Dash 8 100 Non Normal Rev 10

Dash 8 Model 102 Emergency/Non-Normal checklist

DASH 8 102 Emergency/No Emergency/Non-Normal n-Normal Checklist

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Immediate Action Items Index ENGINE FIRE BEFORE V1 ........................................................ 9 ENGINE FAILURE BEFORE V1 ................................................. 9 SMOKE BEFORE V1 ................................................................ 17 SMOKE IN FLIGHT .......................................................... ......... 18 FUSELAGE FIRE OR SMOKE KNOWN SOURCE .................. 19 FUSELAGE FIRE OR SMOKE UNKNOWN SOURCE ............. 20 MAIN OR AUX BATTERY HOT ................................................ 22 PITCH CONTROL JAM ............................................................ . ........................................................... 46 ROLL CONTROL JAM ............................................................. .. ........................................................... 47 RAPID DEPRESSURIZATION DEPRESSURIZATION .................................................. 58 EMERGENCY DESCENT ......................................................... ..................... .................................... 58 APU FIRE ............................................................ ...................... 65


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2 D A S H 8 1 0 2 E m e r g e n c y / N o n -N o r m a l C h e c k l i s t 0 5 / 2 9 / 1 5

Dash 8 Model 102 Caution Panel Quick Reference

PRI INV 22

SEC INV 22

L AC BUS 29

R AC BUS 29

EMER LTS DISARMED

PITOT HEAT 1 64

#1 HYD FLUID HOT 35

#1 STBY HYD PUMP HOT 35

#1 ENG FUEL PRESS 56

#2 HYD FLUID HOT 35

#2 STBY HYD PUMP HOT 35

#1 BLEED HOT 60

#1 ENG HYD PUMP 32

FLT COMPT DUCT HOT 60

PITOT HEAT 2 64

#1 DC GEN HOT 23

#1 DC GEN 24

#2 ENG FUEL PRESS 56

TERRAIN INOP

RUD PRESS 50

#2 BLEED HOT 60

ROLL SPLR INBD GND 49

#2 DC GEN 24

#2 DC GEN HOT 23

ROLL SPLR INBD HYD 48

ROLL SPLR OUTBD HYD 48

NOSE STEERING 45

PARKING BRAKE

#2 ENG HYD PUMP 34

L STALL WARNING 67

ROLL SPLR OUTBD GND 49

R STALL WARNING 67

FLT DATA RECORDER 68

GPWS

AUX INV 22

DC BUS 27

L26 AC 28

L TRU 23

L WSHLD HOT 64

CABIN DUCT HOT 60

MAIN BATTERY 22

#1 AC GEN HOT 23

#1 AC GEN 23

#2 AC GEN 23

#2 AC GEN HOT 23

#1 RUD HYD 50

#2 RUD HYD 50

INBD ANTISKID 44

OUTBD ANTISKID 44

R26 AC 28

R TRU 23

R WSHLD HOT 64

AIR COND PACK HOT 60

AUX BATTERY 22

#1 ENG MANUAL 12

#1 HYD ISO VLV 32

#2 HYD ISO VLV 34

#2 ENG MANUAL 12

RUD FULL PRESS 50

FLAP DRIVE 54

LDG GEAR INOP 38

WT ON WHEELS 44

L ELEV HORN HEAT 63

R ELEV HORN HEAT 63

SIDE WDO HOT 64

L TRU HOT 23

R TRU HOT 23

DE-ICE PRESS 62

#1 FUEL FLTR BYPASS 57

#1 TANK FUEL LOW 56

#2 TANK FUEL LOW 56

#2 FUEL FLTR BYPASS 57

FLAP POWER 55

APU 65

#1 ENG OIL PRESS 11

#2 ENG OIL PRESS 11

SMOKE 17

CABIN PRESS 58

PASS DOOR 67

BAG DOOR 67

MAIN BAT HOT 22

CHECK FIRE DET

AUX BAT HOT 22

FUELING ON

Index

Engines

ENGINE FIRE BEFORE V1 ............. 9 ENGINE FAILURE BEFORE V1 ...... 9 ENGINE FIRE OR FAILURE AFTER V1 ...................................... 10 ENGINE FIRE OR FAILURE IN FLIGHT ...................................... 11 ABNORMAL OIL PRESSURE ........ 11 ECU FAILURE ................................ 12 ENGINE FIRE DETECTOR LOOP FAILURE.............................. 12 SINGLE-ENGINE DESCENT APPROACH ................................... 13 SINGLE-ENGINE LANDING........... 13 SINGLE-ENGINE GO-AROUND .... 13 SINGLE-ENGINE AFTER LANDING ........................................ 14 IN FLIGHT ENGINE START ........... 14

Propellers

UNSCHEDULED PROPELLER FEATHERING IN FLIGHT .............. 15 BETA LOCKOUT FAILURE AFTER V1 ...................................... 15 PROPELLER GROUND RANGE ADVISORY LIGHT CYCLING ......... 16 PROPELLER OVERSPEED ........... 16

Fuselage Fire

SMOKE BEFORE V1 ..................... 17

& Smoke

SMOKE IN FLIGHT ........................ 18 FUSELAGE FIRE OR SMOKE KNOWN SOURCE ......................... 19 FUSELAGE FIRE OR SMOKE UNKNOWN SOURCE .................... 20

DASH 8 102 Emergency/Non-Normal Checklist

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Index

Electrical

MAIN OR AUX BATTERY HOT ............................................. 22 MAIN BATTERY .......................... 22 AUX BATTERY............................ 22 INVERTER FAILURE .................. 22 TRU FAILURE ............................. 23 TRU HOT .................................... 23 AC OR DC GENERATOR HOT ... 23 AC GENERATOR FAILURE ........ 23 DC GENERATOR FAILURE........ 24 LOSS OF BOTH DC GENERATORS ........................... 24 LOSS OF BOTH DC GENERATORS AND ONE TRU .. 24 LOSS OF BOTH TRU’S AND ONE DC GENERATOR ............... 25 LOSS OF BOTH DC GENERATORS AND BOTH TRU’S .......................................... 25 LOSS OF BOTH DC GENERATORS AND BOTH AC GENERATORS ........................... 26 MULTIPLE INVERTER FAILURE ..................................... 26 DC BUS FAILURE ....................... 27 LEFT MAIN BUS FAILURE ......... 27 RIGHT MAIN BUS FAILURE ....... 27 26 AC BUS FAILURE .................. 28 115V AC VARIABLE FREQUENCY BUS FAILURE...... 29 BATTERY ESSENTIAL SERVICES .................................. 30

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Index

Hydraulics

#1 HYDRAULICS SYSTEM FAILURE ....................................... 32 #2 HYDRAULICS SYSTEM FAILURE ....................................... 34 HYDRAULIC FLUID HOT ............... 35 STANDBY HYDRAULIC PUMP HOT ................................................ 35 PARTIAL LOSS OF HYDRAULIC FLUID FROM BOTH SYSTEMS ..... 36

Landing Gear

ALTERNATE LANDING GEAR EXTENSION ................................... 38 LANDING GEAR EXTENSION USING THE PTU ............................ 39 LANDING GEAR INDICATOR MALFUNCTION .............................. 39 ILLUMINATION OF AMBER DOOR ADVISORY LIGHT(S) ......... 40 ILLUMINATION OF RED LANDING GEAR UNSAFE LIGHT(S) ........................................ 40 ALL LANDING GEAR FAIL TO RETRACT ....................................... 40 LANDING GEAR FAILS TO EXTEND ......................................... 41 WEIGHT ON WHEELS ................... 44 INBOARD OR OUTBOARD ANTI-SKID ...................................... 44 NOSEWHEEL STEERING ............. 45


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Index

Flight Controls

PITCH CONTROL JAM ................ 46 ROLL CONTROL JAM ................. 47 ROLL CONTROL MALFUNCTION.............................48 SPOILER CABLE FAILURE ..........48 INBOARD OR OUTBOARD ROLL SPOILER MALFUNCTION ..49 INBOARD OR OUTBOARD GROUND SPOILER MALFUNCTIONS .......................... 49 RUDDER CONTROL MALFUNCTION.............................50 #1 OR #2 RUDDER HYDRAULIC MALFUNCTION.............................50 RUDDER PRESSURE MALFUNCTION.............................50 RUDDER JAM ............................... 51 RUDDER TRIM ACTUATOR RUNAWAY .................................... 52 AILERON TRIM TAB RUNAWAY ..52 MANUAL ELEVATOR TRIM FAILURE ....................................... 52 ELEVATOR CONTROL MALFUNCTION.............................53

Flaps

ABNORMAL FLAP LANDING........ 54 FLAP DRIVE MALFUNCTION .......54 FLAP POWER MALFUNCTION ....55

Fuel

LOW FUEL PRESSURE ............... 56 LOW FUEL LEVEL ........................56 FUEL FILTER IMPENDING BYPASS WARNING ...................... 57 FUEL TRANSFER FAILURE ......... 57 ABNORMAL FUEL TEMPERATURE ........................... 57

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Index

Air Conditioning

RAPID DEPRESSURIZATION ....... 58

& Pressurization

EMERGENCY DESCENT .............. 58 CABIN PRESSURIZATION FAILURE ........................................ 58 BLEED HOT ................................... 60 AIR CONDITIONING PACK HOT ... 60 CABIN OR FLIGHT COMPARTMENT DUCT HOT ........ 60 UNPRESSURIZED FLIGHT ........... 61 RAM AIR VENTILATION ................ 61 ALTERNATE PRESSURIZATION MODES .......................................... 61

Ice Protection

AIRFRAME DEICING SYSTEM AIR SUPPLY FAILURE .................. 62 ELEVATOR HORN HEAT FAILURE ........................................ 63 AIRFRAME BOOT FAILURE .......... 63 PROPELLER DEICING SYSTEM FAILURE ........................................ 63 ENGINE INTAKE BOOT FAILURE ........................................ 64 WINDSHIELD OVERHEAT ............ 64 SIDE WINDSHIELD OVERHEAT ... 64 PITOT HEAT FAILURE .................. 64

