3 1004 788 860 824 842 878 986 968 950 932 230 248.9 716 734 752 806 770 914 219 698 680 662 644 213 212 626 608 209 572 254.4 187.8 214 215 211 160.0 Deg. C. 287.8 896 171.1 154.4 Deg. 193.3 176.7 182.2 C. 404.6 of. or °c .. F. 165.6 226.7 232 210.0 237.8 215.6 198.9 221.1 204.4
Deg.
F.
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Deg.
C.
610 710 1200 1220 1260 1320 471.1 590 600 1652 482.2 620 900 1670 510.0 630 670 910 1814 1778 1724 1688 1706 1760 532.2 526.7 521.1 700 680 640 990 940 960 920 930 548.9 537.8 2228 1280 1240 1000 720 730 1580 1598 615.6 1160 1180 1040 870 740 593.3 2048 2012 1080 1100 1094 1616 880 1634 476.7 890 1130 1742 487.8 950 1274 1256 1202 1292 1776 515.6 504.4 493.3 660 690 650 980 970 1526 1310 1328 1832 1868 1020 830 1562 1454 1472 560.0 2084 1904 2120 2156 2192 2300 1300 850 790 800 810 820 860 840 1382 1400 571.1 604.4 582.2 1940 1976 2408 1120 1060 780 770 750 760 1112 1148 1238 1220 1166 1184 498.9 1544 1490 1508 1346 693.3 2336 2264 1436 1418 1364 Deg. oroC. F 648.9 671.1 682.2 715.6 626.7 637.8 2372 1140 704.4 660.0 of. or C. °C . of. Deg. F.
142
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Deg.
1060.0 1093.3 1104.4 1126.7 1137.8 3200 3488 2444 3560 3524 1071.1 2480 2516 3596 1360.0 1337.8 1204.4 1082.2 3452 3344 2984 2948 2200 2440 2420 2480 3848 1171.1 1193.3 1160.0 3308 3272 3056 3092 3128 2804 2840 2912 2260 2340 3812 3776 3632 3668 3704 3740 1115.6 1148.9 2588 2624 2660 2768 2696 2732 3164 3236 2876 2320 1048.9 1340 1360 4388 1326.7 3380 2552 1640 1400 4352 4316 4028 1315.6 1304.4 1226.7 1237.8 3416 3020 1820 1800 1660 1680 1700 1720 1420 1440 2180 2220 2280 2400 2380 2240 4208 4172 1182.2 1271.1 1780 1760 1580 2160 2360 2300 1380 1940 1960 860 4424 4460 4496 4064 3956 4136 1348.9 1215.6 1620 1980 1 2460 840 880 900 4280 4244 4100 3884 3920 1282.2 1260.0 1540 1560 1600 1460 1480 1520 2120 2060 2000 2040 2140 2020 2080 1740 1920 3992 1248.9 1500 2100 Deg. e. of. Deg. or °e.F. 1293.3 e. of. oroe.
143
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Deg. 1593.3 1526.7 1448.9 1382.2 1393.3 1404.4 1504.4 1515.6 1537.8 1565.6 1621.1 1493.3 1460.0 1648.9
I Deg.
e.
I
10°F = -12.2°e
4748 4784 4532 4568 4640 -12.2 5342 4892 4928 4712 5432 50.0 4820 10 lOoe 4676 4604 4856 4964 5036 5072 5162 5000 2900 = 50.0°F 2620 2640 2660 2500 2520 2540 2560 5252 3000 2680 2600 2720 2740 2760 2780 2800 2850 2950 2700 2580 of. or °C . FDeg. F. or Deg. °e. F.~. C. of. orOC. or EXAMPLE:of. Deg.
C.
144
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INTO
TO CONVERT
MULTIPLY
BY
" """""gilberts/em 0.02471 acres 1.0333 sq feet 0.4950 76.0 0.3937 6.452 2.540 coulombs 39.37 104 0.0254 0.01257 0.1550 1.257 0.01 10-4 eu 100.0 29.92 10-4 14.70 3.259 0.03731 1.562 1.058 x4°C) 10-3 ftin.meter ofof water 33.90 ems of(atA mercury amp-turns/meter faradays gallons 10,332. 43,560.0 sq 4,840. 4,047. mercury gilberts miles yards meters (at O°C) amp-turns/em in.105 amp-turns/meter gilberts/em amps/sq amps/sq 3,600.0 amp-turns/em amps/sq em 1,550.0 amp-turns/in. amps/sq em
"ere-turns/in. "mospheres """""" " em acre-feet ere-turns/em ere-hours eres/sq ere-turns ere-turns/meter peres/sq in. meter amperes/sq
kgs/sq kgs/sq meter em sq meters amp-turns/in. tons/sq pounds/sq ft acres
in.
B
barrels bars
(oil)
gallons
(oil)
42.0
atmospheres
"
dynes/sq kgs/sq
" Btu
0.9869
em meter
pounds/sq
ft
pounds/sQ
in.
ergs foot-Ibs
"
•
by permission
1.020 x 104 2,089. 14.50 1.0:1:10 778.3
gram-calories Reprinted
106
ot
GTE Automatic
1\
1010
252.0 Electr1c
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"/min " hels u/sq /hr
"" CONVERTMULTIPLY kilowatts kilowatt-hrs 17.57 0.03524 TO watts watts cu in. cu 107.5 35.24 INTO 3.931 0.2931 0.02356 4.0 0.2162 0.0700 1.2445 ft BYrs 64.0 32.0 12.96 0.2520 2.928 0.01757 0.1221 3.929 xxin. 1O-~ 1O-~ horsepower-hrs joules foot-pounds/see horsepower gram-cal/sec horsepower-h pints pecks 1,054.8 2,150.4 foot-Ibs/sec watts/sq (dry) ft/min
liters cu meters kilogram-meters quarts kilogram-calories (dry)
Btu C
centares (centiares) Centigrade centigrams centiliters centimeters
sq meters Fahrenheit grams liters feet inches kilometers meters miles millimeters mils yards em-grams
" " " " " " centimeter-dynes " "meter-kgs " "pound-feet centimeter-grams em-dynes " "meter-kgs " "pound-feet centimeters of mercury atmospheres
1.0 (COx9/5)+32 0.01 0.01 3.281 x 10-2 0.3937 10-5
0.01 6.214 x 10-6 10.0 393.7 1.094 x 10-2 1.020 x 10-3 1.020 x 10-8 7.376 x 10-8 980.7 10-5 7.233 x 10-5 0.01316 " " " feet of water 0.4461 " " " kgs/sq meter 136.0 " " • pounds/sq ft 27.85 Reprinted by permisuon of (''TEAutomatic Electric 146
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INTO
TO CONVERT
MULTIPLY
centimeters of mercury pounds/sq in. centimeters/see feet/min " " feet/see " kilometers/hr knots " meters/min " " miles/hr " miles/min feet/see/see centimeters/see/see " " " kms/hr /sec " " " meters/see/see " " miles/hr /sec oircular mils sq ems " " sq mils " sq inches coulombs faradays coulombs/sq in. coulombs/sq em " coulombs/sq meter coulombs/sq em coulombs/sq in. " " coulombs/sq meter coulombs/sq em coulombs/sq meter " coulombs/sq in. cu feet cubic centimeters " " cu inches " cu meters " cu yards " " gallons (U.S. liq.) " " liters
"
pints (U.S. liq.) quarts (U.S. liq.) bushels (dry) cu ems cu inches cu meters cu yards gallons (U.S. liq.) liters
"
cubic feet
" "
" " "
" "
" "
" " " " cubic feet/min " "" "" " "" cubic feet/see " "" cubic inches
pints (U.S. liq.) quarts (U.S. liq.) cu ems/see gallons/see liters/see pounds of water /min million gals/day gallons/min cu ems roll feet
"" Reprinted
by
permission
of GTE
Automatic
BY
0.1934 1.9685 0.03281 0.036 0.0194 0.6 0.02237 3.728 x 10-4 0.03281 0.036 0.01 0.02237 5.067 x 10-6 0.7854 7.854 x 10-7 1.036 x 1O-~ 64.52 104
0.1550 1,550. 10-4
6.452 x 10-4 3.531 x 1O-~ 0.06102 10-6 1.308 x 10-6 2.642 X 10-4 0.001 2.113 x 10-3 1.057 x 10-3 0.8036 28,320.0 1,728.0 0.02832 0.03704 7.48052 28.32 59.84 29.92 472.0 0.1247 0.4720 62.43 0.646317 448.831 16.39 5.787 x 10-4 Electric
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"•cubic "•cubic "•"•meters ""yards/min ubic yards cubic inches
•
•" gallons/see 7.646 1()6 764.6 28.38 27.0 1.639 202.0 264.2 12.74 2.143 0.01732 1.308 0.45 3.367 liters liters mil-feet cu liters ems feet inches feet inches meters cu 35.31 0.01639 0.03463 4.329 1.061 0.7646 meters xxX 10' 10-' 10-3 807.9 MUL TIPL INTO Y BY bushels (dry) TO ""CONVERT pints (U.S. 61,023.0 46,656.0 liq.) lite rs/gallons cu pints quarts cu gallons quarts see yards yards (U.S. (U.S. 2,113.0 1,057. (U.S. (U.S. cubic liq.) liq.) liq.) liq.) ft/sec 1,000.0 1,615.9 cu ems pints (U.S. liq.) gallons (U.S. liq.)
D
days " • decigrams deciliters decimeters degrees (angle) "" ." ." degrees/sec ." ." dekagrams dekaliters
hours minutes seconds grams liters meters minutes quadrants radians leconds radianS/lee revolutionsjmin revolutions/see grams liters meterl
dekameters Reprinted
by
perad •• ion
of r.rE Autoaatic
24.0 1,440.0 86,400.0 0.1 0.1 0.1 60.0 0.01111 0.01745 3,600.0 0.01745 0.1667 2.778 x 10-3 10.0 10.0 10.0 Electric
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drams
MULTIPLY
INTO
TO CONVERT
1.7718
grams
27.3437 0.0625
grains ounces
"
1.020 x 10-3
grams
dynes
joules/em joules/meter
10-7
dynes/sq
em
10-5
(newtons)
kilograms
" "
BY
1.020 x 10-6 10-5
poundals
7.233
pounds bars
2.248 x 10-6
X
10-6
E 9.480 x 10-11
Btu
ergs
"
"
dyne-centimeters
1.0
foot-pounds
7.367
gram-calories
0.2389
gram-ems
1.020 x 10-3
horsepower-hrs joules
3.7250 x 10-14 10-7
kg-calories
2.389 x 10-11
kg-meters kilowatt-hrs
1.020 x 10-8 0.2778 X 10-13 5,688 X 10-9 4.427 x 10-6
Btu/min
"
ft-Ibs/min
" "
10-7
X
0.2778 x 10-10
watt-hours ergs/see
10-8
X
ft-Ibs/sec
7.3756
horsepower kg-calories/min kilowatts
1.341
X X
10-8
10-10
1.433 X 10-9 10-10
F farads
microfarads
faradays
ampere-hours coulombs
fathoms
feet
feet
centimeters
"
"
106 26.80 9.649 x 104 6.0 30.48
kilometers
3.048 x 10-4
meters
0.3048
miles (naut.)
"
miles
millim6t6rs " feet of water Reprinted
by
1.645 x 10-4
(stat.)
1.894 x 10-4
304.8
mils
1.2 x 104
atmospheres
0.02950
permission
of
GTE Automatic
Electric
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TO CONVERT feet of water
INTO
MULTIPLY BY 0.8826
in. of mercury
feet/min
0.03048
kgs/sq
em
kgs/sq
meter
pounds/sq
ft
pounds/sq
in.
