g
LINE MAINTENANCE COURSE A330 Volume 2 Student WorkBook
CF6-80E1
1. ENGINE CONPONENT IDENTIFICATION EXCERCISE
4
3
1 2
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Spinner cover Spinner Fan Blade Forward acoustical panel
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides the majority of the thrust produced by the engine. Provides noise suppression and a smooth aerodynamic secondary airflow path. Provides a smooth, inner aerodynamic flowpath for air entering the engine. Provides access to thirty-four internal bolts that attach the spinner to the fan disk.
7
6 5
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Kevlar Blanket Bore Cooling Valve Thrust Reverser Hold Open Bracket
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Hold open the thrust reverser for engine inspection and/ or maintenance. Reduces the cooling airflow to the bore of the high pressure compressor during cruise conditions. Provides containment of the fan blades in the event of a failure.
8 10
g
GE Aircraft Engines
TYPE CERTIFICATE
PROD CERTIFICATE
E 13NE
PC 108
MODEL NO.
SERIAL NO.
CF6-80C2
XXX-XXX
RATED TO MODEL CONFIGURATION IDENTIFIED BELOW CONFIG
TO THRUST
MAX CONT
SERV BUL
B1F
57,160
49,810
72-389
DATE OF MFG
04/94 CINCINNATI, OHIO
COMPLY MADE IN USA
9
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Engine Data Plate Electronic Control Unit Identification/Rating Plug
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Controls engine systems, provides engine indicating parameters, and displays fault messages. Provides thrust and engine configuration information to the ECU for proper engine valve and actuator control. Accurately identifies each individual engines' model designation/configuration
11
12
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Thrust Reverser Door Hydraulic Opening QD
Provides a hand pump for door opening.
Upper and Lower Ignition Exciters
Produces high energy power to the igniter plugs.
16
13
15
17
20
19 18
14
21
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT N2 Accelerometer Forward Engine Mount
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Pushes or pulls on an adjustable link to rotate a bellcrank. Provides a signal to the ECU as an indication of duct leakage.
Aft Inner Acoustical Panel
Cooling air supply control for the core compartment.
B/C Sump Pressurization Duct
Pressurization air supply to the B/C sump.
7th Stage Delta Pressure Switch
Core vibration signal to the aircraft vibration computer.
11th Stage Cooling Duct
Cooling air supply to the 2nd stage HPT nozzle.
Core Compartment Cooling Valve
Provides noise abatement and smooth airflow.
B/C Sump Vent Duct
Transfers thrust loads from the engine to the aircraft.
VBV Actuator
Vents air from the B/C sump to A sump.
22
23
24
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT N1 Accelerometer Alternate N1 Accelerometer P/T2.5 Sensor
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides a N1 vibration signal to the vibration computer should the primary accelerometer fail. N1 vibration signal to the aircraft vibration computer. Core compressor inlet temperature and pressure to the ECU.
26
27
25
28
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
TGB Scavenge Oil line
Provides an oil return from the TGB and "A" sump to the lube and scavenge pump. Delivers oil under pressure to the engine bearings and gears, and then recovers the oil for reuse. Provides an electrical signal equivalent to the pressure conditions within the bearing sumps.
Transfer Gearbox (TGB)
Transfers output power from the IGB to the AGB.
Oil Pressure Transmitter Lube and Scavenge Pump
31 29
33
30
32
34
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Accessory Gearbox (AGB) Scavenge Oil Line Temperature Engine Oil (TEO) Sensor Low Oil Pressure Switch
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides engine scavenge oil temperature indication to the flight deck. Provides a signal to the aircraft indicating and warning systems when oil pressure is low. Provides an oil return from the AGB to the lube and scavenge pump.
Permanent Magnet Alternator (PMA)
Provides oil filtration at a 74 micron nominal rating.
Lube Supply Filter (GE SB 79-0008 eliminates supply filter)
Trap magnetic particles suspended in the scavenge oil.
Scavenge Pump Magnetic Chip Detector
Power supply for the ECU.
39
38
36
37 40
35
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Fuel/Oil Heat Exchanger
Trap magnetic particles suspended in the scavenge oil.
Master Chip Detector
Interface for the Integrated Drive Generator to the AGB.