APU

APU FIRE ....................................... 65 APU STARTER CONTACTOR FAILURE ........................................ 65 APU GENERATOR OVERHEAT .... 65 APU REARBAY OVERHEAT ......... 65 APU BLEED AIR OVERHEAT ........ 66


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Index

Miscellaneous

PASSENGER OR BAG DOOR WARNING ................................... 67 CRACKED WINDSHIELD ........... 67 LEFT OR RIGHT STAL WARNING FAILURE ................... 67 ABNORMAL INDICATIONS OF AIRSPEED, ALTITUDE, AND VERTICAL SPEED ...................... 67 AUTOPILOT AFCS MALFUNCTIONS ........................ 68 KNS MESSAGES ........................ 68 FLIGHT DATA RECORDER FAILURE ..................................... 68 TCAS FAILURE ........................... 69 SAHS FAILURE........................... 69 AHRS FAILURE .......................... 70 AHRS PRIMARY POWER SOURCE FAILURE ..................... 71 UNS MALFUNCTION .................. 71 EMERGENCY OPENING OF FLIGHTDECK DOOR .................. 72 INCAPACITATED FLIGHT ATTENDANT ............................... 73 FORCED LANDING WITH BOTH ENGINES OPERATING .............. 74 FORCED LANDING WITH BOTH ENGINES INOPERATIVE ........... 75 EMERGENCY LANDING PROCEDURES ........................... 77 AIRCRAFT DITCHING ................ 78 OBSERVER’S JUMPSEAT BRIEFING CARD ........................ 80

Landing Distance

FLAPS 15 LANDING ................... 83

Charts

FLAPS 35 LANDING ................... 84 RUNWAY SLOPE CHART .......... 85

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ENGINE FIRE BEFORE V1 1) 2) 3) 4) 5) 6) 7) 8) 9) 10) 11) 12)

Parking Brake .................................................................................... Set Power Levers...........................................................................Flight Idle Condition Levers........................................................................ Fuel Off Fuel Off Handle ................................................................................ Pull Extinguisher Switch ......................................................... Forward Bottle AUX Pumps ....................................................................................... Off Notify ATC and Evacuate Cabin as required. Wait up to 30 seconds, if fire persists: Extinguisher Switch ..................................................................Aft Bottle APU/DC External Power.................................................................... Off Battery Master ................................................................................... Off Flight Crew............................................................ Evacuate as required Engine Fire Before V1 checklist .............................................. Complete

ENGINE FAILURE BEFORE V1

1) 2) 3) 4) 5) 6) 7)

Parking Brake................................................................................ Set Power Lever ........................................................................ Flight Idle Condition Lever ...................................................................... Fuel Off Fuel Off Handle .............................................................................Pull AUX Pump......................................................................................Off ATC/FA/Company ............................................................................Notify Engine Failure Before V1 checklist ........................................... Complete


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ENGINE FIRE OR FAILURE AFTER V1 (SILENT) 1) 2) 3) 4) 5) 6) 7) 8) 9) 10) 11) 12) 13)

14) 15) 16) 17) 18)

Gear...................................................................................................... Up Power Lever (affected engine) .................................................. Flight Idle Condition Lever (affected engine) ................................................ Fuel Off Propeller (affected engine) ............................................. Verify Feathered Fuel Off Handle ............................................................................... Pulled (Following a fire), bottle discharge light(s)........................................... Out AUX Pump (affected engine)................................................................ Off Flaps ..................................................................................................... Up Autofeather ........................................................................................... Off Bleed (operating engine) ...................................................................... On Bleed Selector .................................................................................... Max Power Lever .................................................................... Max Continuous Ignition: Operating Engine ............................................................ Manual Failed Engine ......................................................................... Off Standby Pumps .................................................................................... On AUX Pump (operating engine) ............................................................. On -Transfer fuel as required to maintain fuel balance Ice Protection......................................................................... As Required Pressurization ............................................................................. Checked Temps & Pressures ..................................................................... Checked (ALOUD)

19) 20) 21) 22) 23)

Both Power Levers ....................................................... Operate Together Landing Distance Factor .................................................... (1.36)Flaps 15 General Landing Distance .......................................... 3074 Dry/3820 Wet ATC/FA/Company ............................................................................ Notify Engine Fire or Failure After V1 checklist ....................................Complete Proceed with the SINGLE-ENGINE DESCENT APPROACH checklist on Page 13.

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ENGINE FIRE OR FAILURE IN FLIGHT (SILENT) 1) 2) 3) 4) 5) 6) 7) 8) 9) 10) 11) 12)

13) 14) 15)

Power Lever (affected engine) .................................................... Flight Idle Condition Lever (affected engine) .................................................. Fuel Off Propeller (affected engine) ............................................... Verify Feathered Fuel Off Handle ................................................................................. Pulled (Following a fire), bottle discharge light(s)............................................. Out AUX Pump (affected engine).................................................................. Off Condition Lever (operating engine) ...................................................... Max Power Lever (operating engine) .............................................. As Required Standby Pumps ...................................................................................... On AUX Pump (operating engine) ............................................................... On -Transfer fuel as required to maintain fuel balance Sync Off Ignition Operating Engine .................................................................... Manual Failed Engine ................................................................................. Off Bleed (affected engine) .......................................................................... Off Seatbelt Sign .......................................................................................... On Pressurization ................................................................................ Checked (ALOUD)

16) 17) 18) 19) 20)

Both Power Levers ......................................................... Operate Together Landing Distance Factor ......................................................(1.36)Flaps 15 General Landing Distance ............................................ 3074 Dry/3820 Wet ATC/FA/Company ..............................................................................Notify Engine Fire or Failure In Flight checklist ..................................... Complete Proceed with the SINGLE-ENGINE DESCENT APPROACH checklist On Page 13.

ABNORMAL OIL PRESSURE #1 ENG OIL PRESS or #2 ENG OIL PRESS For 40-55 psi: 1) Power Lever .................................................................................. Flight Idle To reduce in-flight drag: 2) Condition Lever (affected engine)............................................ Start/Feather If the indicated oil pressure is below 40 psi or continuous illumination of the number one or number two ENG OIL PRESS warning light: 3) Complete the engine shut down procedure and accomplish the ENGINE FIRE OR FAILURE AFTER V1 checklist on Page 10 or the ENGINE FIRE OR FAILURE INFLIGHT checklist Page 11 as appropriate.

4) Abnormal Oil Pressure checklist ................................................... Complete


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ECU FAILURE #1 ENG MANUAL or #2 ENG MANUAL After reaching acceleration altitude, and for all subsequent phases of flight: 1) Autofeather Switch .............................................................................. Off 2) Engine ECU Selector .................................................................... NORM 3) ECU Mode Switch (affected engine)............................................ Manual 4) Power Lever (affected engine) ............................................. As Required For approach and landing: 5) Engine ECU Selector ........................................................................TOP

TOP should be selected during the normal descent checklist.

On landing, do not retard Power Lever below Disc.

On the engine with the inoperative ECU: Power lever positions will be asymmetric for symmetric torque. The rate of engine response to power lever advancement will be reduced at altitudes above 15,000 ft and at all altitudes with torque below 50%.  

The following applies to operations above 15,000 ft: Engine surge may be encountered at altitudes above 15,000 ft and is identified by a muffled popping sound and an unscheduled ITT rise on the affected engine. Engine surge can result from rapid power lever motion, particularly with the engine bleed off. To clear engine surge, immediately retard the power lever of the affected engine until the popping sound stops and the ITT decreases. Reset torque by slowly advancing the power lever of the affected engine until the desired torque is achieved. 







6)

ECU Failure checklist................................................................Complete

ENGINE FIRE DETECTOR LOOP FAILURE FAULT A or FAULT B 1) 2)

With the Appropriate Loop Select Knob, select the Non-illuminated Position. Engine Fire Detector Loop Failure checklist .............................Complete

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SINGLE-ENGINE DESCENT APPROACH 1) 2) 3) 4) 5) 6) 7)

ECU ...................................................................................................... TOP Hydraulic Panel ............................................................................... Checked Altimeters ................................... VERIFY ............................ _____ (IN HG) Landing Data.............................. VERIFY ........................... ____, ____ Set Standby Pumps........................................................................................ On Approach Briefing ......................................................................... Complete Single-Engine Descent Approach checklist ................................. Complete

SINGLE-ENGINE LANDING (Challenge-Response-Response) FOR #1 ENGINE INOPERATIVE: 1) Landing Gear ....................................................................................... Down Verify 3 Green Lights Illuminated 2) Flaps ......................................................................................................... 15 3) Condition Lever..................................................................................... MAX 4) Caution Panel ............................................................................ Appropriate

FOR #2 ENGINE INOPERATIVE: 1) PTU .......................................................................................................... On 2) Landing Gear ....................................................................................... Down Verify 3 Green Lights Illuminated 3) PTU .......................................................................................................... Off 4) Flaps ......................................................................................................... 15 5) Condition Lever..................................................................................... MAX 6) Caution Panel ............................................................................ Appropriate

1) 2) 3) 4)

Pressurization Panel ............................................. Checked, Below .5 (PSI) Bleed ........................................................................................................ Off Flaps ......................................................................................................... 15 Single–Engine Landing checklist .................................................. Complete

SINGLE-ENGINE GO-AROUND (SILENT) 1) 2) 3) 4) 5) 6)

Gear ......................................................................................................... Up Flaps ........................................................................................................ Up Bleed (operating engine) ......................................................................... On Power Lever........................................................................ Max Continuous Temps & Pressures ........................................................................Checked Pressurization ................................................................................. Checked (ALOUD)

7) Single-Engine Go-Around checklist .............................................. Complete


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SINGLE-ENGINE AFTER LANDING 1) 2) 3) 4) 5) 6) 7) 8) 9) 10)

Main Bus Tie......................................................................................... On Ice Protection........................................................................................ Off Lights ....................................................................................... As required Flight/Taxi Switch ............................................................................... Taxi AUX Pump ............................................................................................ Off Radar ............................................................................................ Standby Control Lock ......................................................................................... On Flaps ..................................................................................................... Up Transponder ................................................................................. Standby Single-Engine After Landing checklist ........................................Complete

IN FLIGHT ENGINE START Unless an emergency exists, do not restart an engine in the time period of 4 minutes to 25 minutes after shutdown unless Nh is 3% or greater. Use the in flight engine start envelope below.