304.8 62.43 0.4335
ems/see
0.5080
feet/see
0.01667
kms/hr
0.01829
meters/min
0.3048 0.01136
miles/hr feet/see
30.48
ems/see
1.097
"
kms/hr knots
"
meters/min
0.5921 18.29 0.6818
miles/hr
0.01136
miles/min feet/see/see
ems/see/see
"
a
"
"
feet/1oo
feet
30.48
kms/hr /see
1.097
meters/see/see
0.3048
miles/hr
0.6818
/see
1.0
per cent grade Btu
foot-pounds
1.286 x 10-3
ergs
1.356 x 107
gram-calories
0.3238
hp-hrs
5.050 x 10-7
joules
1.356 3.24 x 10-4
kg-calories
0.1383
kg-meters kilowatt-hrs foot-pounds/min
"
a a
foot-pounds/see
"
3.766 x 10-7
Btu/min
1.286
foot-pounds/see
0.01667
horsepower
3.030 x 10-5
kg-ealories/min kilowatts
3.24 x 10-4
Btu/hr
4.6263
Btu/min
0.07717
furlongs
1.818 x 10-3
kg-ealories/min kilowatts
.0.01945
rods
40.0
feet
10-3
2.260 x 10-5
horsepower
"
X
1.356 x 10-3 660.0
G gallons
eu ems eu feet
" "
3,785.0 0.1337
cu inches Reprinted
by
permission
of
GTE Automatic
231.0 Electric
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TO CONVERT
INTO
MULTIPLY BY
gallons
eu meters eu yards liters pints quarts
gallons (liQ. Sr. Imp.) gallons (U.S.) gallons of water gallons/min
gallons (U.S. liq.) 1.20095 gallohs (Imp.) 0.83267 pounds of water 8.3453 eu ft/see 2.228 x 10-3 liters/see 0.06308 eu ft/hr 8.0208 lines/sq in. 6.452 webers/sq em 10-8 webers/sq in. 6.452 x 10-8 webers/sq meter 10-4 ampere-turns 0.7958 amp-turns/em 0.7958 amp-turns/in 2.021 amp-turns/meter 79.58 liters 0.1183 pints (liq.) 0.25 martinis (dry) 20g + 1v grains (avdp) 1.0 grams 0.06480 ounces (avdp) 2.0833 x 10-3 pennyweight (troy) 0.04167 parts/million 17.118 pounds/million gal 142.86 parts/million 14.286 dynes 980.7 grains 15.43 joules/em 9.807 x 10-5 joules/meter (newtons) 9.807 x 10-3 kilograms 0.001 milligrams 1,000. ounces (avdp) 0.03527 ounces (troy) 0.03215 poundals 0.07093 pounds 2.205 x 10-3 pounds/inch 5.600 x 10-1 pounds/eu ft 62.43 pounds/eu in 0.03613 pounds/mil-foot 3.405 x 10-7 grains/gal 58.417 pounds/1,000 gal 8.345 pounds/eu ft 0.062427 parts/million 1,000.0
"
gausses
gilberts gilberts/em
gills gin grains (troy)
"
" grains/U.S. gal
"
grains/Imp. gal grams
grams/em grams/eu em
" " " "
grams/liter
" Reprinted
by
permission
of
GTE Automatic
3.785 x 10-3 4.951 x 10-3 3.785 8.0 4.0
Electr1c
151
Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
" m-calories am-centimeters m-calories/see a
grams/sq em
" " joules 980.7 4.1868 10-' watt-hrs 14.286 INTO 3.0880 2.343 1.5596 9.807 10-5 10-6 1.1630 TO CONVERT MUL TIPL Btu Y 3.9683 2.0481 9.297 BY x xx10-a 10-8 10-3 ergs ergs foot-pounds horsepower-hrs Btu/hr pounds/sq ft107 kilowatt-hrs kg-cal kg-meters
H
hectares
"
hectograms hectoliters hectometers hectowatts henries horsepower
horsepower (metric) (542.5 ft Ib/sec) horsepower (550 ft Ib/sec) horsepower
" "
horsepower (boiler)
"
horsepower-hrs
" " "
hours
" "
Reprinted
by
acres 2.471 1.076 x 105 sq feet 100.0 grams 100.0 liters 100.0 meters watts 100.0 millihenries 1,000.0 42.44 Btu/min 33,000. foot-Ibs/min 550.0 foot-Ibs/sec 0.9863 horsepower (550 ft Ib/sec) 1.014 horsepower (metric) (542.5 ft Ib/sec) kg-calories/min 10.68 kilowatts 0.7457 watts 745.7 Btu/hr 33.479 kilowatts 9.803 Btu 2,547. ergs 2.6845 x 10'3 foot-Ibs 1.98 x 106 gram-calories 641,190. joules 2.684 x 106 kg-calories 641.1 kg-meters 2.737 x 10' kilowatt-hrs 0.7457 days 4.167 x 10-2 minutes 60.0 seoonds 3,600.0
permission
of GTE
Automatic
Electric
152 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
INTO
TO CONVERT
BY
5.952 x 10-3
hours
weeks
inches
centifTleters feet meters miles millimeters mils yards atmospheres feet of water
Inches of mercury
MULTIPLY
2.540 8.333 x 2.540 X 1.578 x 25.40 1,000.0 2.778 x 3.342 x 1.133 3.453 x 345.3 70.73 0.4912 2.458 x 7.355 X 2.540 X 0.5781 5.204 3.613 x
kgs/sq em kgs/sq meter pounds/sq ft a " " pounds/sq in. inches of water (at 4°C) atmospheres " " inches of mercury kgs/sq em ounces/sq in. pounds/sq ft pounds/sq in.
10-2 10-2
10-5
10-2 10-2 10-2
10-3 10-2 10-3
10-2
J joules
.
joules/em
"
Btu ergs foot-pounds kg-calories kg-meters watt-hrs grams dynes joules/meter (newtons) poundals pounds
9.480 x 10-4 107
0.7376 2.389 x 10-4 0.1020 2.778 x 10-4 1.020 x 1O~ 101
100.0 723.3 22.48
K kilograms
•
Reprinted
980,665. dynes 1,000.0 grams 0.09807 joules/em 9.807 joules/meter (newtons) by permission
of
GTE Automatic
Electric
153 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
TO CONVERT kilograms
" kilograms/cu meter
"
" "
"
a
kilograms/meter kilograms/sQ em
" "
" " " " " "
"
a
"
"
"
"
"
" "
"
"
"
a
kilograms/sQ mm kilogram-calories a a
" "
kilogram meters
"
"
kilolines kiloliters kilometers a
a
" " " kilometers/hr a" "" "" Reprinted
poundals pounds tons (long) tons (short) grams/cu em pounds/cu ft pounds/cu in. pounds/mil-foot pounds/ft
kiiograms/sQ meter
" "
INTO
by
of
BY
70.93 2 205 9.842 x 10-~ 1.102 x 10-3 0.001 0.06243 3.613 x 10-5 3.405 x 10-10 0.6720
atmospheres feet of water inches of mercury pounds/sQ ft pounds/sQ in. atmospheres bars feet of water inches of mercury pounds/sQ ft pounds/sQ in. kgs/SQ meter Btu foot-pounds hp-hrs joules kg-meters kilojoules kilowatt-hrs Btu ergs foot-pounds joules kg-calories kilowatt-hrs maxwells liters centimeters feet inches meters miles millimeters yards ems/see feet/min feet/see knots permission
MULTIPLY
GTE Automatic
0.9678 32.81 28.96 2,048. 1422 9.678 x 98.07 x 3.281 x 2.896 x 0.2048 1.422 x
10-5 10-6 10-3 10-3 10-3
106
3.968 3,088. 1.560 x 4,186. 426.9 4.186 1.163 x 9.294 x 9.804 x 7.233 9.804 2.342 x 2.723 x 1,000.0 1,000.0
10-3
10-3 10-3 107
10-3 10-6
105
3,281. 3.937 x 10~ 1,000.0 0.6214 106
1,094. 27.78 54.68 0.9113 0.5396 Electric
154 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
INTO
TO CONVERT kilometers/hr
"
kilometers/hr /sec
" "
"
kilowatts
"
" kilowatt-hrs
" " " " " knots
BY
16.67 meters/min 0.6214 miles/hr 27.78 ems/see/see 0.9113 ft/sec/sec 0.2778 meters/see/see 0.6214 miles/hr /sec 56.92 Btu/min 4.426 x 1O~ foot-Ibs/min 737.6 foot-Ibs/sec 1.341 horsepower 14.34 kg-calories/min watts 1,000.0 Btu 3,413. 3.600 x 1013 ergs foot-Ibs 2.655 x 106 gram-calories 859,850. 1.341 horsepower-hrs 3.6 x 106 joules 859.85 kg-calories 3.671 x 10' kg-meters pounds of water evaporated from and at 2120 F. 3.53 pounds of water raised from 620 to 2120 F. 22.75 feet/hr kilometers/hr nautical miles/hr statute miles/hr yards/hr feet/see
" "
MULTIPLY
6,080. 1.8532 1.0 1.151 2,027. 1.689
L league lines/sq em lines/sq in. lines/sq in. ((
"
" " links (engineer's) links (surveyor's) liters
"
miles (approx.) gausses gausses webers/sq em webers/sq in. webers/sq meter inches inches bushels (U.S. dry) cu em
"
cu feet cu inches
" Reprinted
by permission
of
GTE Automatic
3.0 1.0 0.1550 1.550 x 10-9
10-' 1.550 x 10-5 12.0 7.92 0.02838 1,000.0 0.03531 61.02 Electric
155 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
liters
MULTIPLY BY
INTO
TO CONVERT
0.001 1.308 x 10-3 0.2642 2.113 1.057 5.886 x 10-4 4.403 X 10-3 1.0 0.0929
cu meters cu yards gallons (U.S. liq.) pints (U.S. liq.) quarts (U.S. liq.) cu ft/sec gals/see foot-candles foot-cand les
•
liters/min lumens/sq ft lux
M maxwells
kilolines webers maxwells microhms ohms centimeters feet inches kilometers miles (naut.) miles (stat.) millimeters yards varas ems/see feet/min feet/see kms/hr knots miles/hr feet/min feet/see kilometers/hr kilometers/min miles/hr miles/min ems/see/see ft/sec/sec kms/hr/sec miles/hr /sec em-dynes
"
megalines megohms meters
" "
meters/min
" "
. •
" "
meters/see
"
" " " meters/see/see
"
"" " " " "
meter-kilograms
0.001
10-' 10' 10"
10' 100.0 3.281 39.37 0.001 5.396 x 10-4 6.214 X 10-4 1,000.0 1.094 1.179 1.667 3.281 0.05468 0.06 0.03238 0.03728 196.8 3.281 3.6 0.06 2.237 0.03728 100.0 3.281 3.6 2.237 9.807 x 107
10'
em-grams «
"
microfarad Reprinted
Aircraft Technical Book Company
7.233
pound-feet farads by
permission
of GTE
10-' Automatic
Electric
I~ 800-780-4115
www.actechbooks.com
INTO
TO CONVERT
micrograms microhms " microliters miles (naut.) "" "" "" "" miles (statute) ." •• •• •• •• •• miles/hr • • " " • " • • • • • • • • miles/hr/see • • • • • • • • • miles/min • • •• ." ." mil-feet milliers milligrams milligrams/liter millihenries milliliters millimeters • • • • • " " Reprinted
by
grams megohms ohms liters feet kilometers meters miles (statute) yards centimeters feet inches kilometers meters miles (naut.) yards ems/see feet/min feet/see kms/hr kms/min knots meters/min miles/min ems/see/see feet/see/see kms/hr/sec meters/see/see ems/see feet/see kms/min miles (naut.)/min miles/hr cu inches kilograms grams parts/million henries liters centimeters feet inches kilometers meters miles mils yards permission
MULTIPLY
BY
10-6 10-12
10-6 10-6
6,076.103 1.852 1,852. 1.1508 2,025.4 1.609x 105 5,280. 6.336x 104 1.609 1,609. 0.8689 1,760. 44.70 88. 1.467 1.609 0.02682 0.8684 26.82 0.01667 44.70 1.467 1.609 0.4470 2,682. 88. 1.609 0.8684 60.0 9.425x 10-6 1,000. 0.001 1.0 0.001 0.001 0.1 3.281x 10-3 0.03937 10-6
0.001 6.214x 10-7 39.37 1.094x 10-3
of GTE AutOlllatic Electric
157 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
INTO
TO CONVERT million mils
gals/day
MULTIPLY
yards
1.54723 2.540 x 8.333 x 0.001 2.540 x 2.778 x
cu ft/min
1.5
cu ft/sec centimeters feet inches kilometers
miner's
inches
minutes
"
(angles)
" "
" "
quadrants radians seconds
myriameters
kilograms kilometers
myriawatts
kilowatts
10-3 10-5 10-8 10-5
0.01667 1.852 x 10-. 2.909 x 10-. 60.0 10.0 10.0 10.0
degrees
myriagrams
BY
N 8.686
decibels
nepers
o ohms ohms
megohms microhms
ounces
drams
10-6
106
grains
"
grams pounds ounces (troy) tons (long)
ounces (fluid)
tons (metric) cu inches
ounces (troy)
grains
"
"
liters grams ounces (avdp.)