Pneumatic Starter IDG Mounting Pad Accessory Gearbox (AGB) Starter Control Valve
Provides cooling of the engine oil and heating of the engine fuel. Applies torque through spur gears to drive attached accessories. Initiates and terminates the supplied airflow to the pneumatic starter turbine. Drive the engine core from stationary to idle speed and provide rotation for engine motoring.
45
42
44 43
41
46
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT 11th Stage Cooling Duct Upper EGT Harness
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides T4.9 signal from 4 thermocouples to junction box. Provides sensing lead protection against extreme engine heat.
HPTACC Cooling Manifold
Delivers air to stage 1 LPT nozzle trailing edge.
T3 Sensor Hard Lead
Provides an interface for upper and lower EGT harnesses that provide a signal to the ECU.
HP Recoup Tube
Distributes the air to the HPT case.
EGT to ECU Interface Connection
Cooling air supply to the 2nd stage HPT nozzle.
48
49
51
52
47
50
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Borecope Inspection Port B4-4
Regulates cooling air flow to the exterior of the LPT case.
LP Recoup Vent Tubes
Provides inspection views of stage 5 trailing edge.
LPTACC Control Valve
Vents air from the CRF into the primary exhaust.
Turbine Rear Frame
Support interface to the shipping stand.
LPTACC Cooling Manifold
Distributes the air to the LPT case.
Ground Handling Mount
Provides the aft connection of the engine to the pylon and is the structure supporting the “D” sump.
54
53
55
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
No. 6 Bearing Oil Supply Line
Returns oil from the No. 6 bearing.
"D" Sump Scavenge Line
Heat protection for the "D" sump cover.
"D" sump Cover Heat Blanket
Delivers oil to the No. 6 bearing
58 56
57
IMG0014.JPG
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Core Cowl Hold Open Bracket
Provides security for nut securing bracket to LPT case.
Engine LPT "CU" Measurement Identification Tag
Measurement data for LPT module installation.
LPTACC Manifold Mount Bracket Anti-tamper Pin
Secures core cowl open during inspection or maintenance.
59
60
62
61
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT No. 6 Bearing Oil Supply Line Spray Shield Borescope Inspection Port B4-2 Borescope Inspection Port B4-3 Borescope Inspection Port B4-1 or Optional P4.9 Probe
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides inspection views of stage 3 (LPT) leading edge and stage 2 (LPT) trailing edge. Provides inspection views of stage 2 (LPT) leading edge and stage 1 (LPT) trailing edge. Provides inspection views of stage 1 (LPT) leading edge and stage 2 (HPT) trailing edge. Prevents oil spray onto hot engine in case of a leak.
65
64
63
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Lower Ignition Lead Ignition Cooling Shroud Engine Accessory Heat Shield
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Protects engine accessories from extreme engine heat. Delivers DC power from the upper exciter to the lower igniter. Provides a cooling chamber for the ignition lead to igniter connection.
69
67
68
66
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Fuel Nozzle Supply Manifold
Distributes metered fuel to each nozzle.
Altitude Relight Fuel Nozzle (Blue Band)
Collects fuel leakage from fuel nozzle drain shrouds.
Fuel Drain Shroud
Delivers a richer fuel flow for altitude relights.
Fuel Nozzle Drain Manifold
Collects leakage from the fuel supply line to fuel nozzle connection.
71
72 70
73
74
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
7th Stage Cooling Supply Manifold
Delivers cooling air to the stage 2 HPT nozzle.
11th Stage Cooling Supply Manifold
Measures air temperature exiting the HPT.
EGT Probe
Delivers cooling air to the stage 1 LPT nozzle leading edge. Delivers DC power from the lower exciter to the upper igniter. Delivers cooling air to the stage 1 LPT nozzle trailing edge.
HP Recoup Tube (right side) Upper Ignition Lead
75
79
76 77 78
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Ps3 Sensor Line
Collects air for use by aircraft systems.
8th Stage Bleed Air Manifold
Collects cooling air for the stage 1 LPT nozzle leading edge. Collects cooling air for the stage 1 LPT nozzle trailing edge. Regulates cooling air flow to the exterior of the HPT case to minimize the clearances. Transfers the pressure of compressor discharge air to the ECU to be used in several of its calculations
7th Stage Bleed Air Manifold HPTACC Control Valve 11th Stage Bleed Air Manifold
80 82
83
81 84
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Fuel Filter Delta Pressure Switch
Returns fuel to the main fuel pump.
Fuel Supply Pressure Line to HMU
Removes contaminants from the engine fuel.