1) 2) 3) 4) 5) 6) 7) 8) 9) 10) 11) 12) 13)

Sync...................................................................................................... Off Power Lever .............................................................................. Flight Idle Condition Lever ............................................................................ Fuel Off Fuel Off Handle ............................................................................. Push In Ignition ........................................................................................... Manual Bleed switch ......................................................................................... Off AUX Pump ............................................................................................ On Autofeather ........................................................................................... Off Alternate Feather.............................................................................. Norm Bus Tie ............................................................................................... Tied Start Select Switch .......................................................................... Select Engine Start Switch .......................................................................... Press Condition Lever (at 10 to 19% Nh) ....................................... Start/Feather When engine stabilizes: 14) Condition Lever ................................................................................... Min

If prop does not unfeather immediately, select alternate feather/unfeather switch to UNFEATHER. Following prop unfeathering: 15) 16) 17) 18) 19) 20) 21) 22)

Power Lever ............................................................................ As required DC & AC generator caution lights ....................................................... Out AUX Pump ............................................................................................ Off Bleeds................................................................................................... On Ignition Switches...................................................................... As required Bus Tie ................................................................................................. Off Sync...................................................................................................... On In-Flight Engine Start checklist ...................................................Complete

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UNSCHEDULED PROPELLER FEATHERING IN FLIGHT 1) 2) 3)

4)

Power Lever (affected engine) ................................................. Flight Idle Accomplish the engine shut down procedure. Complete the ENGINE FIRE OR FAILURE AFTER V1 checklist on Page 10 or the ENGINE FIRE OR FAILURE INFLIGHT checklist on Page 11 as appropriate. Unscheduled Propeller Feathering In Flight checklist.............. Complete

BETA LOCKOUT FAILURE AFTER V1 1) 2) 3)

Power Lever (affected engine) .. As required to not exceed 100% torque Condition Levers .......................................................................900 RPM Continue the flight with the condition levers at MIN/900 RPM.

Approach and Landing: 4) 5) 6) 7)

Flaps...................................................................................... 15 Degrees Condition Levers .......................................................................900 RPM Landing Distance Factor .................................................. (1.14)Flaps 15 General Landing Distance........................................ 2577 Dry/3350 Wet

Go-Around from Final Approach: 8)

Condition Levers ............................................................................... Max

The RPM of the affected propeller will commence cycling above 1,000 Np. 9)

Power Levers ................................... Advance to Normal Takeoff Power

Adjust the Power Lever of the affected engine to ensure that the peak torque does not exceed 100%. With normal inflight takeoff power set on the non-affected engine, the Power Lever positions will be asymmetric. 10) Once established at 1500 feet, proceed with item 1. 11) Beta Lockout Failure After V1 checklist ................................... Complete


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PROPELLER GROUND RANGE ADVISORY LIGHT CYCLING 1) Power Levers................................................... Advance above Flight Idle 2) Avoid Power Lever positions that result in illumination of ground range advisory lights. 3) Landing Distance Factor .................................................... (1.14)Flaps 15 (1.15)Flaps 35 4) General Landing Distance .........................(Flaps 15) 2577 Dry/3350 Wet (Flaps 35) 2332 Dry/3031 Wet

Do not select affected Power Lever aft of Flight Idle gate on landing. 5) Propeller Ground Range Advisory Light Cycling checklist ......... Complete

PROPELLER OVERSPEED 1) Synchrophase....................................................................................... Off 2) Airspeed ........................................................................................Reduce

Minimum airspeed will be appropriate to flap configuration and flight conditions. 3) 4) 5) 6)

Power Lever (affected engine) .................................................. Flight Idle Condition Lever (affected engine) ............................... START/FEATHER Alternate Feather Switch (affected engine) .............................. FEATHER Power Lever (non-affected engine) As required to maintain desired flight profile

►

If propeller does not feather: -

7) 8) 9) 10)

DO NOT SHUT DOWN THE ENGINE

Alternate Feather Switch (affected engine) ...................................... Norm Condition Levers................................................................................. Max Power Lever (affected engine) ........ Advance. Do not exceed 1212 RPM Power ......... As required to maintain the desired flight profile and reduce airspeed

Power and POWER levers will be asymmetric. 11) Land as soon as possible. 12) Propeller Overspeed checklist....................................................Complete ►

If propeller does feather:

7) Accomplish the engine shutdown procedure. 8) Complete the ENGINE FIRE OR FAILURE AFTER V1 checklist on Page 10 or the ENGINE FIRE OR FAILURE INFLIGHT checklist Page 11 as appropriate. 9) Propeller Overspeed checklist....................................................Complete

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SMOKE BEFORE V1 SMOKE Before V1

1) 2) 3) 4) 5) 6) 7) 8) 9) 10)

Both Power Levers .......................................................................Disc Braking .......................................................... Maximum until stopped Parking Brake ................................................................................ Set Power Levers....................................................................... Flight Idle Condition Levers..................................................................... Fuel Off Notify ATC and Evacuate Cabin. APU/DC External Power ................................................................ Off Battery Master ................................................................................ Off Flight Crew ....................................................... Evacuate as required Smoke Before V1 checklist ................................................. Complete


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SMOKE IN FLIGHT SMOKE In Flight

1) Flight Crew ...................... Suit up & Communicate 2) RECIRC Fan ....................................................Off 3) Cabin Signs ......................................................On On aircraft 914 thru 975, 837 & 838, with MASK selected, PA transmissions can be made with the captain’s side only using the interphone system.

4) 5)

Establish Communications with Flight Attendant Instruct the Flight Attendant on the following: • Turn on the Baggage Compartment Light. • Check the Baggage Compartment Access Door for a possible fire; feel for heat. • If the access door is hot, immediately report to the flight crew. • Otherwise, open the door and check for evidence of a fire. • If required, use the PBE and fire extinguishers located in row 9 to extinguish the fire.

5) If it is determined that there is, or has been a fire, land as soon as possible. 6) AUTO/MAN/DUMP Switch (if necessary) ....... Dump 7) ATC/Company ................................................ Notify

Descend below 14,000 ft as soon as possible 8) Smoke In Flight checklist .......................... Complete

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FUSELAGE FIRE OR SMOKE, KNOWN SOURCE

1) Flight Crew ..................... Suit up & Communicate 2) RECIRC Fan.................................................... Off 3) Cabin Signs ..................................................... On On aircraft 914 thru 975, 837 & 838, with MASK selected, PA transmissions can be made with the captain’s side only using the interphone system. 4) Emergency Lights ................................. As required ►

5) 6) 7)

For Fire or Smoke in Flight Compartment:

Extinguish fire with portable fire extinguishers. Cabin Altitude Manual Control Knob....... Increase Fwd Outflow Valve (if necessary) ................ Open Descend below 14,000 ft as soon as possible

8) 9)

►

5) 6) 7) 8)

ATC/FA/Company........................................Notify Fuselage Fire or Smoke, Known Source checklist .............................................................. Complete For Fire or Smoke in Cabin:

Evacuate passengers from the affected area. Extinguish fire with portable fire extinguishers. Open baggage compartment access door at rear of cabin. AUTO/MAN/DUMP Switch (if necessary) ... Dump Descend below 14,000 ft as soon as possible

9)

ATC/FA/Company........................................Notify

10) Fuselage Fire or Smoke, Known Source checklist .............................................................. Complete


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FUSELAGE FIRE OR SMOKE, UNKNOWN SOURCE

1) 2) 3)

Flight Crew .................... Suit up & Communicate RECIRC Fan .................................................. Off Cabin Signs .................................................... On On aircraft 914 thru 975, 837 & 838, with MASK selected, PA transmissions can be made with the captain’s side only using the interphone system.

4) Emergency Lights................................. As required

To prepare for and manage a landing as soon as possible, the procedures in this checklist may be terminated prior to completion. IF Bleed Source or Air Conditioning Suspected:

5) Bleed Air 1 ..........................................................Off Wait up to one minute. If conditions improve leave bleed air switch off. If conditions improved: 6) Fuselage Fire or Smoke Unknown Source checklist..................................................... Complete ►

If conditions did not improve: 7) Bleed Air 1 ............................................................ On 8) Bleed Air 2 ............................................................ Off Wait up to one minute. If conditions improve leave bleed air switch off. ►

If conditions improved: 9) Fuselage Fire or Smoke, Unknown Source checklist................................................... Complete ►

Continued on next page

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FUSELAGE FIRE OR SMOKE, UNKNOWN SOURCE (Continued) (Continued)

If conditions still do not improve: 9) Bleed Air Switches ........................................... Off 10) Descend below 14,000 ft as soon as possible. 11) Proceed with If source of fire or smoke cannot be identified below . ►

If source of fire or smoke cannot be identified:

5) 6) 7) 8) 9) 10) 11)

Dome Light ........................................ As required Battery Master ................................................. On Main & AUX Batteries ...................................... Off Both DC Generators ........................................ Off Both AC Generators ........................................ Off ATC/FA/Company........................................Notify Land as soon as possible.