"
pennyweights
(troy)
pounds (troy) ounces/sq
in.
pounds/sq
in.
16.0 437.5 28.349527 0.0625 0.9115 2.790 x 10-5 2.835 x 10-5 1.805 0.02957 480.0 31.1 03481 1.09714 20.0 0.08333 0.0625
p grains/U.S. gal
parts/million
" "
grains/Imp. pounds/million Reprinted
by
permission
of
GTE
0.0584 0.07016
gal gal Automatic
8.345 Electric
158 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
INTO
TO CONVERT pennyweights
"
(troy)
grains ounces (troy) grams
" pints (dry)
pounds (troy) cu inches
pints (liq.)
cu ems. cu feet' cu inches cu meters cu yards gallons liters
"
quarts
"
pounds
"
pounds (troy)
pounds of water
"
pounds of water /min
Reprinted
BY
24.0 0.05 1.55517 4.1667 x 10-3 33.60 473.2 0.01671 28.87 4.732 x 10-· 6.189 x 10-. 0.125 0.4732 0.5
13,826. grams 14.10 joules/em 1.383 x 10-3 joules/meter (newtons) 0.1383 kilograms 0.01410 pounds 0.03108 drams 256. dynes 44.4823 x 10· grains 7,000. grams 453.5924 joules/em 0.04448 joules/meter (newtons) 4.448 kilograms 0.4536 ounces 16.0 ounces (troy) 14.5833 poundals 32.17 pounds (troy) 1.21528 tons (short) 0.0005 grains 5,760. grams 373.24177 ounces (avdp.) 13.1657 ounces (troy) 12.0 pennyweights (troy) 240.0 pounds (avdp.) 0.822857 tons (long) 3.6735 x 10-· tons (metric) 3.7324 x 10-· tons (short) 4.1143 x 10-· cu feet 0.01602 cu inches 27.68 gallons 0.1198 cu ft/sec 2.670 x 10-· em-dynes 1.356 x 10' em-grams 13,825. meter-kgs 0.1383 dynes
poundals
pound-feet
(liq.)
MULTIPLY
by permission
of GTE Automatic
Electric
159 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
" """"""
nds/cu nds/sq nds/in. nds/ft unds/mil-foot ftin.
" " CONVERT " pounds/mil-foot TO feet of of water 703.1 144.0 INTO 09.425 20.06804 .01602 .307 106 178.6 1.488 2.306 4.725 MULTIPLY BYem 16.02 27.68 2.768 0.01414 4.882 2.036 5.787 0.01602 5.456 6.944 xx em 10~ 10-~ 10-9 10-6 10-3 pounds/cu pounds/mil-foot pounds/cu kgs/cu inches pounds/sq kgs/sq meter 1,728. ftatmospheres grams/cu mercury in. ft kgs/meter gms/cm gms/cu kgs/sq kgs/cumeter meter
pounds/cu ft
Q quadrants (angle)
quarts (dry) quarts (liq.)
degrees minutes radians seconds cu inches cu ems cu feet cu inches cu meters cu yards gallons liters
90.0 5,400.0 1.571 3.24 x 105 67.20 946.4 0.03342 57.75 9.464 x 10-~ 1.238 x 10-3 0.25 0.9463
R radians
degrees minutes quadrants seconds
radians/see Reprinted
2.063 x 105
degrees/see revolutions/min by permission
of
57.30 3,438. 0.6366
GTE Automatic
57.30 9.549 Electric
160 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
" " " ds olutions olutions/min/min olutions/min olutions/see volutions/see/see ans/see/see
•" revs/see/see 6.0 feet 16.5 2.778 0.1047 1.745 4.0BYxsee 573.0 360.0 60.0 INTO 6.283 0.01667 9.549 10-3 10-4 TO"" "revs/see/see CONVERT MUL TIPL Y 0.1592 degrees degrees/ revs/min/min revs/min/sec revs/see 3,600.0 radians/see/see degrees/see revs/min/min revolutions/see radians radians/see revs/min/sec revs/min revs/min/sec quadrants radians/see
radians/see
s seconds (angle)
"
"
square centimeters
"
square feet
" "
" " square inches
"
Reprinted
degrees minutes quadrants radians circular mils sq feet sq inches sq meters sq miles sq millimeters sq yards acres circular mils sq cms sq inches sq meters sq miles sq millimeters sq yards circular mils sq ems sq feet sq millimeters
by permission
of GTE Automatic
2.778 x 10-4 0.01667 3.087 x 10-6 4.848 x 10-6 1.973 x 105 1.076 x 10-3 0.1550 0.0001 3.861 x 10-11 100.0 1.196 x 10-4 2.296 x 10-5 1.833 x 10e 929.0 144.0 0.09290 3.587 x lO-e 9.290 x 104 0.1111 1.273 x 106 6.452 6.944 x 10-3 645.2 Electric
161
Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
MULTIPLY BY
INTO
TO CONVERT
10·
square inches
sq mils
square kilometers
sq yards acres
"
7.716
10.76 x 10.
sq ft sq inches
1.550
sq meters
10· 0.3861 2.471 x 10-4
1.196 x 10. 104 10.76
sq inches
1,550. 3.861 x 10-7
sq miles
10·
sq millimeters
1.196
sq yards acres
640.0 27.88 x 10·
sq feet sq kms
2.590
sq meters
2.590 x 10· 3.098 x 10·
sq yards circular mils
1,973. 0.01
sq cms
square mils
" square yards
" "
sq feet
1.076 x 10-5
sq inches circular mils
1.550 x 10-3
sq cms
6.452 x 10-·
sq inches acres
2.066 x 10-4
1.273
10-·
sq cms
8,361.
9.0
sq feet
1,296. 0.8361
sq inches
"
sq meters
u
109
sq yards acres sq feet
square millimeters
X
sq miles
sq cms
square miles
10-4
1010
sq cms
square meters
X
247.1
sq miles
3.228 x 10-7
sq millimeters
8.361
X
105
T temperature (OC) +273
absolute
temperature
temperature
(OC)
(OC)
1.0
1.8
(OF)
+17.78
temperature (OF)
temperature
absolute
temperature
1.0
(OF)
+460
temperature
(F) -
tons (long) R~printed
32
temperature
by
permission
of GTE
5/9
(OC)
kilograms
1,016. Automatic
Electric
162 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
"
"•""" """" "
" "of " (metric) tons (short) (short) /sq ft /24 hrs water tons (long)
32,000. 907.1848 1.120 MUL INTO Y BYmeter 83.333 0.16643 1.3349 0.89287 0.9078 2,240. pounds tons tons TIPL (metric) 29,166.66 (short) 1,000. kilograms gallons/min cu ft/hr pounds/sq pounds2,205. (long) in. 9,765. 2,000. 2,430.56 kgs/sq of water /hr
ounces pounds(troy) pounds ounces (troy) TO CONVERT W
watts
• watt-hours ." ." • " ." ." ." ." webera • webers/sq in. • "" • "" • "" webers/sq meter • "" • "" • ". Reprinted
Btu/hr Btu/min ergs/see foot-Ibs/min foot-Ibs/sec horsepower horsepower (metric) kg-calories/min kilowatts Btu ergs foot-pounds gram-calories horsepower-hrs kilogram-calories kilogram-meters kilowatt-hrs maxwells kilolines gausses lines/sq in. webers/sq cm webers/sq meter gausses Iines/sQ in. webers/sq cm webera/sq in.
by permission
of
GTE Automatic
3.413 0.05688 107
44.27 0.7378 1.341 x 10-3 1.360 x 10-3 0.01433 0.001 3.413 3.60 x 1010 2,656. 859.85 1.341 x 10-3 0.8598 367.2 0.001 10' 10' 1.550 x 107 108
0.1550 1,550.
10. 6.452 x
10'4
10-4
6.452 x 10-4 tlectric
163 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
"
914.4 91 36.0 9.144 0.9144 4.937 5.682 3.0 .44 TO CONVERT MULTIPLY millimeters INTO BYx centimeters
10-4
meters inches feet kilometers miles (naut.) (stat.) yards
Y
Reprinted
by permission
of
GTE Automatic
Electric
164 Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
Torque wrench with various adapters. NOTI WHEN USING A TOIOO£ WIENCH "DAnu WHICH CHANGES THE DISTANCE flOM THE TOlQUf. WlfNCH OliVE TO THE ADAPTER fOLLOWING fORMULAS TOIQUE
OliVE •.•• "" Y THE TO OITAIN THE COllECTED
READING
Short Open End Ada.pter HANDCtI' CINrllLINf IPIIDfTIIMINIDI
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M
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T
=
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=
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I
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t~~ =
FOUUA lXAMPlI, T
= 135
y
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L
1.1.
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(WTIH "I"
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=
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15•.• 2
lfGfHD T = ACTUAl IDf$lllfDl TOIQUI Y = ""AlENT PNDICATIDI TOIQUI L = IPffCTIVE LINGTH UVfI I = ImCTIVI UNGTH 0# EXTENSION
Spanner Wrench Adapter
165
Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
Aluminum Steel Aluminum Steel Tension Shear Tension Shea.r Steel Shear AN NAS 3100 3650 363 310 315 320 1022 NAS AN NAS AN AN AN NAS 3200 3640 320 364 17826 10220 365 10210 364 1022 MS M8 MS 20364 17825 20364 17826
021NUTS 825 046 27039
MS NAS24694 21045 20365 20500 679NK9 AN MS 509 525 NK525
NASj64 BOLTS
I
Steel 644 shear Steel Tension Aluminum BOLTS NUTS BOLTS NUTS N MS AS 20004 624 583 144 thru thru NAS MS AS 20024 590 158 1303 NAS 1320bolt AN MS 300 270390 5250 50900 333 thru ANN 2000 340 20365 1021 NAS 2469400 517 172 174 17300 AN 18600 MS NAS N AS 21045 679 1291
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J"INE 1 ••rl.EAD b",rl.IES
---
--------------5 In.-Ibs. Mu. M Mu. Min. M••. Mu. M••. Min. ••. tn.-Ibs. In.-lb •.L1m1tB 420 In.·lbs. 15 Min. 7 Torque -14 ------103 110 280 410 270 290 30 110 230 670 580 550 380 12 45 25 65 40 120 180 160 10 100 20 25 45 75 200 60 95 400 630 450 520 770 300 410 780 9;;0 500 600 800 1 150 5 250 4 85 70 140 190 170 260 550 950 30 690 6 90 880 145 80 3 360 70 120 660 480 950 50 70 750 5 0 4 480 800 100 750 650 60 50 20 Torque Torque Torque Limite Llml'-' Limits 9 15 12 160 50 Limits 1,250 1,250 1,500 1,200 1,900 I,300 3,200 2, 11,000 5,600 2,200 3,.000 1,250 4,500 3,550 4,200 1,300 1,500 3,300 1,900 2,600 4, 13,400 6,000 4,400 6,600 2,000 1,550 1,600 2,700 2,100 5,500 3,600 6,600 350 3,700 1,000 I,100 2,400 1,500 3,900 2,300 2,500 1,600 2,300 2,650 5,400 2,500 1,800 7,000 8,000 3,200 3,000 9,000 3,650 7,300 5,000 I,100
In.-lbo.