HMU Fuel Bypass Line
Provides additional heating for the fuel that will be used in the servo section of the Hydromechanical Unit.
Servo Fuel Heater
Provides flight deck indication of fuel filter clogging.
Fuel Filter Assembly
Delivers high pressure fuel to the HMU.
86
85 87
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Fuel/Oil Heat Exchanger Fuel Flow Transmitter IDG Fuel/Oil Cooler
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Measures the total mass flow of fuel supplied to the engine combustor and sends a signal to the ECU. Provides cooling of the engine oil and heating of the engine fuel. Provides cooling of the IDG oil by means of fuel system flow.
89 88
91 90
92
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
VBV Actuator
Delivers cooling air to the shrouded igniter.
Ignition Lead Cooling Supply Air Tube
Provides cooling of the IDG lubrication oil.
Stage 5 VSV Unison Ring Clevis Link
Controls the fan airflow to the IDG air/oil cooler.
IDG Air/Oil Cooler Control Valve
Push or pull on an adjustable link which rotates the bellcrank.
IDG Air/Oil Cooler
Attaches unison ring to master arm
95
94
93 96
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT VBV Door (12 total) IDG Air/Oil Cooler Control Valve Manual Lockout VSV Actuator N1 Speed Sensor
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Holds the normally spring loaded open valve to the closed position for removal and installation. Allows bypass of booster discharge into the secondary airflow. Repositions the master arm attached to the unison rings. Provides fan speed signals for the flight deck display, and for several of the ECU's control calculations.
99
98
97
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Servo Fuel Inlet to HMU
Meters and distributes fuel needed for combustion positioning of actuators and valves.
HMU Metered Fuel Discharge
Supplies fuel from the HMU to the fuel manifold.
Hydromechanical Unit (HMU)
Supplies fuel from the servo fuel heater to the HMU.
100
101
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
VSV HEAD fuel pressure line.
Delivers fuel to the VBV valves for actuation.
VBV OPEN fuel pressure Line
Delivers fuel to the VSV valves for actuation.
102
103
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
BSI Motoring Pad Cover Plate
Encloses the BSI motoring access port when not in use.
N2 Speed Sensor
Provides core engine speed signals for flight deck display and several ECU's control calculations.
106
104
105
107
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Scavenge Oil Return Line
Delivers engine oil form the oil tank to the oil pump.
Oil Supply Line
Provides smooth aerodynamic airflow around the fan strut and reverser halves.
Drain Mast
Returns oil to the tank from the scavenge oil filter.
Fan Frame Strut Fairing
Discharges fluids directly overboard.
108 109 110
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Bore Cooling Valve (BCV) Inspection Hole
Holds thrust reverser halves closed.
Thrust Reverser Door Latch Bracket
Provides visual inspection of valve.
Bore Cooling Valve (BCV)
Regulate the booster discharge air is extracted from leading edge scoops.
111 112
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Fan Frame Strut No. 4 (3 o'clock)
Pickup and delivery of booster discharge to the bore cooling valve.
Outlet Guide Vane (OGV)
Straightens fan discharge air.
114
113
115
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Oil Scavenge Line
Supplies booster air for seal pressurization.
Inflatable Seal Air Supply Line
Vents oil tank to the "A" sump.
Oil Tank Vent Line
Returns oil to the tank.
118
120
116 117
119
121
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Oil Tank
Catches oil servicing overflow.
Scupper Drain
Provides visual oil level indication.
Oil Tank Manual Fill Cap
Provides non-pressurized oil servicing port.
Oil Tank Sight Gage
Provides pressurized oil servicing port.
Oil Tank Pressure Fill Connection
Provides relief of excessive tank vent pressure.
Oil Tank Pressure Relief Valve
Provides oil storage.
123
122
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Scavenge Oil Filter Scavenge Oil Filter Delta Pressure Switch
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides flight deck indication of scavenge oil filter clogging. Screens contaminants from oil returning from the engine bearings and gears.
126
124
125
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
T12 Temperature Sensor
Recovers oil from the vent air leaving A-sump by centrifugal action.
Number One Bearing MAnifold
Provides the temperature of the fan inlet air to the ECU.
Fuel Temperature Sensor
Senses the temperature of metered fuel discharged from the HMU.
130
128 127
129
131
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Core Module Accessory Drive Module Low Pressure Tubine Module Fan Module High Pressure Turbine Module
ITEM NO.