Automatic control of cabin altitude is lost. Cabin differential pressure will increase until the safety outflow valve opens. See BATTERY ESSENTIAL SERVICES on Page 30 for list of powered services. 12) Fuselage Fire or Smoke, Unknown Source checklist ................................................ Complete


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MAIN OR AUX BATTERY HOT MAIN BAT HOT or AUX BAT HOT

1) Battery Temp Monitor .............................................. Confirm Overheat 2) Affected Battery switch .................................................................... Off

If battery temperature continues to rise: 3) Land as soon as possible. 4) Main or Aux Battery Hot checklist ..............................................Complete

MAIN BATTERY MAIN BATTERY 1)

Main Battery switch............................................ Off, then to MAIN BATT

If caution light remains on: 2) Main Battery switch............................................................................. Off 3) Main Battery checklist ...............................................................Complete

AUX BATTERY AUX BATTERY 1)

AUX Battery switch ............................................. Off, then to AUX BATT

If caution light remains on: 2) AUX Battery switch ............................................................................. Off 3) AUX Battery checklist ...............................................................Complete

INVERTER FAILURE PRI INV 1) 2) 3)

Auxiliary Inverter switch ......................................................................... L Primary Inverter switch ....................................................................... Off Primary Inverter Failure checklist .............................................Complete SEC INV

1) 2) 3)

Auxiliary Inverter switch ........................................................................ R Secondary Inverter switch .................................................................. Off Secondary Inverter Failure checklist.........................................Complete AUX INV

1) 2)

Auxiliary Inverter switch ...................................................................... Off Auxiliary Inverter Failure checklist ............................................Complete

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ONLY TO BE USED ON AIRCRAFT THAT HAVE 400 HZ BUS MOD INSTALLED ON AIRCRAFT. REFERENCE FLIGHT RELEASE FOR SIL.

INVERTER FAILURE PRI INV 1) Primary Inverter switch ......................................................................... Off 2) Auxiliary Inverter switch ........................................................................... L 3) Primary Inverter Failure checklist .............................................. Complete

SEC INV 1) Secondary Inverter switch .................................................................... Off 2) Auxiliary Inverter switch .......................................................................... R 3) Secondary Inverter Failure checklist.......................................... Complete

AUX INV 1) Auxiliary Inverter switch ........................................................................ Off

With the Auxiliary Inverter switch selected L or R and a failure of the primary, secondary, or auxiliary inverter, both associated inverters may indicate failed (illumination of PRI INV and AUX INV or SEC INV and AUX INV caution lights). Selection of PRI INV or SEC INV switch OFF, may result in the AUX INV caution light extinguishing. If caution light remains on: 2) Auxiliary Inverter switch ........................................................................ Off 3) Auxiliary Inverter Failure checklist ............................................. Complete

DASH 8 102 Emergenc y/Non-Normal Checklis t TEMPORARY AMENDMENT (TA)

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(Page Intentionally Left Blank)

TRU FAILURE L TRU or R TRU 1) 2)

Pull the appropriate L TRU or R TRU circuit breaker (located on the 115v variable AC circuit breaker panel on the right rear bulkhead). TRU Failure checklist ............................................................... Complete

TRU HOT L TRU HOT or R TRU HOT 1) 2)

Pull the appropriate L TRU or R TRU Circuit Breaker (located on the 115v variable AC circuit breaker panel on the right rear bulkhead). TRU Hot checklist..................................................................... Complete

AC or DC GENERATOR HOT #1 DC GEN HOT or #2 DC GEN HOT #1 AC GEN HOT or #2 AC GEN HOT 1)

Affected DC or AC Generator switch .................................................. Off

Continued operation of the engine after the generator is switched OFF is permissible for the remainder of the flight. The affected DC GEN HOT or AC GEN HOT caution light may remain illuminated. 2)

AC or DC Generator Hot checklist ........................................... Complete

AC GENERATOR FAILURE #1 AC GEN or #2 AC GEN 1)

Affected AC Generator switch .............................................. Off, then On

After selecting the affected AC Generator switch back to ON, it may be necessary to cycle the synchrophase switch to maintain propeller synchronization. If caution light remains on: 2) Affected AC Generator switch ............................................................. Off 3) AC Generator Failure checklist ................................................ Complete


05/29/15

23

DC GENERATOR FAILURE #1 DC GEN or #2 DC GEN 1)

Affected DC Generator switch ............................................. Off, then On

If caution light remains on: 2) Affected DC Generator switch ............................................................ Off 3) DC Generator Failure checklist.................................................Complete

LOSS OF BOTH DC GENERATORS #1 DC GEN AND #2 DC GEN

1)

DC Generators ................................................. Off then On (individually)

If caution lights remain on: 2) Affected DC Generators ..................................................................... Off 3) AUX and Main Battery switches ......................................................... Off

With the Battery Master switch OFF, failure of one TRU will cause loss of all electrical power until the Battery Master switch is selected ON. The AHRS will require a 3 minute re-initialization before displaying valid attitude and heading data. 4) 5) 6)

Battery Master switch ......................................................................... Off Land as soon as practicable. Loss of Both DC Generators checklist......................................Complete

LOSS OF BOTH DC GENERATORS AND ONE TRU #1 DC GEN + #2 DC GEN + L TRU or R TRU

1)

DC Generators ................................................. Off then On (individually)

If caution lights remain on: 2) Battery Master switch ......................................................................... On 3) AUX Battery and Main Battery switches ............................................. Off 4) Land as soon as possible.

See BATTERY ESSENTIAL SERVICES on Page 30 for list of powered services. Automatic control of cabin altitude is lost. Cabin differential pressure will increase until the safety outflow valve opens. When below 14,000 ft use manual pressurization control to depressurize cabin. 5)

Loss of Both DC Generators and One TRU checklist ..............Complete

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05/29/15

LOSS OF BOTH TRU’S AND ONE DC GENERATOR L TRU + R TRU + #1 DC GEN or #2 DC GEN 1)

Emergency Lights switch ...................................................... On then Off

If emergency lighting is required: 2) Emergency Lights switch .................................................................... On 3) Loss of Both TRU’s and One DC Generator checklist ............. Complete

LOSS OF BOTH DC GENERATORS AND BOTH TRU’S #1 DC GEN + #2 DC GEN + L TRU + R TRU + AUX INV 1)

DC Generators and AC Generators ................. Off then On (individually)

If caution lights remain on: 2) Storm Lights switch .....................................................................STORM 3) Battery Master switch .......................................................................... On 4) AUX and Main Battery switches.......................................................... Off 5) Emergency Lights switch ..................................................... On, then Off 6) Pull the following circuit breakers on the Left Avionics Circuit Breaker panel: TCAS PLT IVSI CO-PLT IVSI   

If emergency lighting is required: 7) Emergency Lights switch .................................................................... On 8) Land as soon as possible.


Loss of Both DC Generators and Both TRU’s checklist........... Complete


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25

LOSS OF BOTH DC GENERATORS AND BOTH AC GENERATORS #1 DC GEN + #2 DC GEN + L TRU + R TRU + #1 AC GEN + #2 AC GEN + AUX INV 1)

DC Generators and AC Generators................. Off then On (individually)

If caution lights remain on: 2) Storm Lights switch..................................................................... STORM 3) Battery Master switch ......................................................................... On 4) AUX and Main Battery switches ......................................................... Off 5) Emergency Lights switch ..................................................... On, then Off If emergency lighting is required: 6) Emergency Lights switch .................................................................... On 7) Land as soon as possible.


Loss of Both DC Gens and Both AC Gens checklist ................Complete

MULTIPLE INVERTER FAILURE PRI INV + SEC INV + AUX INV + L 26 AC + R 26 AC

1)

115V BUS TIE circuit breaker (top of avionics circuit breaker panel) ................................................ Pull

PRI INV and/or SEC INV and/or AUX INV caution lights remain illuminated: 2)

Affected PRI, SEC or AUX INV switches............................................ Off

If the AUX INVERTER is operative: 3)

AUX INVERTER switch ............................... Select L or R appropriate to the illuminated L26 AC or R26 AC caution light.

With one or more inverters operating (PRI INV and/or SEC INV and/or AUX INV) caution lights extinguished: 4)

115V BUS TIE circuit breaker .......................................................... Push

Check L26 AC and R26 AC caution lights out. 5) Monitor inverter VOLTS and LOAD. 6) Multiple Inverter Failure checklist ...............................................Complete

26


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DC BUS FAILURE DC BUS with no other associated lights 1)

Allow 10 seconds for BBPU to operate.

If no other caution lights illuminate: 2) Bus Fault Reset switch........................................................ Select Reset 3) DC Bus Failure checklist .......................................................... Complete

LEFT MAIN BUS FAILURE DC BUS + #1 DC GEN + AUX BATTERY + AUX INV 1) 2) 3)

AUX Battery switch ............................................................................. Off #1 DC Generator switch ...................................................................... Off Bus Fault Reset switch........................................................ Select Reset

If DC BUS caution light goes out: Power is restored to the Left DC Bus. Leave AUX Battery and #1 DC Generator switches in the OFF position. If DC BUS caution light remains illuminated: Power has not been restored to the Left DC Bus. Leave the AUX Battery and #1 DC Generator switches in the OFF position and land as soon as possible. 4)

Left Main Bus Failure checklist ................................................ Complete

RIGHT MAIN BUS FAILURE DC BUS + #2 DC GEN + MAIN BATTERY 1) 2) 3)

Main Battery switch ............................................................................. Off #2 DC Generator switch ...................................................................... Off Bus Fault Reset switch........................................................ Select Reset

If DC BUS caution light goes out: Power is restored to the Right DC Bus. Leave Main Battery and #2 DC Generator switches in the OFF position. If DC BUS caution light remains illuminated: Power has not been restored to the Right DC Bus. Leave the Main Battery and #2 DC Generator switches in the OFF position and land as soon as possible. Proceed with the Inboard or Outboard Anti-Skid Failure checklist on Page 44. 4)

Right Main Bus Failure checklist .............................................. Complete