Min. T°"l~.~l;.~t'-'
0....•
COARSE THREAD SERIES -------------. ---------------------------------------------- --- -------. ---'-..• -------------------------24 ---------------------83,700 --------------12 240 300 420 25 110 140 420 95 1 25 290 540 3 155 480 900 950 50 5 255 700 185 20 700 5 0700 40 80 -32 7 15 9 12 400 48 90 235 160 500 3,300 1,600 1,800 6,500 2,200 4,000 1,300 I,150 4,000 3,000 5,000 8,000 2,200 5,500 6,500 8
Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
~ill~lJrn~rn[lli ~[IDrn~lJ~~~©illlJ~®~ -
courtesy of
Rockwell International
Aircraft Technical Book Company
800-780-4115
www.actechbooks.com
INSERT BLIND NG TRUCT S DNSTRUCT CK THREADED
FASTENER SPECIFICATIONS NO. PANel
FASTENERSFASTENERS IHISHEAR)
SPECIFICA nON 01L002HOI 01L013H·Ol 01L008HOI 1L005HO lL009H03 1L009H02 LA0101005 LAO LA0101019 LAD101019 LAD101018 10 1NO. 1005 1·0 10 02 17 1 14 01L003HOI o 01 01L009H01 01L001 01L007H01 01L004H·Ol 01L010H02 01L007H02 01L011HOI 01L010HOl 1L00 L002H02 LA0101016 LA010l016 ST0101LAOO02 ST0101LA002 LA010l·014 ST0101LAOOOl 1HO H02 1& 1020 03 MPP ST0101LA~003
FASTENERS
MAXIMUM
SPEEDS (HAND·FED OPERATIONS)
7/16 15/32 1/2 .r Less Less 2500 2250 1750 1700 2100 1900 2000 2300 3000 25/64 9/64 3/32 FRACTION TITANIUM 1000 STACK 1200 120 STE 1600 5300 SFMI E L UP 15/64 7/32 17/64 13/64 1/4 5/16 3/8 5/32 3/16 11/64 250 200 350 300 160 400 450 500 or 800 700 or 1400 or 1500 2650 1850 2850 3200 4300 3900 4800 6100 or 7000 .r.r less less less Less 13/32 5/64 1/16 1500 180 175 130 600 900 STACK 1BOO 280 250 240 or 10700 or 8500 Less SFMI less UP ALUMINUM 9/32 19/64 7/64 1/8 21/64 23/64.r 11/32 1200 1000 400 550 450 600 500 350 650 800 750 .r 3600 Less 1175 150 300 1300 230 DRILL SIZE
ST ACKUP
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BLUEPRINT
FASTENER
CALLOUTS
Basic Code letters
Ir---r
1
Dash Head No. for Diameter Mfd Farside (See (See NoteNote 2) 1)
$pL
3 Required
D2
Flush Riveting Operations
64 F
(See Note 3)...-J
Dash No. for length
or Grip
(See Notes 4 and 6)
NOTES:
1. Dash numbers for fastener shank diameter are obtained from fastener drawings. 2.
The location of the manufactured
(preformed) head of the fastener
is defined
by the code letter "F" (for far side) or "N" (for near side). When the code letter is omitted. the location of the head is understood side. but may be interpreted 3.
to be on the near
as optional.
Flush riveting operations:
(Sheets are numbered
from Mfd head)
DC D Dimple Countersink D2C SheetSheets 1 Sheet Sheet 1;1. 1 Sub·countersink and 2; C3; D3C Dimple 2.1 and D3D2 Dimple DimpleSheets Sheets1.1.2. 12,and 234 D4 Sheet 3.and and
Sheet 2 Sub·countersink
4.
Sheet 34
Dash numbers for length or grip are obtlined epply to III flltlnerl
5.
National Aarosplca thosl
Itandard
from fasten"
Irl IVlnlbl1
NAS523 is thl blsis
Codas for preferred
parts
drlwingl
and
rivets. for thl fastlnlr
codas Ihown on NAS523 shall ba uSld. Improvised
prohibited.
B.
except conventionll
Irl reproduced
cadiS
coda. Only arl
herlln.
Addltionll
cod.
numblr
thlt reprnantl
Ind new cod •• can bl .tlbUlhad.
Thl Itngth II Ihown
by I number which II the dllh
thl length In the fuU Plrt number.
3 Aircraft Technical Book Company
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YH ZF ZS ZH ZK AAW AAR AKO ZV ZL 22 XD XA XB RS TO AKW CODE ABE ABH ACN ACD CODE AKV XG AJN XF TV 27 22 12 239 25 PAGE 24 259 26 24 10 27 PAGE 15 23 1 20 19 23 25 16 24 26 27 14 21 1 6 8 1 7 6 531 TM TK TN TR XC RP RR SH TP TL AJW AKF AKB AKR AKA AKK ADB AKP XH AKY RN RO XJ AJV TS ADF XE 26 ALF 24 14 27 258 10 16 237 15 22 11 12 11 12 9 18 7 17 10 9 7 13 11 14 BASIC NO. PAGE NO. NO. AKD AKM AKC AKE AKH AKN AKS AKJ AKX AKL ADJ 10 26 AEJ AEK AFP AFY AJF AJL AJH AJM BASIC !
BASIC ALPHABETICAL
CODE LISTING
PAGE
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AST CODE CODE BASIC PAGE PAGE NO. NO. ASY ASU ASM ASL AMT YAB YAC YAD ASZ YAE AT ATB YAG YAH YAF ATC ATG ATD ATE ATF 21 20 25 22 24 29 19 14 21 2 28 25 17 23 2 15 A 19 BASIC PAGE NO. AMX APM APN AMP AMY ASJ AMO APK ASH ATH YAA ANE APL APJ YAJ 16 14 12 13 28 16 10 18 12 13 23 15 1 25 17 97 7
ALPHABETICAL
CODE LISTING
BASIC
USE OF INDEX
Locate desired code alphabetically. Page No. of code on which fastener is found is located adjacent to it.
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G" .•••.••• " •• HHOWI ••••O
SUf
H ) I ADW
..Dfu
IIECE55
0.'" Jl ••.••• (,1t"'6,'" , I
AKR
SELF AlIGNINGGIIIA'"
HI)
NUT-HL89DU-t,
AKO
LEI14-0032-()
GII'. "'M
:~.O~:j
NA 203
ti
..
GilA"
~"OW:;114_0035
23
Aircraft Technical Book Company
800-780-4115
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~.
ADW
!lfCns
"fCfSS
GII"''' liED
01"'32_ HI-LOK BOLTS DlA'J2n6a\~ 0I••·J2•.••••
01 •••31 ••••• 01 •••32 •••••
GfIIP1111'''. Gill' 11••••
PIN-HL645lt(' )-(")."" PIN-HL 11~.'(~-( 0IA32_1 I,'" " ..
I
~. ~.
." '".. ".."
d
G~ op[JIIQ ~Q~ [t1rn Q[t=D[1© [ill nUJ§ 00 00 [ID O~ [JB ".
Sfll,UIGfiHNG -NUMBER SfLFAUO...-.o ""SElf PIN-HL645LL-( PIN-HL41-( Gl'If'I''''' H )HI) '" 'A,nGRAY "" ''':~' GIIAY AUQNfNG SElf GRAY ALIGNING Rfcns PART SHfAliGNIHG TORQUE CONTROL TOOLING REQUIRED IDENTIFICATION AL TERN AGRAY TEGRAY (114-0032 .. '\ '''''''/110 SELf IIECUS AlIG"'ING friO '..,IITNO ''''''',,",0 HEAD ~.'_.~I 1111HEX LE nmJ!ij I LE114-0030 COUNTERSUNK LE 114-0034 114-0033-( I I ADW NUT-HL70-( )) ADW NUT-HL82-( NUT-HL175DU-( LE114-0032 mOO LE GII"'II•••• DI""~2_ ,/, 011"' ••••• NUT-HL97DJ-( ) NUT-HL94~.~:1 ) a'''LE114_0036_( )
/
OUr.-~Z"""
/
P,I.IIITI\IO~,
~Q []§ "6dCi
::~u~cJ©
COUNTERBORE HEX NUT
LE114-0036
[JB
NA 202
24 Aircraft Technical Book Company
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COUNTERSUNK
HI-LOK BOLTS BASIC CODE
PART
COUNTERSUNK
ASM
I PIN-Hl233-(
H
ALTERNATE
HEAD
COUNTERBDRE HEX NUT TORQUE CONTROL TOOLING REQUIRED
IDENTIFICATION
NUMBER
HEAO
GRAY
NONE
I
! AW
NUT-Hl584-(
""
SelF
ALIGNING
I
SELF ALIGNING
RECESS
ALV
!
I PIN-Hl4 H H NUT-Hl185DU-(
/
DIAJ2nd.
GlltP'6
\
AMB
I PIN-Hl227-(
RfCHS
I
lE 114-0032 -(
!
GRAY
RECESS
NONE
cnfd "" RECESS
H ) I )
I PIN-Hl647ll-{ NUT-Hl89DU-(
0"
0
[C:U
GRAY WITH YHlDW 8,U~D
GRAY VHlDWBANO
G:J© I [ID
""
I H)
[Jg H()( RECESS
jGAIPI6t".
lE114-003H)
SELF AliGNING GRAY, YEllOW
IUCESS
) ADW
GRAY YEllOW
GR"" WIT'" YEllOWBA"'O
BAND
lEl14-0035-() 8ANO
H)
PIN-H113V-( NUT-Hl73DY-(
)
0' Hl73DU(
)
Q'''J2nd.
NUT-Hl89DU-(
""
GRIP,16''''
I PIN-Hl6471l-( NUT-Hl73DY-( 0' Hl73DU-(
PIN-Hl13V-(
lEl14-0037-(
G"AY
D®100
) AW
otAni'
AKS
""
I
\
AKP
[ID'"
QIIIfd
•••••
H )
DIA31nd.""
AKN
\
,_••_ I ', .•••. ()-D
!
NUT-Hl584-(
AKB
Dt.