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Drives the fan rotor thru the fan mid shaft. Supplies 80 percent of the total engine thrust and boosts airflow to the HPC. Compresses and accelerates 20 percent of the total engine thrust and provides drive to the AGB. Extracts energy from the combustion gases leaving the combustor to drive the HPC. Applies torque through spur gears to move attached accessories.
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
2
PLACE PICTURE HERE 3 1
RIGHT HAND SIDE IMG0002.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL ENGINE COMPONENT IDENTIFICATION EXERCISE
Page 12-4 Mar 02
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Nacelle Temperature Probe Pressure Relief Panel Latch Housing and Anchor Bolt (Typical)
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Opens if the differential air pressure between the nacelle air and ambient air exceeds 3.5 psid. Provides flight deck temperature monitoring in the event of a pneumatic leak. Provide attach point for the left thrust reverser half mounted tension latches.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-5 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
LIFT HAND SIDE
RIGHT HAND SIDE
6 5
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7
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LEFT HAND SIDE IMG0007.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL ENGINE COMPONENT IDENTIFICATION EXERCISE
Page 12-6 Mar 02
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Access Panel
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Secure both thrust reverser halves together.
Guide Tube Tension Latch (Typical) Thrust Reverser Cowl Opening Actuator
Opens the thrust reverser halves to provide access to systems and components installed on the engine. Provides access for manual operation of the starter air valve. Provides access to the IDG and the Master Chip Detector for servicing.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-7 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
8
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9
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL ENGINE COMPONENT IDENTIFICATION EXERCISE
Page 12-8 Mar 02
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Handpump
Provides hydraulic pressure to the opening actuator.
Left Hand Thrust Reverser Half.
Provides one half of the fan discharge duct and core cowling.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-9 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
11
10
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-10 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Core Cowl Hold Open Rod (Retracted) Flexible Shaft
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Provides a safe 33o open position of the thrust reverser half. (extracted position is 45o open.) Transmit mechanical force form the CDU to the upper and lower Angle gearboxes. Opens the blocker door when the translating cowl is deployed.
Blocker Door Link Arm
Creates the inner wall of the fan discharge duct.
Upper Ballscrew Actuator Ball Nut
Transfers the rotational movement of the ballscrew to the linear movement of the rod end during stow/deploy.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-11 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
LEFT HAND SIDE
19
16
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17 RIGHT HAND SIDE IMG0010.JPG
RED WARNING PLATE AND LOCKOUT BOLTS IMG0023
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Top Latch Handle
GENERAL
Page 12-12 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Red Warning Plate and Lockout Bolts
Provides remote access to the upper latch clamp.
Top Latch Handle
Used to hold the reverser half in the open position.
Lower Angle Gearbox
Assist the Center Drive Unit in driving the transcowl.
Angle Gearbox Actuator Pin
Provides a visible and mechanical lockout of the reverser in the stowed position.
Hold Open Rod (stowed)
Secures the angle gearbox to the T/R fixed structure.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-13 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
20 22
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21
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-14 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT 450 Cascade Vane Straight Cascade Vane Translating Cowl
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT When deployed moves the blocker doors into position and exposes the cascade vanes. 1 of 14 that provides reverse airflow and does not interfere with aircraft control or cause debris ingestion. 1 of 16 that provides reverse airflow and does not interfere with aircraft control or cause debris ingestion.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-15 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
23
24
25 HERE PLACE PICTURE
IMG0012.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-16 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Cover Plate
Transfers the linear movement of the actuator to the translating cowl.
Ballscrew Actuator Rod End
Provides access to the ballscrew actuator rod end.
Ballscrew Actuator Pin Cover Plate
Provides access to the rod end attach pin.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-17 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
28
29
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
LEFT HAND SIDE
GENERAL
Page 12-18 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
CF6-80E1
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Center Drive Unit
Provides electronic feedback to the ECU of transcowl position.
Center Drive Unit Stow Rig Pin
A visual indicator used for rigging of the transcowl.
Thrust Reverser Rotary Differential Transducer (RVDT) Center Drive Unit Manual Brake Release Handle
Transfers pneumatic power the transcowl and through flex shafts to two angle gearboxes. Manually locks the air motor from rotating in the deploy direction.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-19 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
31
32
33
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30
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LEFT HAND SIDE FORWARD LOOKING AFT
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-20 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Center Drive Unit Shims (stowed)
Provides end of travel information to the ECU.