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27

26 AC BUS FAILURE L 26 AC or R 26 AC 1) AUX Inverter switch ....................................... Select to the operating side The fault could lie with the 26vac bus, the 115vac fixed frequency bus, or the step-down transformer. The following is a list of 115v and 26v AC services: Left 115vac: Flight Data Recorder SYM GEN 1 (bearing pointer and CDI bar) ADVSY 1 FAN GPWS F/A Panel Lighting     

Left 26vac: #1 ADI #1 HSI #1 Altimeter #1 VHF NAV #1 ADF #1 and #2 RMI PFCS Indicator #1 Hydraulic quantity indicator & transmitter        

Right 115vac: Weather Radar SYM GEN 2 (bearing pointer and CDI bar) Cockpit Voice Recorder ADVSY 2 FAN    

Right 26vac: #2 ADI #2 HSI #2 Altimeter #2 VHF NAV #1 and #2 RMI #2 Hydraulic quantity indicator & transmitter      

2)

26 AC Bus Failure checklist .......................................................Complete

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115V AC VARIABLE FREQUENCY BUS FAILURE Crew awareness if flying in icing conditions. L AC BUS A Left 115vac Variable Frequency Bus failure will result in the loss of the following services:          

Left auxiliary fuel pump Left propeller deicing Left stall transducer heater Right standby hydraulic pump Left TRU Pilot's side window heat Pilot's windshield heat (full & warm-up) Left engine intake heater Copilot's windshield heat (warm-up) Left elevator horn heat

R AC BUS A Right 115vac Variable Frequency Bus failure will result in the loss of the following services:        

1)

Right auxiliary fuel pump Right propeller deicing Right stall transducer heater Left standby hydraulic pump Right TRU Copilot's windshield heat (full) Right engine intake heater Right elevator horn heat

115V AC Variable Frequency Bus Failure checklist ................ Complete


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29

BATTERY ESSENTIAL SERVICES

Battery Duration for Operation of Essential Services is 30 Minutes.

-

SAHS, ADF, VSI and TCAS are not available. On Electromechanical Instruments the Flight Director Command Bars park at the 90° Position and should be ignored.

With BATTERY MASTER switch at BATTERY MASTER, MAIN and AUX battery switches OFF the following services are powered: Flight instruments: AHRS 1 & 2 (Basic) Left and Right ADI’s & HSI’s Standby Altimeter Standby Attitude Indicator Clock 1     

Comm and Nav: VHF Comm 1 VHF Nav 1 Pilot and Copilot Audio PA & Cabin Interphone Audio    

Lights:         

Position Lights Emergency Lights Storm Lights Flight Compartment Dome Lights Caution/Warning Lights Advisory Lights Circuit Breaker Panel Lights Passenger Signs Baggage Compartment Lights

Hydraulics: Hydraulic Power Transfer (PTU) Hydraulic Pressure Indication Hydraulic Quantity Indication Landing Gear Control & Indication    


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BATTERY ESSENTIAL SERVICES (Continued) (Continued) Flight Controls: Aileron Trim Actuation & Indication Rudder Trim Actuation & Indication Elevator Standby Trim Flap Control & Indication Roll Spoilers Emergency Control Roll Spoilers Ground Mode Arm PFCS Indication       

Engines and Fuel: Engine Instruments: Torque, ITT, Np, Nh, NL, Oil Temp, Oil Pressure Engine Ignition & Start Engine ECU’s Fuel & Hydraulic Shut-off Valves Fuel Quantity Indication 

   

Anti-ice: Pitot Heat 1 

Fire Protection: Engine Fire Detect & Extinguish Smoke Detectors  

Miscellaneous: Battery Temp Indicator Flight Data Recorder (FDR) Cockpit Voice Recorder (CVR)   

1)

Battery Essential Services checklist......................................... Complete


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31

#1 HYDRAULIC SYSTEM FAILURE #1 ENG HYD PUMP and/or #1 HYD ISO VLV

#1 HYD ISO VLV caution light may go out with very low hydraulic fluid quantity in the number 1 hydraulic system. 1) #1 Hydraulic Quantity ...................................................................... Check If quantity is normal:

►

2) #1 Standby Pump ................................................................................. On 3) Normal operating procedures apply.

Operation of the flaps with the #1 Standby Pump may cause sporadic illumination of the FLAP POWER caution light. Flap movement will be slow and may require additional activation of the flap handle trigger. 4) #1 Hydraulic System Failure checklist........................................Complete If pressure is normal and quantity is low:

►

Expect the loss of the following systems: Flaps Anti-skid PTU Inboard Roll Spoilers Normal Brakes     

For a zero flap approach and landing with the #1 system failed: 2) GPWS flap override switch ............................................................. Press

Check that the GPWS Flap Override advisory light illuminates. 3) 4) 5) 6) 7) 8)

Approach speed and Vref = Vref (flaps 0) + 10 V2 for Flaps 0 is _______ Power should be reduced gradually to Flight Idle at or just prior to touchdown. Max pitch at touchdown ........................................................................8° Use max discing. Use reverse as required. Use emergency brake judiciously (unlimited brake application available).

There will be no differential braking. There will be no anti-skid control. Excessive application can result in skidding and tire failure. 9) Landing Distance Factor (use Flaps 35 landing data) ........ (3.32)Flaps 0 10) General Landing Distance ........................................ 6730 Dry/8749 Wet Continued on next page

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#1 HYDRAULIC SYSTEM FAILURE (Continued) (Continued) 11) After landing: GPWS flap override switch .......................................................Press Off 12) #1 Hydraulic System Failure checklist...................................... Complete If pressure is low and quantity is ZERO:

►

Expect the loss of the following systems: Flaps Anti-skid Rudder Actuator #1 PTU Inboard Roll Spoilers Normal Brakes      

2) 3)

#1 Standby Pump ................................................................................ Off Maximum allowable speed is 200 KIAS.

For a zero flap approach and landing with the #1 system failed: 4) GPWS flap override switch............................................................. Press

Check that the GPWS Flap Override advisory light illuminates. 5) 6) 7)

Approach speed and Vref = Vref (flaps 0) + 10 V2 for Flaps 0 is _______ Power should be reduced gradually to Flight Idle at or just prior to touchdown. 8) Max pitch at touchdown ........................................................................ 8° 9) Use max discing. Use reverse as required. 10) Use emergency brake judiciously (unlimited brake application available).

-

There will be no differential braking. There will be no anti-skid control. Excessive application can result in skidding and tire failure.

11) Landing Distance Factor (use Flaps 35 landing data) ........ (3.32)Flaps 0 12) General Landing Distance ........................................ 6730 Dry/8749 Wet 13) After landing: GPWS flap override switch .......................................................Press Off 14) #1 Hydraulic System Failure checklist...................................... Complete


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33

#2 HYDRAULIC SYSTEM FAILURE #2 ENG HYD PUMP and/or #2 HYD ISO VLV

#2 HYD ISO VLV caution light may go out with very low hydraulic fluid quantity in the number 2 hydraulic system. 1) ►

#2 Hydraulic Quantity..................................................................... Check If quantity is normal:

2) 3)

#2 Standby Pump................................................................................ On Normal operating procedures apply.

When operating on #2 Standby Pump, use the LANDING GEAR EXTENSION USING THE PTU checklist on Page 39 to extend the landing gear. 4) #2 Hydraulic System Failure checklist ......................................Complete If pressure is normal and quantity is low:

►

Expect the loss of the following systems: Nose Wheel Steering Outboard Roll Spoilers Landing Gear (normal operation) Emergency/Parking Brake (if brake pressure is zero)    

For approach and landing with #2 system failed: 2) Add 6 knots to Vref. 3) Use max discing. 4) Landing Distance Factor ................................................... (1.52)Flaps 15 (1.55)Flaps 35 5) General Landing Distance........................(Flaps 15) 3436 Dry/4466 Wet (Flaps 35) 3142 Dry/ 4085 Wet Use the ALTERNATE LANDING GEAR EXTENSION checklist on Page 38. 6) ►

#2 Hydraulic System Failure checklist ......................................Complete If pressure is low and quantity is ZERO:

Expect the loss of the following systems: Nose Wheel Steering Outboard Roll Spoilers Rudder Actuator #2 Landing Gear (normal operation) Emergency/Parking Brake (if brake pressure is zero)     

2) #2 Standby Pump ................................................................................. Off 3) Maximum allowable speed is 200 KIAS.


34


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#2 HYDRAULIC SYSTEM FAILURE (Continued) (Continued)

For approach and landing with #2 system failed: 4) Add 6 knots to Vref. 5) Use max discing. 6) Landing Distance Factor .................................................... (1.52)Flaps 15 (1.55)Flaps 35 7) General Landing Distance ........................ (Flaps 15) 3436 Dry/4466 Wet (Flaps 35) 3142 Dry/4085 Wet Use the ALTERNATE LANDING GEAR EXTENSION checklist on Page 38. 8) #2 Hydraulic System Failure checklist ....................................... Complete

HYDRAULIC FLUID HOT #1 HYD FLUID HOT or #2 HYD FLUID HOT 1) 2)

Monitor pressure and quantity of affected system. Hydraulic Fluid Hot checklist .................................................... Complete

STANDBY HYDRAULIC PUMP HOT #1 STBY HYD PUMP HOT or #2 STBY HYD PUMP HOT 1)

Check flap selector lever.

If set greater than 0°, no action is required. If set at 0°: 2) Associated Standby Pump .................................................................. Off 3) Standby Hydraulic Pump Hot checklist .................................... Complete


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35

PARTIAL LOSS OF HYDRAULIC FLUID FROM BOTH SYSTEMS #1 HYD ISO VLV + #2 HYD ISO VLV When both Hydraulic Rudder Isolation Valves activate, approximately onehalf quart of fluid remains in each system’s reservoir and the #1 and #2 Rudder Actuators are the only functions on the #1 and #2 system that will continue to operate. 1) 2) 3)

Both Standby Pumps .......................................................................... On Control aircraft using aileron, elevator and rudder. For landing with Flaps 0° or 5°: GPWS Flap Override Switch ........ Press

Check that the GPWS Flap Override advisory light illuminates. 4)

Land as soon as possible at an airport with minimum turbulence and crosswind.