H )
I PIN-Hl11V-{ NUT-Hl94DU-(
\ ASL
,." I ADW
\
i
GRIP'6,,,,
H
o"UP
CI© [ID I
lEl14-003H
I
I ADW
NA 204
25 Aircraft Technical Book Company
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\\ D BOLTS OIA·16ths DIA·32nds
DIA-16ths
/
//NAS MS21141-( 1669(( )K( NAS1671( NAS 1669( 1671 )l(H ))) CLASS 21 CODE CODE GRIP·16ths GRIP NO 1 6th5 GRlp·16thG GRIP·
ID
lOCK
CODElOCK
CODE MECHANICAL MECHANICAL MAT'l PART NUMBER
CODE
@~ ~-P=D CODE
USE AKX
MFRSID
IDENTIFICA INACTIVE TION FOR DESIGN
((Q) ~
PROTRUDING
HEADS
MFRS MFRS
~
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BASIC CODE
PART NUMBER
ZK
I NAS 1670(
IK(
I
ZL
I NAS1672(
IK(
I
OIA-16ths
~
IDENTIFICA TION
INACTIVE
FOR DESIGN
USE AKV
INACTIVE
FOR DESIGN
USE AKW
CLASS CODE
GRIP·16ths
/
\ AKV
/,R
BLIND BOLTS
COUNTERSUNK HEADS
MECHANICAL LOCK CODE
Il( I
I NAS 1670(
MFR$ ID
DIA- 1 6ths
CRES
MFRS ID
/
\ AKW I NAS 1672(
"C"
GRIP·16ths
IL(
I GRIP NO
DIA-32nds
\ TV
I MS90353-(
GRIP·16ths
/ HI
MArl
MFAS
CODE
10
GRIP
NO OIA·32nds
\ ACO
I MS21140·(
GRIP·16ths
MAT'l CODE
/ H I
MFAS 10
(@ GRIP NO
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-.0 O~ [I] [JJ -901 ID9U O~ O[]=m!,9 [I O[ OW ,, PIN-TLV400IJI IE PART NUMBER
10 MFRS 10 ID 10
liHW GRIP·16ths lbths ISEE NOTE NOTE BELOW) SHOWI WASHER NUT NUT SElF·AlIGNING SELF ALIGNING WASHER NUT GRIP-16ths \\ WASHER WASHER NUT (SEE 10 CODE WASHER NUT ISEE NOTE !D ID CODE CODE ISHIDENTIFICA NOTE BELOW) BELOW)
\ ID CODE 10 10 CODE CODE \ (ISEE SEE NOTE BELOW BelOW) I NOTE OIA-16ths ID oror OIA MFRS OIA((32nds DIA·16ths MFRS 32nds GRIP-16ths when preceded "0") ))(32nds w~~~'~~et::d~~by "0") MFRS MFAS when preceded by by "0" "0" CODE GRIP·16ths GRlp·16ths A-16ths or GRIP·16ths //// GRlp·'6ths GRlp·'6ths GRIP 16th, ~'~~e~:d~~ by "0") (32nds W~~~'~~et~:d~~ by "0" ) MFAS
CPOI( II H IE OPOI( ER-LOK 001 PIN-TL04001 H H IE IE BOLTS F00( A OIAOIA OIA OIA
lIJIO
NUT-TLN 1021 CPOII ~ JIillIDO NUT-TLN 1024 1010 1001 OPOIA( CPOI( CPOI( III I
TION
/
GRIP·16ths HEADS // PROTRUDING
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---
MFAS
MFAS
OP
H )E
-.0 O~
PIN-TlV-300l(
GRIP 16ths IC WASHER NUTNUT 14 FOR Tl4QOJ WASHER Ie 4CODE 01 4-DIA-16Ihs -NOTE 32nds SERIES when (SEE NOTE BElOW! ( SEE NOTE preceded BHOW byNUMBER "0·· ' IC ID ID CODE WASHER NUT IDENTIFICA (SEE PART BElOW IDCODE H TL-- MA LOK CIA lTlH HRIAl MFRS 2TAPER EXCEPT GROUP (EXCEPT 046 051 -16ths 11 ••••. OIA orpreceded CIA GRIp· 1 6!hs (32ndS when . ·0" ) (32nds hen preceded by "0") CODE GRIP·16ths
PIN-TlO-300l( 0 I CPOI( ) BOLTS GAIP-16thsH )E (32nds ER-LOK CIA
w~~~-~~t~:d~~
by "0'"
)
/
0 [I]JITWo[i]
NUT-TlN 1010 1001 CPOI( ) OPOI( ~ NOTE
IDENTIFICATION
CODE
TION
/
GRIP 16ths
HEADS COUNTERSUNK
GRIP 16th!.
29
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LOCKHOLTS, HI·LOKS, HI·METAL RIVETS CODE:
AJH, AMP, AJF, AMO, AKC, AMN, AFP, AJL, AEK,AJV, AMO, AFY,AJM, AEJ, AJW, AME, NO, ABE, AKH,AKK,
~~M~~~~~~m~~~~~~~~~~ AKB, AKN,AKP, AKS
Trans
0.1662 Fit II 114 3116
SHANK 0.168 0.1850 0.2450 0.2510 0.1590 0.1910 IV IVA III IVA
I
STANDARD HOLE Hole Io.11 0.2041 0.1900.26560.2227 0.1900 0.2500,1640.16400.19000.25000.1625 0.25000.2485 0.1900 0.1885 0.1650 0.2500 0.2410 0.1910mm 0.1620 Reamer 0.16100.2470 Reamer 0.21870.21570.1640 0.27820.2209 0.2812 0.2197 Size Drill 0.2678 Size 0.2782 0.2834 0.2626 0.2656 0.2157 Size NI.21 N NI.11 4.75 4.2 mm E 20 21 0.20010.20310.262610.1770) 0.2071 0.18800.1870 0.2500 (0.25201 10.2500) 10.2050) (0.2660) 10.26801 0.2187 10.19201 0.2812 0.2852 0.2470 No. 0.2031 0.2001 Hole 15164 1ID /4Drill) 24 16 0.2656 SECOND 10.1520) 0.2656 FIRST OVERSIZE 0.2696 OVERSIZE (Pilot! IPilot) 0.2031 IPilotl (0.2520) (0.26801 0.2053 10.2040) (0.19201 (0.1910) 3116 10.2340) Spec Size TYPE NOMINAL IV
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118
CONVENTIONAL CODE:
BH, BJ, BK, CX,
n, LN, SH,
RIVETS AND STANDARD
MM, XC, XF, AMY, XJ, BA, BB, BC, CY, BF, MN, MC, MO, XB, XE, AM X, XH, XA, XO,
ANE, XG, LZ, MA, AW, RK, RL, RM, RN, TK,
0.132 0.101 5132
SHANK 0.261 0.164 0.196
BLIND RIVETS
n, TM,
TN, AKE, APM, ASJ, ZV, AST, RH, ZS, ASU, AOF, AMT, AV,
RO, RP,RR,RS,TO,TP,TR,TS, ASH,AKO,APL,AKF,APN,ACN,ACO 0.0970.128Reamer Hole D,iII Hole 3 .25 Hole I I TYPE 0.1590.1900.256-6.5 (Standa,d Reame, Size No. No.11 2mm .45 Size 21 Disposition SECOND FIRST Manuall OVERSIZE OVERSIZE Fo, (Pilot) blind conventional ,ivots, uso ,ivots, bulbod uso blind SDM ,ivots fo, HOLE ovo,sizo fo, 1st data. O.S. STANDARD HOLE DIA (Inches)
3/16 1/4
BULBED BLIND RIVETS CODE:
SHANK 0.209 0.180 0.146
AAR,AAW,ADB,ADJ,AJN,ALP,APJ,APK,AST,RH,ZV
I
DIA (lnchosl
TYPE Holo 0.1430.1760.205Sizo Holo Roamo, D,iII No. No.5 Holo Sizo 27 I16 I (Pilot) (Pilotl HOLE
SECOND FIRST OVERSIZE OVERSIZE STANDARD
HOLE
5132 3116
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THREADED
3/16
0.1662 7/16 3/8 1/2
II
SHANK 0.5022 0.4425 0.505 0.379 0.3772 0.3147 0.4397 0.3165 0.168
FASTENERS
STANDARD HOLE Hole Reamer Reamer 0.2812 0.28120.2834 Drill Size 0.2187 Size Hole mm IE 24 0.2071 0.2696 IPilotl Size 0.190-No.11 0.3125-5/16 0.3750.43750.5000.1640.2500.16400.25000.31250.37500.43750.5000-112 0.19000.21870.2500 0.20310.2209 0.2227 0.2852 0.26560.1900 0.1640 0.2053 0.2678 10.26801 0.28120.2812 No. 0.2031 0.2656 I3/8 16 0.2656 SECOND 0.203110.1520) FIRST OVERSIZE OVERSIZE (Pilot) (Pilotl (0.2520) (0.19201 (0.2050) (0.1920) 10.2520) 10.20501 10.2680) 15/64 7/16 74.2 5 318 1/2 /16 116 (0.17701 (0.23401 Size TYPE
II
NOMINAL
II
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INTERNAL
THREADED
BLIND BOLTS
(JO-BOL TS AND HUCK BOLTS)
PART NAS MS21141 1671 1672 1670 1669 MS21140 MS90353 Huck Blind Flush Bolt Protruding General·Purpose Jo·Bolt to 450 High·Temp Flush Head Head Protruding Flush Jo·Bolt Head Head Jo·Bolt Huck (Up Huck Bolts to(Up 12000F) Bolts 450 FI Protruding Jo Bolt to(Up 12000FI DESCRIPTION
°
NO. TV AK, ACN,ZK ACO, ZH, AKW AKY AKV ZL AL,
°F)
CODE ZF, AKX
DIA {lnchesl -6L ·12 Drill ·4L ·08 ·08L ·10 ·5L Huck STANDARD SECDND FIRST HOLE DVERSIZE DVERSIZE 3/B 5/16 0.375Size Hole 0.2140 G Reamer O.IBOSize No.8 No. .275·06 O.IBO 0.214 0.275 ·3L ·05 Size Hole 0.1990.2600.1650.312DASH 19 NOMINAL 0.183 0.217 0.278 SHANK NO. (0.375) (Pilot) (Pilotl (0.16BI (0.202) (0.2631 (0.260) (0.1641 (0.3121 (0.200) FASTENER Hole Size 0.168 0.202 0.263
0.315 0.37B
31B
NOTES:
(1) Piloted reamer required
(2) Double margin drills
where drill guide is not used.
may be used in lieu of drill·ream
(3) For hole types of transition thickness
operations
fit, Types IV and IVA. In aluminum
must be two times the hole diameter
for Type II holes. Drill guides must be used.
stackups
(only) the maximum
material
(nominall.
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TIPS
FOR GOOD DUALITY
HOLES
1. Select a drill/reamer that will provide a high quality hole at the low end of the tolerance
range.
2. Use a drill guide. 3. Ensure good clamp·up of material 4.
during drill/reamer
operations.
Use Boelube on final ream.
5. Ream to size using low feed rate and slow speed. 6. Carefully continue turning reamer while withdrawing flute lines (marks) in the hole. TRANSITION·FIT
Transition
it from the hole to avoid
HOLE PROCEPURE
holes should be used in place of Type II FIF holes in all areas
(except cold·
worked holes) when Hi·Loks, Bi·Metals or Lockbolts are called out.
DRilLING 1. After parts are located, drill pilot holes (using drill guide) and cleco parts together. 2. Step hole size up. 3. Using core drill or piloted reamer and Boelube, ream hole to final size within tolerance shown. 4. Cleanly deburr hole. 5. Visually examine hole surface
finish (125 RHR for aluminum stack up, 63 RHR for
all other metal stackups). 6. Have the hole inspected. 7. Apply blueprint hole finish. FASTENER B. Tap fastener
in hole until head seats
INSTAllATION using a non·metallic
mallet or aluminum drift
punch while using a backup on the structure. CAUTION: Do not pull the fastener 9. Install the collar/nut NOTE:
into the hole using the collars/nuts.
and ensure fastener
Spinning of fastener
does not spin during installation.
may cause galling and be cause for rejection.
FASTENER
REMOVAL
1. Remove collar/nut. 2. Support structure
from head side and use an aluminum drift to tap fastener
out of
hole.