Center Drive Unit Lockout Plate (unlocked position)
Used to adjust transcowl gap during rigging.
Stow/Deploy Switch Module
Provides physical locking of the CDU gearbox during deactivation.
CDU Directional Valve Override Linkage
Mechanical shutoff for the DPV at end of travel.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-21 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
36
TRAINING MANUAL
37
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34
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-22 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Stow/Deploy Switch Electrical Connector
Provides a cushion for the transcowl when in the stowed position. Provides a mounting attach point for the thrust reverser transcowl during lockout. Provides an attach point on the transcowl for the deactivation lockout bolts.
Transcowl Bumper
Provides a control and indication signal to the ECU.
Transcowl Locking Bolt Holes Transcowl Lockout Plate
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-23 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
38
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40
39
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EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-24 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Power Door Opening Interlock Valve Power Door Opening Power Pack Power Door Opening Switch
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Self contained power source for opening the thrust reverser halves without the need for ground support. A control device that initiates the operation of the Power door opening system. Prevents hydraulic fluid from entering or exiting actuator to prevent damage to core cowling.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-25 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
44 41
PLACE PICTURE HERE 43
42
RIGHT HAND SIDE FWD LOOKING AFT IMG0025.JPG
IMG0024.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-26 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Center Drive Unit Signal Air Line
Used to adjust transcowl gap during CDU rigging.
Center Drive Unit Air Supply Line
Used to unlock the CDU air motor during maintenance.
Center Drive Unit shims (installed)
Provides ECS air to the Center Drive Unit.
Center Drive Unit Hand Brake (off)
Provides an air signal to the DPV to disengage the brake assembly.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-27 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
45
PLACE PICTURE HERE
45
46 LEFT HAND SIDE AFT LOOKING FORWARD
IMG0028.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-28 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Ballscrew Actuator Pin Access (alternate)
Provides alternate access to the ballscrew actuator rod end pin if normal access is not possible.
Blocker Doors (2 of 6 deployed)
Deflects fan airflow through the cascade vanes.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-29 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
PLACE PICTURE HERE
TRAINING MANUAL
48
47
LEFT HAND SIDE FORWARD LOOKING AFT
IMG0030.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-30 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Thrust Reverser Electromechanical Brake
Provides manual release for maintenance purposes.
Thrust Reverser Brake Handle
Locks thrust reverser in stowed position.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-31 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
50
49
IMG0031.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
PLACE PICTURE HERE
LEFT HAND SIDE FORWARD LOOKING AFT
GENERAL
Page 12-32 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Upper Latch "U" Bolt
Adjustable to control latch closing tension.
Upper Latch
Secures the thrust reverser half to the aft fan case.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-33 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
51
IMG0035.JPG
FWD LOOKING AFT
PLACE PICTURE HERE
52 IMG0012.JPG IMG0036.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-34 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT
Actuator Ballnut Service Fitting
Provides a grease fitting for ballscrew servicing.
CDU Actuator Ballnut Service Fitting
Provides a grease fitting for ballscrew servicing.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-35 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
CF6-80E1
TRAINING MANUAL
55 56
PLACE PICTURE HERE 54
57
58
53
LEFT HAND SIDE FORWARD LOOKING AFT
IMG0039.JPG
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
GENERAL
Page 12-36 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
GE AIRCRAFT ENGINES
ITEM NO.
IDENTIFY THE LINE, ACCESSORY, OR COMPONENT Upper Angle Gearbox Dust Cap Directional Pilot Valve Inhibit Electrical Connector Directional Pilot Valve
CF6-80E1
ITEM NO.
TRAINING MANUAL
SELECT THE PURPOSE THAT MATCHES THE LINE, ACCESSORY, OR COMPONENT Covers electrical connector during thrust reverser deactivation. When removed the ECU will send a signal to the aircraft indicating that the thrust reverser is inhibited. Provides an air signal to the CDU mechanically releasing the CDU. Monitors air pressure in the thrust reverser system and provides a feedback to the ECU.
Pressure Switch
Transfers air from the ECS system to the CDU.
CDU Air Supply Line
Assist the CDU in driving the transcowl.
GENERAL
EFFECTIVITY A330/ALL GE PROPRIETARY INFORMATION
Page 12-37 Mar 02
ENGINE COMPONENT IDENTIFICATION EXERCISE