For approach and landing with both systems isolated: 5) Use the ALTERNATE LANDING GEAR EXTENSION checklist on Page 38. 6) Approach speed and Vref = Flaps 0°............................................................................... Vref + 10 Flaps 5°.................................... Vref(Flaps 0) (Not less than 105kts) Flaps 15° ........................................ Vref + 10 (Not less than 100kts) 7) V2 speed for Flaps ___ is ____ knots. 8) Power should be reduced gradually to Flight Idle at or just prior to touchdown 9) Max pitch at touchdown ........................................................................8° 10) Use max discing. Use reverse as required.   

If landing with one engine inoperative, use discing and reverse commensurate with directional control. 11) Use Emergency Brake judiciously (approximately 6 brake applications available).

-

There will be no differential braking. There will be no anti-skid control. Excessive application can result in skidding and tire failure.

Directional control on the ground is available from differential power only, once the rudder loses aerodynamic effectiveness. The approximate number of emergency brake lever applications is six.


36


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PARTIAL LOSS OF HYDRAULIC FLUID FROM BOTH SYSTEMS (Continued) (Continued) 12) Landing Distance Factor (use Flaps 35 landing data) ........ (3.32)Flaps 0 (2.87)Flaps 5 13) General Landing Distance ......................... (Flaps 0) 6730 Dry/8749 Wet (Flaps 5) 5818 Dry/7563 Wet 14) Landing Distance Factor................................................... (2.54)Flaps 15 15) General Landing Distance ....................... (Flaps 15) 5741 Dry/7463 Wet After landing: 16) GPWS flap override switch ........................................................Press Off 17) Partial Loss of Hydraulic Fluid from Both Systems checklist ... Complete


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37

ALTERNATE LANDING GEAR EXTENSION Loss of #2 Hydraulic Quantity or Landing Gear Malfunction or LDG GEAR INOP

On aircraft 815 & 816 the TAXI light switch must be OFF when confirming the nose gear is down and locked using the alternate landing gear indication system.

Landing Gear cannot be retracted following extension by Alternate Extension Procedure. Do not select PTU to Manual during approach. Nose Wheel Steering is inoperative following Alternate Landing Gear Extension. The main/nose gear release handle pull force will be significantly higher than experienced during practice alternate landing gear extensions. The required pull force, to release the main/nose gear uplocks, can be as high as 90 pounds. It may require repeated pull effort to achieve a main/nose landing gear down and locked indication.

1) 2) 3) 4)

Airspeed ......................................................................... 140 KIAS (max) LDG GEAR INHIBIT Switch ........................................................... Inhibit Landing Gear Selector Lever .......................................................... Down Main Gear Release Handle.......................... Open door & pull fully down If LEFT and/or RIGHT green gear locked down advisory lights do not to illuminate, insert hydraulic pump handle in socket and operate until green LEFT and RIGHT green gear locked down advisory lights illuminate.

5)

Nose Gear Release Handle ............................. Open door & pull fully up Leave landing gear alternate release and landing gear alternate extension doors fully open and landing gear inhibit switch at Inhibit.

6) 7) 8) 9)

Landing Gear Alternate Verification ................................. On/3 green/Off Anti-Skid Switch ................................................................................ Test Flaps .................................................................................................... 15 Condition Levers ............................................................................... Max

IF it cannot be confirmed that the landing gear is down and locked proceed to the LANDING GEAR FAILS TO EXTEND checklist on Page 41. After Landing: 10) As soon as possible after engine shutdown install main-gear safetylock pins, and engage nose-gear lock. 11) Alternate Landing Gear Extension checklist .............................Complete

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LANDING GEAR EXTENSION USING THE PTU 1) 2) 3) 4) 5) 6) 7) 8)

#2 Standby Pump................................................................................ On Manual PTU switch ........................................................................ Press Check illumination of the HYD PWR TRANSFER advisory light Landing gear selector lever ............................................................ Down Confirm that all three green “gear locked down” advisory lights illuminate. Confirm that all amber door-open, red gear-unsafe, and gear selector handle advisory lights are extinguished. Manual PTU switch ........................................................................ Press Check that HYD POWER TRANSFER advisory light is extinguished.

Continuous operation of the PTU should be limited to a maximum of 5 minutes 9)

Landing Gear Extension Using the PTU checklist ................... Complete

LANDING GEAR INDICATOR MALFUNCTION If any of the green “gear locked down” advisory lights fails to illuminate: 1) 2) 3) 4) 5)

Open the Landing Gear Alternate Extension Door located on the floor. Alternate “gear locked down” indicator switch .................................... On Check for illumination of all three “gear locked down” lights. Alternate “gear locked down” indicator switch .................................... Off Close the Landing Gear Alternate Extension Door.

Illumination of the alternate “gear locked down” indicator lights is a positive confirmation that the gear are down & locked. An external visual check is not required. 6)

Landing Gear Indicator Malfunction checklist .......................... Complete


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39

ILLUMINATION OF AMBER DOOR ADVISORY LIGHT(S) If more than one amber door advisory lights remains illuminated proceed to the ALTERNATE LANDING GEAR EXTENSION Checklist on Page 38. On Landing Gear retraction: 1) 2) 3) 4) 5) 6)

Limit airspeed to 140 KIAS and, when appropriate, select Flaps to 0°. If the amber door advisory light stays on, select the Gear down. If the amber door advisory light stays on, leave the Gear down. If the amber door advisory light goes out, retract the Gear. If the amber door advisory light re-illuminates, limit airspeed to 140 KIAS. Illumination of Amber Door Advisory Light checklist.................Complete

On Landing Gear extension: 1) 2) 3)

Maximum airspeed ................................................................... 140 KIAS Complete flight with Landing Gear down. Illumination of Amber Door Advisory Light checklist.................Complete

ILLUMINATION OF RED LANDING GEAR UNSAFE LIGHT(S) If any red landing gear unsafe light remains illuminated: 1) 2)

Proceed to the ALTERNATE LANDING GEAR EXTENSION checklist on Page 38. Illumination of Red Landing Gear Unsafe Light(s) checklist ..... Complete

ALL LANDING GEAR FAIL TO RETRACT If all 3 green Gear Locked Down advisory lights are illuminated with the landing gear lever selected up:

Landing gear doors may be open or closed (amber doors open advisory lights illuminated or out). If the landing gear alternate release door is open, the landing gear will not retract.

1) 2) 3) 4) 5)

Landing Gear selector lever............................................................ Down Confirm 3 green gear locked down advisory lights remain illuminated. Do not select the landing gear back up. Land as soon as practicable. All Landing Gear Fail To Retract checklist ...............................Complete

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LANDING GEAR FAILS TO EXTEND This checklist is to be used after the ALTERNATE LANDING GEAR EXTENSION checklist has been performed in addition to troubleshooting directed by Maintenance Control and the flight crew cannot verify that the landing gear is down and locked. When it is known that a landing must be performed which could be identified as an emergency landing due to the presence of factors which introduce a hazard to the airplane and its occupants the following points should be addressed as applicable. 1) Instruct Flight Attendant to brief and prepare passengers appropriate to the emergency. 2) If possible, ensure that no passengers are seated adjacent to the propeller arc. 3) Secure all loose items in the flight compartment and cabin. 4) Complete all necessary radio communications concerning the intended landing with ground support personnel. 5) Review the procedures to be followed covering all aspects of crew actions and coordination. 6) Consider the applicability or suitability of a practice approach and overshoot. 7) Ensure that both pilot and copilot harnesses are secure and locked. 8) Deactivate the GPWS by pulling EGPWS ANNUC circuit breaker B3 and EGPWS COMP (A3, H3, J3, or M3) on the left main circuit breaker panel. 9) Deactivate the LDG GEAR HORN circuit breaker E5 on the left main circuit breaker panel. 10) Cabin altitude Auto/Man/Dump switch ............................................. Dump 11) Emergency light switch ......................................................................... On IF landing with the Nose Landing Gear UP or Unsafe and the Main Landing Gear Down: It is possible to safely land the airplane with the nose gear retracted. The geometry of the airplane is such that the propellers will not come in contact with the ground with the main landing gear extended. The following items should be considered:  

   





Reduce landing weight through fuel burn. Attempt to achieve an aft CG by moving passengers towards the rear of the aircraft. Select a runway with minimal crosswind. Land with flap 35°. Fly the appropriate VREF for the landing weight. Touchdown offset from the runway centerline if the runway is equipped with a centerline lighting system. On touchdown, hold the nose up off the runway as long as possible. Prior to losing elevator effectivity, gently lower the nose onto the runway. If the nose landing gear is not extended or collapses, maintain directional control with rudder until it is no longer effective, at which point asymmetric braking may be used as required. Continued on next page


05/29/15

41

LANDING GEAR FAILS TO EXTEND (Continued) (Continued) 

Apply brake or reverse thrust only after the nose wheel is on the ground and appears to be locked. If the nose landing gear is not extended or it collapses, apply brakes only.