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COMMON
Primer Areas (Fuel Tanks Only) er Than Other ThanFuel FuelTanks) Tanks) Fuel Tanks Only)
COOE Wet Chem-Film, with Primer Sealant Install Fastener Fastener Wet with Primer Sealant Install Wet Fastener Sealant Film, Prime Hole and Dry, (Head Only) Dry with with Sealant (Head Only) Dry Install Fastener Dry
BLUEPRINT
FINISH
CODES
FINISH REOUIREMENT Install Fastener Wet with Clean, Bruch ChemBrush Chem· Clean, Brush Install Solvent Clean,
35
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rn~rn©Tfrn~©ill~ ©®~~rn©Tf®rn u[]Jrn~Tf~~~©illTf~®~
courtesy of
McDonnell Douglas
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Contacts for Front Release Connectors TYPICAL CALLOUTS:
DC26 10-6 ConnectorS Style
Endbell (Backshelll Insert Contact Clocking Sex DesignatorDesignator
Shell
1.
FVF6E14S-7PX
FVF6X P 14S-7
Designator
Size and Layout
OC26F1G-6S
Designator
In the fronf release contact
connector
fami-
lies, the contacts may be of either the pin or socket variety, so the contact sex designator must be noted. 2.
The shell size and layout designator determine the number and size of contacts. In the examples listed above, the 14S-7P arrangement contains 3 size 16 pin contacts, PIN 030-1878-001, Term Code 1009 (see page 6). Th3 lO-BS arrangement contains 6 size 20 socket contacts, PIN S00023-20S, Term Code 702 (see page 10) NOTES Contact size refers to the mating size and the wire barrel size of the contact. (For example, a 16-20 contact has a 16 mating size and a 20 wire barrel size.) A contact size containing only one number implies that the mating size and the wire barrel size are the same. (Hence, 16 equates to 16-16) Approved equivalent vendor proprietary part numbers are included at the end of each section These may also be found in DPS 1.834-40.2.
3.
Endbell (Backshell) Designators: Class A: Grommet seal, conduit adapter Class E: Grommet seal Class F: Grommet seal, strain relief clamp Class L: Grommet seal, 90-degree strain relief clamp
1
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1S·
FZ & FV Electrical Connectors (EMPLOYING DOUGLAS
FRONT DRAWING
RELEASE CONTACTS. 7913200,
CONNECTORS
ANO INTERMATEABLE
FVFO IFRFO, FZCO, FRAO, FVAO, FFRO, CAVOI PLUG CONNECTORS FVF6 IFRF6, FZC6, FRA6, FVA6, FFR6, FZH6, CAV61
1009 1057 1013 1058 16 12 16 816 030-1878-001 o:JO..1878'()()1 030-1878.()()6 030-1878-007 o:JO..1878-001 030-1880'()()1 o:JO..l878-001 0030-1878'()()1 030-1879-003 30-1880-001 (CHROMELI IALUMELI 031-1040'()()1 031-1040.()() 031-11J4O.001 031-1040.()()1 031-1 031-1041-003 19 32 7 51 8 1J4O.00 1 ICHROMELI lOSL-3P 1015 031-1040.()()4 031-11J4O.003IALUMELI 14 3 031-1042-001 5
ARE TO THE REQUIREMENTS THREADED
PIN CONTACTS
RECEPTACLE CONNECTORS
24-10S 22-14S 20-175 2O-27S 10SL-3S 14S-7S 145-9S 16S-1S 1 ZO-7S 22-2S 10SL-4S 12S-3S 16S-8S
WITH
• •
MIL-C-5015
OF
CONNECTORS)
SOCKET CONTACTS
• •
1016 1010 1014 1058 1060
2 Dovgias
Se/~lCeSpec.a1 ~rne'"
Aircraft Technical Book Company
NOvemDe(
I~
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1017 1009 1013 12 1137 16 46 18 28-11P 1019 4/0 16 0416 030-1878-001 030·1878.(J()1 030-1881.(J()1 030-1882.(J()1 030-1879-003 030-1879.()03 BAN7027-501" 03H041.()03 03H040.(J()1 03H043.(J()1 031·1 031-1041.()03 03"'040.(J()1 BAN7027·1" 37 031·1040-001 031.10«).001 234 Q44.001 28-215 28-225 28-115 36-85 46-355 3,.,5
431
"Douglas
Pa" Numbers:
1137 -
1014 1138 1020 1018 1010 BAN7027-501,
1138 -
BAN7027-1
contacts.
THE FOLLOWING
Douglas
ARE SPECIAL
APPLICATION
CONTACTS:
1007
030-1878-008
1008
031-1040-002
ITT
1011
012-0012·101
FLT
1012
012·1012-201
FLT
1027
030-1878.(J()4
ITT
1028
030-1879-003
ITT
1037
031-1040-006
ITT
1038
031-1040.(J()7
ITT
ServICe
SpeCial Suwlemenl
No~emoer
ITT
198t
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Substitutions APPROVED
EQUIVALENT
PART NUMBERS:
PIN OR TERM CODE
roar;;"
1010 1138 -
•
SOCKET
ITT CANNON
030-1~1 030-1881.001 030-1878.004 031-1041-003 030-1882.001 031·1040-007 030-1878.006 031·1040-004 031·1040-003 S 012-1008-201 000-1006-204 016-1011·207 016-0007-107 030-1878-001 030-1878-008 030-1879-003 031-1042.001 030-1878-003 030-1878.Q07 031·1040-002 031·1040-001 031·1043.001 031·1044.Q0l 031-1040-006 P 012-0000.101 008-0004-104 008-1004-204 004-1005-204 0IJ4.0005.104 000-0006-104 016-0011·107 016-0011·106 016-1011-206 016-0007·106 016-1007-207 016-1007-206 01E>-OOII·101 016-0007c 101 _ S P016-1007;201 016-1011·201 _. P 3.)8-1620-096
FLIGHT
TRI-STAR
315-4040-066' 316-4040-066"
BAN7027-1
Electrical Connectors DCOO through DC08
(EMPLOYING DOUGLAS
FRONT RELEASE DRAWING
RECEPTACLE CONNECTORS DCoo DC02 PLUG CONNECTORS DC06 DC08
CONTACTS.
7913200, AND
CONNECTORS
INTERMATEABLE
ARE TO THE REQUIREMENTS
WITH
PIN CONTACTS
THREADED
MIL·C·5015
OF
CONNECTORS)
SOCKET CONTACTS
•• ••
•• ••
4
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SHELL SIZE
ITT CANNON
AND LAYOUT DESIGNATOR
CONTACTS QTY - SIZE
IOSL-3P
16 16 2 48 7 00LRMI6M-6 LRCI6M-6 LAC16M-6 3 709LRMI6M-6 700LRMI6M-6 700LAMI6M-6 00LRM 16M-6 14 7 LACI6M-6
THE FOllOWING
ARE SPECIAL
TERM CODE
ITT CANNON
PART NUMBER (PIN CONTACTS)
TERM CODE
PART NUMBER (SOCKET CONTACTS)
710
145-7S IOSL-3S IOSL-4S 125-3S 14S-2S 20-75 2O-27S 14S-9S 165-1S
APPLICATION
CONTACTS: WIRE AND GAGE BXS700B 7t!01684 All
PIN OR TERM CODE
SOCKET
PART NUMBER
SIZE
BXS7007
607
P
lRM22M-2
16-22
24,22
606
S
lRC22M-2
16-22
24,22
707
P
lRM20M-2
16-20
OTHERS
24,22,20
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OC20 through OC28 Electrical Connectors (EMPLOYING FRONT RELEASE CONTACTS. CONNECTORS ARE TO THE REQUIREMENTS OF DOUGLAS DRAWING 7913200, AND INTERMATEABLE WITH BAYONET MIL-C-26482 CONNECTORS)
•
RECEPTACLE CONNECTORS SOCKET CONTACTS
0RS
DC26IPT06SEIIKPSE)
lG-6P 12-3S 14-19S 16-85 18-115 2o-16S 12-8S 14-5S 12-10S 14-15S 10-6S 16-26S 18-325
14 2
•
PIN CONT ACTS
(MS31261 (DTKI
20 16 16 20 705 7 16 SOOO23-20P lRMI6M-32DJ5 lRM16M-32DJ5 500023-20P 05 lRCI6M-32DJ5 SOOO23-20S SOOO23-205 500023-20S S00023-205 500023-205 32 10 19 11 8 5 3 61 701 26 37 16 16
706 706 702 702
6 DougfasSeI~lCe5Decllj/SuPOlemenINovemoer
Aircraft Technical Book Company
'986
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3
CONTACTS QTY SIZE 706 16 SOOO23-2OP 37 41 55 16 20 701 lRMI6M-32DJ5 lRMI5M-32DJ5 500023-2OP lRCI5M-32DJ5 500023-205 lRCI6M-32DJ5 500023-2OS 21
20-395 20-415 22-215 22-555
706 702
2
THE FOllOWING
ARE SPECIAL
APPLICATION
CONTACTS:
lRC20M-1 lRMI6W-2 lRM20M-1 16-22 lRM22M-1 lRCI8W-2 20-16 lRC22M-1 16-20 18,18 18,16 )8,18
P
24, ~, 22, 20 20 24,
5P
5 SP
APPROVED
701 1004 704 705
703 702
EQUIVALENT
PART NUMBERS:
lRMI6W-2 lACI8W-2 lRC20M-1 lAMI6M-32DJ5 lACI6M-32DJ5 55P P lRM2OM-1 lRC2OW-21 LRM2OW-21 316-2020-084 317-2020-084
10-330931 1().31455().16P 1()'257982-162 0007-013-000 0004-065-000 ZZl-4116-361 46-1825-02 22l-4016-361T 46-1026-02 T 1()'330932-162 1()'330933-162 1(),33093O;-202
46-100-16005-02
Douglas
$€rv,ee Special
Suppiement
Novemoor
1986
7 Aircraft Technical Book Company
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48 Series Bayonet Type Electrical Connectors (EMPLOYING MIL-C-26500,
FRONT RELEASE
CONTACTS.
AND INTERMATEABLE
WITH
CONNECTORS DC50 BAYONET PIN CONTACTS
RECEPTACLE CONNECTORS
••
48-10, ZZB-R17, MS24264RB 48-13. ZZB-R15, MS24265RB PLUG CONNECTORS
CONTACTS
DESIGNATOR OB-03P
QTY
SIZE
20 16 20 16 705 720 500023-2OP SOOO23-2OP LRM16M-32DJ5 05 500023-205 S00023-2OS 500023-2OS SOOO23-205 SOOO23-2OS 24 31 41 14 55 12 7 53 3 701 500023-20P S00023-2OP LRC16M-32DJ5 15
OF
CONNECTORS)
SOCKET CONTACTS
••
•
•
48-16. ZZB-R10, MS24265RB
SHELL SIZE ANO LAYOUT
ARE TO THE REOUIREMENTS COUPLED
TERM
PART NUMBER
CODE
(PIN CONTACTS) 706 705 702
22-555 20-415 18-315 18-14S 14-07S 14-155 OB-03S 16-24S 10-05S 12-12S 12-03S
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THE FOLLOWING
ARE SPECIAL
APPLICATION
CONTACTS:
~. ~. ~. ~. ~am
~,~,m
APPROVED
701 704 1004 705
702 703
EQUIVALENT
PART
NUMBERS:
LRM20W-21 LRC20W-21 LRM20W-1 LRC20M-1 LRMl6W-. LRC16W-2 P 55 P LRM16M·32DJ5 LRC16M-32DJ5 317-20m-084 318-2020-084
10-330-932-162 10-330-933-162 10-330930-202 10-330-931 0007-013-000 ZZL-4016"36lT ZZL-4116-36LT 10-314e80-16P 10-257982-162 0004-065-000 48-1625-02 48-1026-02
48-100-16005-02
Deutsch Electrical Connectors (EMPLOYING
FRONT RELEA5E
RECEPTACLECONNECTOR5 DSOO, DS04, 17064 PLUG CONNECTOR5 DS07, PD504, PDS07
CONTACTS) PIN CONTACTS
SOCKET CDNT ACTS
•
•
•
• 9
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SHELL SIZE AND LAYOUT DESIGNATOR
CONTACTS QTY
SIZE
TERM
PART NUMBER
TERM
PART NUMBER
CODE
(PIN CONTACTS)
CODE
(SOCKET CONTACTS)
•
12 16 7 189 187 8 800-16/32·1 800-20/32· 000· 00-20/32·1 27 37 61 12 19712 12/32·1 12130-3 I PIN CONTACTS 20 185 800-20/32-1 34762·203-2000 3 20 ·3P 800-20/32·1 20016/30-3 SOCKET CONTACTS
1116 190 189
19125 ·197S ·195 -37S ·275 -61S ·125 -35 -7S 14158-2 PLUG CONNECTOR
Boost Pump Connector (EMPLOYING
FRONT RELEASE
CONTACTS)
CONTACTS PLUG CONNECTOR J"I58-2
.
OTY
SIZE
TERM CODE
7
20
1116
III••
SOCKETCONTACTS
1
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CAOOKE through CA3106KE Electrical Connectors (EMPLOYING FRONT RELEASE CONTACTS, AND INTERMATEABLE WITH THREADED MIL-C-5015 CONNECTORS) RECEPTACLE
CONNECTORS
CAOOKE
CA3100KE PLUG CONNECTORS CA06KE CA3106KE
Douglas
Service Special
Suppi9menf
NOVfi!moor
1986
11 Aircraft Technical Book Company
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28-215 3&85 28-225
12 16 733 727 7816 31 030-1082-000 030-113&-000 031-0732'()()o 031.(J706..000 031-073J..OOO 46 37 3 030-1134-000 0 30-1082'()()o 031.(J706..000
728 734 732
31
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Contacts for Rear Release Connectors CONFORMING OF DOUGLAS
TO THE REQUIREMENTS DRAWING BAN7025
TYPICAL CALLOUT:
Connector
Endbell
Style
Size
Shell
{Material}
Contact
Insert
DC62
Designator
(Backshall)
Shell
layout
DC62E20M27SX
Designator
20
Designator
M
Designator
27
Designator
5
Sex Designator
Clocking
x
Designator
1.
With BAN7025 series connectors, the contact sex is automatically determined by the connector style. In the example shown above, DC62 always contains socket contacts.
2.
The shell size and layout designators determine the quantity and size of contacts. The arrangement noted above, 20-27, contains 14 size 16 contacts (NOTE: A contact size containing only one number implies that the contact mating size and the wire barrel size are the same. Hence. 16equates to 16-16. A number such as 16-20 indicates a 16 mating size and a 20 wire barrel size). According to the applicable list. the contacts for this connector are PIN DC65-16S. Term Code 1121 This PIN is the Douglas specification number. Approved equivalent vendor proprietary PINs are Included at the end of each section. These may also be found In DPS 1834-40.2. Connectors may contain more than one size contact. For example, the 14-15 layout of the DC30 series employs 14 size ~O contacts and one size 16 contact.
3.
4
Endbell (Backshell)
Designators:
Class E: Grommel
seal, endbell accessory
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Class F: Grommet
5.
Code J:
seal, strain relief clamp
Class L: Grommet seal. gO-degree strain relief clamp Class - (Dash): No endbell accessory The shell material designator specifies one of the following shells. Noted coupling nuts are provided with plugs only Code - (Dash) Aluminum shell, conductive electroless nickel, hex non locking coupling nut; for plug or receptacle use
Aluminum
shell. conductive
elec-
troless nickel. self-locking coupling nut; for plug use only. Code M Steel shell, cadmium, hex nonlocking coupling nut; for plug or receptacle and firewall use only, NOTE
Receptacles coded as .oj' shells are intercl1angeable with those coded as "-" shells and receplacles coded as .oK' shells are Interchangeable with those coded as .oM" sl1ells
Code K: Steel shell. cadmium, self-locking coupling nut; for plug and firewall use only.
DC 30 through DC 37 Electrical Connectors IEMPLOYING
REAR RELEASE
CONTACTS.
TO THE REQUIREMENTS OF DOUGLAS AND INTERMATEABLE WITH BAYONET
CONNECTORS
ARE
DRAWING BAN7025, MIL-C-26482 CONNECTORS)
II
II
PIN CONTACTS RECEPTACLE CONNECTORS SOCKET CO NT ACTS
OC35 C31 OC33 OC37 0C30
OC34 0C32 PLUG CONNECTORS
OC36
10-6
16 20 16 1 1131 1126 1126OC38-20P 131 126OC38-20P 126DC38-2OP DC38-16P OC38-2OP 19 OC39-16S DC39-16S OC39-2OS DC39-20S 6 3 DC35-2OS 1123 20 1126OC38-2OP 14 10 OC39-20S 85 1124
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SHELL SIZE AND LAYOUT
CONTACTS
DESIGNATOR
OTY
SIZE
TERM
lIT CANNON PART NUMBER
TERM
lIT CANNON PART NUMBER
CODE
(PIN CONTACTS)
CODE
(SOCKET CONTACTSI
1e.8 1131 16 1126OC38-2OP 20 1126DC38-2OP 11 37 41 55 DC39-2OS DC39-20S 8 1124 16 1126 DC38-16P DC39-16P DC38-2OP DC39-2OP 26 21 16 DC39-16S 1123 32
APPROVED
EQUIVALENT
TERM
PIN OR
CODE
SOCKET
PART NUMBERS:
MATRIX DOUGLAS
SCIENCE
TRI-STAR
lIT CANNON
BURNDY
~
1123 1124
S
1126
P
1131
P
,REC2OW4DJ5
OC50 through OC57 Electrical Connectors (EMPLOYING
REAR RELEASE
CONTACTS.
CONNECTORS
ARE TO THE REQUIREMENTS
OF DOUGLAS DRAWING BAN7025, AND INTERMATEABLE WITH MIL-C-B3723 SERIES 3 AND MIL-C-26500 THREADED OR BAYONET CONNECTORS, AS APPLICABLEI INTERMATEABLE
WITH
BAYONET
RECEPTACLE CONNECTORS DC50 DC51
MIL-C-B3723
SERIES 3 AND MIL-C-26500
PIN CONTACTS
SOCKET CONTACTS
•
•
•
•
PLUG CONNECTORS DC52 DCS3
CONNECTORS:
15 Aircraft Technical Book Company
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DC 50 through DC57 Electrical Connectors INTERMATEABLE
WITH
THREADED
MIL-C-83723
•
SERIES 3 AND
RECEPTACLE CONNECTORS SOCKET CONTACTS PIN CONTACTS
C57 DC55 DC54
MIL-C-26500
•
CONNECTORS:
DC56
PLUG CONNECTORS
08-03
APPROVED
20 1126 20 1126DC39-2OP 16 DC38·16P DC39-16P DC39-20P 24 31 15 DC39-2OS 37 1123 16 1131 1126DC38-2OP 1126DC38-2OP DC38-2OP DC38-16P 41 55 14 12 DC39-20S DC39·165 DC39·16S DC38-2OS 5 1124
EQUIVALENT
PART NUMBERS:
1123
S
DC39-16S
5100-181-16
1124
S
DC39-2OS
5100-181-20
1126
P
DC38·2OP
5000-102-20
1131
P
DC38-16P
5000-102·16
031-1318-000 031-1317-000 317-2020-088
REC20W-4DJ5
030-9173-D40 030·9205-027
16 Aircraft Technical Book Company
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DC 60 through DC 63 Electrical Connectors IEMPLOYING
REAR RELEASE
CONTACTS,
TO THE REQUIREMENTS OF DOUGLAS AND INTERMATEABLE WITH THREADED
CONNECTORS
ARE
DRAWING BAN7025, MIL-C-5015 CONNECTORS)
•
•
RECEPT~CLECONNECTORS SOCKET CONTACTS PIN CONTACTS
3 1
th
DC60
PLUG CONNECTORS
DC62
10SL-3 12SB-51S' contacts.
48 1136DC64-8P 16 12 16 1128 1127 8 116 163 160 O C64-16PCH DC65-12S 10 14 19 3 2 5 7 6 171129 1122 1121 1125 D DC64-12P C64-16P C64-12P DC66-12S DC65-8S DC66-16S DC65·16S DC65-16SS DC66-8S DC66-16SS DC65-16S OC66-16SS OC66-16SSAL OC66-16SSCH AL 11~
1164 1161
1
17
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SHELL SIZE AND LAYOUT
PART NUMBER
DESIGNATOR 22-18
APPROVED
(SOCKET CONTACTSI 1136 1128 12 16 14 816 165 DC64-8P 35 DC65-8S 2 1129 1122 1173 1/0 1127 16 166DC64-16P DC64-0P DC64-4P DC64-12P DC64-OP 37 40 46 DC65-16S DC65-4S DC65-12S DC6S-12S DC65-0S 43 7 8 1121 1167 1174 DC65-OS 11?7
EQUIVALENT
1121
PART NUMBERS:
DC64-16PAL DC64-0P DC64-4P DC65-12S DC65-0S 018-1616-117A 317-1212-092 5000-101-16 DC65-16S DC65-4S DC64-8P DC64-12P DC64-16PCH DC64-16P DC6S-16SSAL DC65-16SSCH S P 5000-106-116 017-1616-091A 5000-101-08 017-1616-091C 5100-193-116-1 5000-101-12 5000-106-216 5100-193-216-1 5100-179-0 317-1616-001 031-3113-015 030-3197-015 031-3113-016 NO SUPPLIER 030-3198--010 030-32
1173 1122
18 Aircraft Technical Book Company
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MIL-( - 38999
Electrical Connectors
(EMPLOYING
CONTACTS)
REAR RELEASE
SERIES I RECEPTACLE CONNECTORS MS27466,
•
MS27467
20 446 446 32 16 M39029/68-363 M39029/68·364 M39029/68·363 M39029/68-351 M39029/68-352 M39029/68·351 20
19-32P
• •
•
MS27468
PLUG CONNECTOR
25-43S 19-32S
SOCKET CONTACTS
PIN CONTACTS
461 462
23
NOTE: Contacts can be obtained from ITT Cannon and Bendix using PINs listed above, except the only approved Bendix PIN for Term Code 461 is 10-407035-205.
(EMPLOYING
REAR RELEASE
CONTACTS
I
SERIES II RECEPTACLE CONNECTORS MS27474,
MS27497
PLUG CONNECTORS MS27473,
8·35P
MS27484
220446 220446 20 35 M39029/68-360 M39029/58-363 M39029/68-363 M39029/57·354 M39029/67·357 6
SOCKET CONTACTS
PIN CONTACTS
• •
• •
442 444
8·35S 8·98S
19
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annon
Electrical Connectors
(EMPLOYING
CONTACTS
REAR RELEASE
10-55 20 220446 220 22D 220 22D 446 M39029/57-357 M39029/57 M39029/57-357 M39029/57-354 M39029/57 22 32 37 61 79 13 65 -354 -357 20 M39029/58-360 M39029/58-363 M30929/58-360 M39029/58-363 M39029/57-354 100 66 55 41 10 18 PIN for Term Code 444 is 10-251416-205.