After ground contact: 12) 13) 14) 15) 16)

Condition Levers ......................................................................... Fuel Off Both Fuel Off Handles ....................................................................... Pull Battery Master switch ......................................................................... Off Evacuate Landing Gear Fails to Extend checklist ....................................Complete

IF One Main Landing Gear Unsafe, Nose Landing Gear and Opposite Main Landing Gear Down and Locked: The flight crew must assume and prepare for the gear to collapse on landing. The following items should be considered:  



  





Reduce landing weight through fuel burn. Passengers should be moved from the seats in the arc of the propellers and re-seated elsewhere in the cabin (if possible). Priority is to be given to the passengers seated on the side with the indicated unsafe main landing gear. Crosswind (if any) would be advantageous from the side with the unaffected main landing gear. Land with flap 35°. Fly the appropriate VREF for the landing weight. Giving due regard to the specific approach to be flown, flight conditions and possible missed approach; prior to commencing the final approach, feather and secure the engine on the side with the affected main landing gear (use immediate action items to shutdown engine). On touchdown, maintain maximum wing down lateral control on the side with the unaffected main landing gear. If the landing gear collapses, in an effort to reduce the airplane turning moment in the direction of the failed main landing gear, apply maximum braking and reverse thrust on the side with the unaffected main landing gear. Be prepared to perform the ENGINE FIRE BEFORE V1 immediate action items on Page 9.

After ground contact: 12) 13) 14) 15) 16) 17)

Perform Engine Fire Before V1 immediate action items if necessary. Condition Levers ......................................................................... Fuel Off Both Fuel Off Handles ....................................................................... Pull Battery Master switch ......................................................................... Off Evacuate Landing Gear Fails to Extend checklist ....................................Complete Continued on next page

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LANDING GEAR FAILS TO EXTEND (Continued) (Continued) IF Performing an All Gear Up Landing: It is possible to safely land the airplane with all gear retracted. The geometry of the airplane is such that the propellers should not come in contact with the ground with all landing gear retracted if it is possible to maintain the wings level throughout the landing. The following items should be considered:  

   





Reduce landing weight through fuel burn. Passengers should be moved from the seats in the arc of the propeller and reseated elsewhere in the cabin (if possible). Select a runway with minimal crosswind. Land with flap 35°. Fly the appropriate VREF for the landing weight. Touchdown offset from the runway centerline if the runway is equipped with a centerline lighting system. Maintain a nose-up pitch attitude not exceeding 5° prior to runway contact. On touchdown, maintain wings level using lateral control and directional control with rudder.

After ground contact: 12) 13) 14) 15) 16)

Condition Levers ......................................................................... Fuel Off Both Fuel Off Handles ........................................................................Pull Battery Master switch .......................................................................... Off Evacuate Landing Gear Fails to Extend checklist.................................... Complete


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43

WEIGHT ON WHEELS WT ON WHEELS 1)

Complete flight with WT ON WHEELS caution light illuminated.

Landing gear may not retract with WT ON WHEELS caution light illuminated. Illumination of WT ON WHEELS caution light at any time in flight requires rectification before the next flight, even though caution light may go out on touchdown. 2)

Weight on Wheels checklist ......................................................Complete

INBOARD OR OUTBOARD ANTI-SKID INBD ANTI SKID or OUTBD ANTI SKID

With either caution light on, anti-skid control is reduced by 50% 1) 2) 3) 4)

Anti-Skid switch ................................................................................... On Pedal Brakes ............................................ Apply using manual technique Landing Distance Factor ................................................... (1.54)Flaps 15 (1.43)Flaps 35 General Landing Distance........................(Flaps 15) 3481 Dry/4525 Wet (Flaps 35) 3122 Dry/3769 Wet

Excessive application of Pedal Brakes can result in skidding and tire failure.

For maximum deceleration with reduced anti-skid control, brakes should be applied intermittently, with the duration of each application approximately one second, with intervals of reduced braking as brief as possible 5)

Inboard or Outboard Anti-Skid checklist ...................................Complete

44


05/29/15

NOSEWHEEL STEERING FAILURE NOSE STEERING 1) 2)

Steering handle and nose wheel ................................................... Center If necessary, Steering switch................................................ Off, then On

If NOSE STEERING caution light remains illuminated: 3)

Steering switch .................................................................................... Off

Taxi the aircraft using differential braking and power. 4) Nosewheel Steering Failure checklist ...................................... Complete


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45

PITCH CONTROL JAM 1) AUTOPILOT ............................................................. Verify Disengaged 2) PITCH DISCONNECT ................................................ Pull and Turn 90° 3) Retain Flap Setting and approximate Airspeed at time of Jam.

With the Pitch Disconnect Handle pulled, the Autopilot must be disengaged.

Elevator control forces will be lighter and pitch control degraded. If jam occurs below 150 KIAS ................................................ 150 KIAS (max) If jam occurs above 150 KIAS ........................... Airspeed at time of jam (max) If elevator is free and floating ................................................. 180 KIAS (max) ►

If the jam occurs with flaps 0° or 5°:

4) 5) 6)

Do not change flap setting Land at airport with minimal crosswind and turbulence GPWS flap override switch ............................................................. Press

Check that the GPWS Flap Override advisory light illuminates. 7)

Approach speed and Vref = Flaps 0° ................................................................ Vref (flaps 0) + 10 Flaps 5° ........................................................................ Vref (flaps 0) V2 speed for Flaps ___ is ____ knots. Power should be reduced gradually to Flight Idle at or just prior to touchdown. Max pitch at touchdown ........................................................................8° Use max discing. Use reverse as required. Landing Distance Factor: Flaps 0° (use Flaps 35 landing data) ........................... (2.90)Flaps 0 Flaps 5° (use Flaps 35 landing data) ........................... (1.88)Flaps 5 General Landing Distance..........................(Flaps 0) 5879 Dry/7642 Wet (Flaps 5) 3811 Dry/4954 Wet  

8) 9) 10) 11) 12)

 

13)

After landing: 14) GPWS flap override switch ....................................................... Press Off 15) Pitch Control Jam checklist .......................................................Complete ►

If the jam occurs with flaps 15°:

4) 5) 6) 7) 8) 9)

Do not change flap setting. Land at airport with minimum crosswind and turbulence. Use normal Vref (flaps 15) speed. Landing Distance Factor ................................................... (1.10)Flaps 15 General Landing Distance ........................................ 2486 Dry/3232 Wet Pitch Control Jam checklist .......................................................Complete

46


05/29/15

ROLL CONTROL JAM 1) AUTOPILOT ........................................................... Verify Disengaged 2) ROLL DISCONNECT................................................ Pull and Turn 90°

With the Roll Disconnect Handle pulled, the Autopilot must not be engaged. The pilot with the free control wheel will have roll control. ►

If the Right control wheel is free:

3) SPLR 1 + SPLR 2 PUSH OFF switch-lights: If illuminated............................................................................ Push Off 4)

Check for illumination of ROLL SPLR INBD HYD and

7) 8) 9)

ROLL SPLR OUTBD HYD and that PFCS indicator shows all spoilers retracted. Roll control will be degraded and forces will be normal. Land at an airport with minimal crosswind and turbulence using flaps 15°. Landing Distance Factor .................................................. (1.17)Flaps 15 General Landing Distance ........................................ 2645 Dry/3438 Wet Roll Control Jam checklist ........................................................ Complete

►

If the Left Control Wheel is free:

3)

Roll control forces will be low and tendencies to over-control should be avoided. Land at an airport with minimal crosswind and turbulence using flaps 15° or 35°. Roll Control Jam checklist ........................................................ Complete

5) 6)

4) 5)


05/29/15

47

ROLL CONTROL MALFUNCTION 1)

Apply Roll Control as required to hold wings level.

►

If SPLR 1 or SPLR 2 PUSH OFF switch light is illuminated: Appropriate switch light .............................................................. Push Off Check for illumination of ROLL SPLR INBD HYD or

2) 3)

4) 5) 6) 7) ►

2) 3) 4) 5) 6) 7) 8)

ROLL SPLR OUTBD HYD and that PFCS indicator shows appropriate spoilers retracted. Land at airport with minimal crosswind and turbulence using flaps 15° or 35°. Landing Distance Factor ................................................... (1.16)Flaps 15 (1.18)Flaps 35 General Landing Distance........................(Flaps 15) 2622 Dry/3409 Wet (Flaps 35) 2392 Dry/3110 Wet Roll Control Malfunction checklist .............................................Complete If SPLR 1 or SPLR 2 switch light is not illuminated: Apply Power as required Increase Airspeed as required Land at airport with minimal crosswind and turbulence using flaps 15° or 35°. Add 10 knots to approach speed and Vref. Landing Distance Factor ................................................... (1.55)Flaps 15 (1.56)Flaps 35 General Landing Distance........................(Flaps 15) 3503 Dry/4554 Wet (Flaps 35) 3163 Dry/4111 Wet Roll Control Malfunction checklist .............................................Complete

SPOILER CABLE FAILURE ROLL SPLR INBD HYD + ROLL SPLR OUTBD HYD 1)

SPLR 1 AND SPLR 2 PUSH OFF switch lights........................... Push Off

Switch Light will not be illuminated 2) 3) 4) 5) 6)

Check PFCS indicator shows all spoilers retracted. Land at an airport with minimum crosswind and turbulence using Flaps 15°. Landing Distance Factor ...................................................... (1.17)Flaps 15 General Landing Distance ........................................... 2645 Dry/3438 Wet Spoiler Cable Failure checklist..................................................... Complete

48


05/29/15

INBOARD OR OUTBOARD ROLL SPOILER MALFUNCTION ROLL SPLR INBD HYD 1)

SPLR 1 PUSH OFF switch light ................................................Push Off

Switch Light will not be illuminated 2) 3) 4) 5)

Add 6 knots to Vref. Landing Distance Factor .................................................. (1.52)Flaps 15 (1.55)Flaps 35 General Landing Distance ....................... (Flaps 15) 3436 Dry/4466 Wet (Flaps 35) 3142 Dry/4085 Wet Inboard Roll Spoiler Malfunction checklist ............................... Complete ROLL SPLR OUTBD HYD

1)

SPLR 2 PUSH OFF switch light ................................................Push Off

Switch Light will not be illuminated 2) 3) 4) 5)