20-41 24-615 14-355 22-355 20-355 10-985 18-355 12-355 12-985 14-1855 16-35S 18-325 10-355 and Bendix
MIL -C- 38999
using
PINs
listed above,
except
the only approved
444 442
Bendix
20
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Contacts for Rack & Panel (Rectangular)
Connectors
Because ITT Cannon descriptive part numbers may exceed the 15 digits allotted in the Douglas computer system, ITT Cannon drawing numbers have been assigned to many rack and panel connectors, Both numbers will appear on the connector shell: the ITT descriptive part number metalstamped into the shell, and the drawing number ink-stamped onto the shell. The following listing provides a cross-reference to the descriptive part numbers and drawing numbers, the term codes and part numbers of the applicable contacts, and the sizes and quantities of contacts required for the applicable connector. Because of some subtle variations in descriptive part numbers, connectors the ITT drawing number,
should be ordered using
21
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CONTACTS QTY SIZE 8-8 COAX 10-10 16-16 20-20 16-16 20-20 20-20 022000-6023 COAX 041700-0037
TERM PIN CODE CONTACTS
TERM SOCKET CODE CONTACTS
DPDMA-32C2-33S-1A DPDMA-E32C2-33S-1B 146 42 COAX DPDMA-32-33S-1B DPAMA-L24C2-33$-B DPDMA-4S-33S-1 DPDMA-78G-33S-1B DPAMA-32-33$-G DPAMA-24HV2-33$-G DPDMA-U32C2-33S-1B DPDMA-A32-33S-1B DPAMA-24HV2-33$-B DPAMA-B24C1 DPEMA-60-33S-A DPEME-60-33S-A DPSRC-2OCS-33A-l DPSRC-42-33A-1 DPD2MA-I52-33S-2 DPD2MA-152-33S-2POSZ DPD2MA·I52G-33S-2POSZ DPD2MA-I52G-33S-1BPOSZ DPDMA-4S-33S-1A DPDMA-78-33S-1B 1033 1034 _714 718 719 720 714 716 22 30 43 78 28 60 32 22 15 HVI-33$-B 031-1758-000 031-9206-004 031·9206-004 031-9206-000 030-1758-000 031-9176-000 031-9177-003 030-9176-000 031-1046-002 031'1046-002 031-1141-000 031-9174-003 031-9177-003 B 101-A 101 101'A 106 106 001-1046-002 DPD2MA-152-33S-2-1B
22 4 65
23
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m
32 4 45 6
6
73 7-8 10-10 16·16 20-20 030-9083-001 621 1099 DPX2MA-45S45S-33B-0265 DPDME-76-33S-1 DPDMA-76G-33S-3LPOSN DPDMA-45G-33S·1 SPL 128 43 28 52 73 031-1046-002 COAX 031-9134-004 031-1046·002 BPOSN 8-8 16-16 COAX 20-20 20·20 16-16 2O-20HD 2O·20HD 20·20 030·9081-003 DPX2MA·57S57S-33B·0210 DPX2MA-67S67S-33B-02IXXI DPDMA·32G-33S·1 DPDMA-U32C2G-33S-1 DPX2MA-57S57S-33B.Q281 DPX2MA·26S45S·33B.Q201 DPX2MA-57S57S-33B·0204 DPX2MA·57S57S-33B·0243 DPX2MA-45545S·33B.Q220 DPX2MA-32F2S57S-33B-0202 DPX2MA-57S57S·33B.Q206 DPX2MA·57S57S-33B-02IXXI DPX2MA-57S57S-33B·0211 DPX2MA-40Fl DPDMA-76G-33S·3L DPX2MA-57S57S·33B-0202 718 721 719 716 720 716 114 90 26 87 81 57 S40F1 031·9206·004 031-9206-004 031·9206-004 030-1758-000 031·1149-001 030-9176-000 031·1046.(J()2 B S·33B-0203 B DPX2MA·67P67P-34B.(J()IXXI DPDMA-76-33S-1APOSN DPDMA-76-33S-1 DPX2MA-26S28S·33B·0201 DPX2MA-45S45S·33B.Q221 DPX2MA·C2G S57S-33B.Q203 031·1046-002 BPOSN 041700-0329 DPX2MA·45545S-33B·0266 DPX2MA·57S57S-33B.Q244 DPX2MA-57S57S·33B-0247 28
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ITT CANNON ITT CANNON
DESCRIPTIVE P! N
DRAWING NUMBER
IREF ONL YI
CONT ACTS OTY
SIZE
PIN
TERM
SOCKET
CODE CONTACTS
TERM
CODE
CONTACTS
..
"'~ ~:...~:~-~-=
~~·;-~f.j_,iMIiI,',
.~_ .. ~;~~;IiIi1I~
~'~
~ :041'-
IMUO:OU
w
IMI~
'~j}~ Df>~
__ ::"
~
'.~
::::;'-~.02110
~'-~~t5 Ot__ Ot1•..•••••
''''c·....••. ,,~.Q220 ~
~~iii"i2MA~
~'"
-:~3
Ot~---
-DPx2MA~
04~=:" .Ot~-"' Oft __ Oft __
'0tI~-
~~
~_
.• ·~DPx2MA~ "':'
-
= ~~
DPX2MA-87S51S-33B-OZ1a
04f11134/!1
~
O4f111S.G28t
~
041__
~-
04'nOO:1S Ot1'11M21O 041713427a
~."" 0417li34iio 0417lI).02II1 041783G18Z O4f1113.Oa!3
0417a:J.o:zE 0411134288 041183-0304 Ott7a;l-03o7 04118343ff1, 041~
.fIi'~ 1M'
25
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ITT CANNON ITT CANNON
DESCRIPTIVE
DRAWING NUMBER
(REF ONL YI
PIN
CONTACTS
TERM
OTY
CODE CONTACTS
Q3G.2289..OOODPX2MA-108P57S-33B-0401 Q3G.2289..OOODPX2MA~-338-li9(XXI .1005 OPX2MA-32A2S67S-338..o41XXI DPX2MA-57SII1S-338~1 DPX2MA-A DPX2MA-2603S67S-338-0441 DPX2MA-2503S57S-338~1 DPX2MA-23CI~..Q4(XX) 10C3S32A2S-338.o«12 101M 723 67 78 80 716 718 723 031-1069-001 031-9134-GM 031-104500Z 031-104e.002 031-9134-GM 031.e134-GM 031-1~ 031-9134-GM Q3G.2289..OOOOPX2MA-45S8S-338~1 030-22BIHJOO 1005 1008 1005 DPX2MA-AI08PAI08P-338-1i9(XX) DPX2MA-I08PI08P-338..Q4(XX) DPX2MA-AC3S67I).338.02(XX) DPX2MA-57$ DPX2MA-108S10es-348-0215 OPX2MA-40S40S-338-0415 DPX2MA-408IS4081S-338~ 212 1081'-338-0002 721 108 45 30 III 85 22 7723COAX 031-8206-004 031-9208-004 20-20 3).20 22-22 COAX 2O-2DHD 031-1046-00'2 1005 212 128 1008 O31-111UOO 721.~~ a.zz.' 723 031-9134-GM 041~15Q3G.2289..OOO ~ '~"128 (:iI;!iiHoTt .~
P108P-338-1i8OO 2O-2DHD 16-18 30 108 20-20 64 2 6 38 •• COAX 2O-2DHD 16-16 ,.,8 16-16 DPX2MA-AIQ8SAI08S-34B.eIIXX) 64 2O-2DHO 1 22-22 I08P:338-1i8OO~ Df'~ .8.,1~16.~ 12-12
67 212
SIZE 22-22
PIN
TERM
SOCKET
CODE CONTACTS
1008 031-1.11UOO
20-20 22-22 _
26
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ITT CANNON
64
72 34 62 45 64
ITT CANNON DRAWING NUMBER
DESCRIPTIVE PIN !REFONLY)
CONTACTS aTY SIZE
20-20 1006 041784-0112·!XX! COAX 16-16 COAX 2O-2OHD 20-20 16-16 20-20 20-20 030-2289-000 22·22 22-22
DPX2MA·A DPX2MA·57S57S·33-«J01 DPX2M DPX2ME-67S675·33B-03(XXI DPX2MA·57S57S·33A-roo1 DPX2MA-57S57S·33-0302 DPX2MA-57S57S-33-OOOI E-40S40S·33B-0315 721 723 I06PA 031-9206-004 031·9206-004 COAX 031·9134-004 031-1046-002 C"OAX OPX2ME·AC3S67S·33B-03IXXI DPX2ME·57SOOS·33B-03(XX) DPX2AD-C7BS67S-33B-oJ(XX) DPX2MA-I06PI06P-33M-06(XXI DPX2ME-32A2S67S-33B·0353 OPX2ME-57567S-33B-031 DPX2ME-OOS57S-33B-03(XXI DPX2ME·C2R557S·33B-03IXXI DPX2ME-40F DPX2ME-C2MS575·33B-03(XX) DPX2ME-45S45S·33B-03(XX) DPX2ME·26S26S-33B-roo1 DPX2ME·26S45S-33B-roo1 DPX2ME·A32C2S57S·33B-03(XX) DPX2DA-26575·33B·59(XX) DPX2ME-57S575·33B-03!XX) DPX2ME-57S00s·33-03(XXI DPX2DA·26S7S-33B-OOXXI DPX2ME·57S57S-33-0301 716 5PL 1S4OF1S·33B-03(XXI 212 114 129 90 60 64 29 26 80 52 30 031·1046-002 57 031106P·33M-0501 031031-9134-004 67 -1046-002 1046-002 XXI 60
TERM PIN CODE CONTACTS
TERM SOCKET CODE CONTACTS
90
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21-0000-IXXI 84
I"IT CANNON
:.IO-2OHD 4 312 COAX 18-16 12-12 16-16 16-18 12·12 COAX
48 :.IO-2OHD 2 18-16 16-18
ITT CANNON
DESCRIPTIVE PIN
TERM
DRAWING
(REF ONLY)
CODE CONTACTS
NUMBER
PIN
TERM
SOCKET
CODE CONTACTS
030-9083-001 030-22II!HJOO 030-90111-000 030-91Il4-OO3 621 1006 1113 1098 DPX2ME·57S57S·33A·Q3tXX) DPXBME·57·33S-03()()(1 OPX2ME·45P45P-34B-03IXX) DPXBME-87·33S-03IXXI DPXBME-8-33S·0301 DPX2ME·26D3S67S-33B-0301 DPX2ME·57P67P·34B-03IXX) BKAE2-87403-26-(XXI DPX2ME·23C 1S40S·33B-03IXXI 1064 300 106 114 128 721 723 90' 84 28 46 67 718 723 :.IO-2OHD :.10-::10 :.10-20 16-18 COAX 031·1069-Q01 031·92Q&.004 031-1069-Q01 031-81~ 031-105001 031·91~ COAX 031·1048-002 031·1048i002 031·91~ 031·1048-002 066442-G430-41 1113 DPXBME·A DPX2ME·57P57p·33B-03IXXI DPXBME·26-33S-0301 DPXBME-4&33S-03(XXI DPXAME·57·33S·17 BKAE2-87403-006HXX) BKAEI-87401·7-(XX) DPX2ME·AC3S67S·33B-03(XX) 106-33P-03IXXI SPL ISO 22 57 721 871622·22 12·12 0:11·1048-002 031·92Q&.004 031-1048-002 031.g1~ (2) Term Codes and 721 specify identical contact, 1TT Cannon PIN 031-9206-004. (3)57 inserted where (XX)anare found indicate PINthe 031-9206-004. polarizing position when .the wire it is being terminated to is 22 or 24 gage. 721, size 16-16 contact, In Cannon 66 Numbers :.10-::10718
031-9203-008, is a size 16-20 contact that can be substituted
for Term Code
. ~. ~
. 28
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