Add 6 knots to Vref. Landing Distance Factor .................................................. (1.52)Flaps 15 (1.55)Flaps 35 General Landing Distance ....................... (Flaps 15) 3463 Dry/4466 Wet (Flaps 35) 3142 Dry/4085 Wet Outboard Roll Spoiler Malfunction checklist............................. Complete

INBOARD OR OUTBOARD GROUND SPOILER MALFUNCTION ROLL SPLR INBD GND or ROLL SPLR OUTBD GND Affected roll spoilers may not extend at touchdown. 1) Landing Distance Factor .................................................. (1.17)Flaps 15 (1.19)Flaps 35 2) General Landing Distance ....................... (Flaps 15) 2645 Dry/3438 Wet (Flaps 35) 2690 Dry/3136 Wet 3) Inboard or Outboard Ground Spoiler Malfunction checklist ..... Complete


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49

RUDDER CONTROL MALFUNCTION RUD 1 or RUD 2 PUSH OFF Illuminated 1) 2) 3)

Illuminated switch light .............................................................. Push Off. Observe RUD FULL PRESS and RUD PRESS caution lights come on. Airspeed ................................................................... 200 KIAS maximum

Avoid abrupt or excessive rudder movements above 150 KIAS. 4)

Rudder Control Malfunction checklist .......................................Complete

#1 OR #2 RUDDER HYDRAULIC MALFUNCTION #1 RUD HYD or #2 RUD HYD 1)

Associated RUD 1 or RUD 2 PUSH OFF switch light............................................................. Push Off

Switch Light will not be illuminated 2) 3)

Observe RUD FULL PRESS and RUD PRESS caution lights come on. Airspeed ................................................................... 200 KIAS maximum


#1 or #2 Rudder Hydraulic Malfunction checklist......................Complete

RUDDER PRESSURE MALFUNCTION RUD PRESS and/or RUD FULL PRESS 1)

Airspeed ................................................................... 200 KIAS maximum


Rudder Pressure Malfunction checklist.....................................Complete

50


05/29/15

RUDDER JAM (RESTRICTED RUDDER PEDAL MOVEMENT)

Should the rudder pedal (rudder jam) suddenly break free, do not apply rudder pedal input in the opposite direction 1)

Affected Rudder Pedal ............ Apply a normal push force in the desired direction

►

If rudder pedal moves as required:

2)

Affected rudder pedal .......Reduce push force and allow rudder pedal to center Rudder pedals ................................................................ Use as required Rudder Jam checklist ............................................................... Complete

3) 4) ►

If rudder pedal does not respond to normal push force (rudder remains jammed or rudder jam reoccurs):

2) 3)

Directional Control........................................ Use roll control as required Minimum Airspeed ................................................................... 125 knots

Landing: 4) 5) 6)

Nosewheel Steering ............................................................................ Off Approach Speed ............................................... Vref (for Flaps 15 or 35) Land at an airport with minimal crosswind and turbulence.

If the rudder jam occurs on takeoff and conditions permit, return for a landing on the takeoff runway. Small amounts of asymmetric power may be used to maintain directional control on approach and after landing. Use asymmetric braking and power, as required, to maintain directional control after touchdown. 7) 8) 9)

Landing Distance Factor .................................................. (1.36)Flaps 15 (1.31)Flaps 35 General Landing Distance....................... (Flaps 15) 3074 Dry/3996 Wet (Flaps 35) 2656 Dry/3452 Wet Power .............................................. Maintain as required for touchdown

After the aircraft has come to a stop: 10) Nosewheel Steering ............................................................................ On 11) Directional Control Malfunction checklist ................................. Complete


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51

RUDDER TRIM ACTUATOR RUNAWAY 1)

Apply opposite rudder and attempt to reverse trim and stop movement at the neutral position by pulling the RUD TRIM ACT circuit breaker (F7 on left essential circuit breaker panel)

If the rudder trim actuator cannot be reversed: 2) RUD TRIM ACT circuit breaker .......................................................... Pull 3) Rudder Trim Actuator Runaway checklist .................................Complete

AILERON TRIM TAB RUNAWAY 1) 2)

Reduce Airspeed Attempt to reverse trim and stop movement at neutral position by pulling AIL TRIM ACT circuit breaker. (J7 on left essential circuit breaker panel)

If the aileron trim actuator cannot be reversed: 3) AIL TRIM ACT circuit breaker ............................................................ Pull 4) Aileron Trim Tab Runaway checklist.........................................Complete

MANUAL ELEVATOR TRIM FAILURE 1) 2)

STBY Elevator Trim switch .................................. Raise guard and ARM Operate Standby Elevator Trim as required.

Elevator Trim Indicator will not indicate trim tab position. The standby elevator trim rate is slow. 3)

Manual Elevator Trim Failure checklist .....................................Complete

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05/29/15

ELEVATOR CONTROL MALFUNCTION Use of Standby Elevator Trim If control of the elevators and the manual trim is lost in flight, the standby elevator trim system may be used to maintain pitch control. 1) 2)

STBY ELEVATOR TRIM Switch ................Raise guard and select ARM Nose Down/Nose Up............................................................. As required

Standby elevator trim rate is low, which requires that the effect of a change in trim setting be monitored before a subsequent trim change is made.

Elevator Trim Indicator will not indicate trim tab position. Crew Coordination • One pilot should control power with the inboard hand, and pitch using one of the STBY ELEVATOR TRIM switches. • The other pilot should assume rudder and roll control (maximum bank angle 15°). • Minimize power changes. • If possible, move passengers to shift the C.G. aft. Landing Considerations • Land at an airport with minimal crosswind and turbulence under VMC conditions. • Land with Flap 15 maximum • Stabilize aircraft on approach and in landing configuration Flap 15, prior to passing 1000 ft AGL. • No configuration change may be made after the approach has been commenced.

Power changes during the approach should be limited to small amounts and the aircraft should be trimmed before a subsequent power change is made. Do not flare or reduce power to Flight Idle prior to touchdown. Approach and Landing 3) Select Flaps 5° and Trim (no less than Vref (Flaps 0)) 4) Select Flaps 15° and Trim (no less than Vref + 10) 5) Minimum speed to touchdown = Vref + 10 6) Power levers............................................... Flight Idle only at touchdown 7) Landing Distance Factor .................................................. (1.28)Flaps 15 8) General Landing Distance........................................ 2893 Dry/3761 Wet 9) Elevator Control Malfunction checklist ..................................... Complete


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53

ABNORMAL FLAP LANDING If flaps have failed between 0 and 15: 1) GPWS flap override switch ............................................................. Press

Nosewheel should be promptly brought into contact with the ground following main wheel contact. 2) 3) 4) 5) 6)

Approach speed and V REF = VREF (Flaps 0) V2 for Flaps 0 is _______ Power should be reduced gradually to Flight Idle at or just prior to touchdown. Max pitch at touchdown ........................................................................8° Use max discing. Use reverse as required

If Reverse Power is required, ensure that Engine Torque does not exceed 90%. 7) 8)

Landing Distance Factor (use Flaps 35 landing data) ........ (2.55)Flaps 0 General Landing Distance ........................................ 5169 Dry/6720 Wet

If flaps have failed between 15 and 35: 1) Approach speed and V REF = VREF (Flaps 15 or Flaps 35)

The smaller flap angle must be used when calculating landing performance. 2)

Use appropriate Unfactored Landing Distance chart on Page 83 or 84 to determine landing distance.

After landing: 1) GPWS flap override switch ....................................................... Press Off 2) Abnormal Flap Landing checklist ..............................................Complete

FLAP DRIVE MALFUNCTION FLAP DRIVE The secondary cable is under load. Flaps will continue to operate and may be used to complete the flight. 1)

Flap Drive Malfunction checklist ...............................................Complete

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05/29/15

FLAP POWER MALFUNCTION FLAP POWER 1)

#1 Hydraulic quantity and pressure............................................... Check

►

If pressure is low and quantity is normal:

2) 3)

#1 STBY pump ................................................................................... On Flaps ............................................................................ Operate normally

Operation of the flaps with the #1 Standby Pump may cause sporadic illumination of the FLAP POWER caution light. 4)

Flap Power Malfunction checklist ............................................. Complete

►

If pressure is low and quantity is depleted:

With complete loss of hydraulic fluid, flap will remain in selected position. 2) 3)

Proceed with the #1 HYDRAULIC SYSTEM FAILURE checklist on Page 32. Flap Power Malfunction checklist ............................................. Complete


05/29/15

55

LOW FUEL PRESSURE #1 ENG FUEL PRESS or #2 ENG FUEL PRESS 1) 2)

Appropriate AUX PUMP ...................................................................... On Check AUX PUMP advisory light on, and ENG FUEL PRESS caution light out.

If caution light does not go out: 3) Appropriate AUX PUMP ...................................................................... Off 4) Check for external leaks and for fuel odor within airplane. If either is confirmed, shut down the engine. 5) Low Fuel Pressure checklist .....................................................Complete

LOW FUEL LEVEL #1 TANK FUEL LOW or #2 TANK FUEL LOW 1)

Contents of affected tank ............................................................... Check

►

If fuel is low:

2)

Check for external and internal fuel leaks.

A check of the cabin will be necessary to identify a possible internal fuel leak. No indication of a fuel leak: 3) Transfer fuel from unaffected tank. 4) Monitor fuel quantity. Fuel leak confirmed: 5) Shut down engine on affected side. 6) Low Fuel Level checklist ...........................................................Complete ►

If affected tank fuel content is normal:

2) 3) 4)

Maintain a level attitude as much as possible. Appropriate AUX PUMP ...................................................................... On Monitor fuel quantity.

If associated ENG FUEL PRESS caution light illuminates: 5)

6)

Shut down engine on affected side. Low Fuel Level checklist ...........................................................Complete

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05/29/15

FUEL FILTER IMPENDING BYPASS WARNING #1 FUEL FLTR BYPASS or #2 FUEL FLTR BYPASS 1)

Affected engine performance .......................................................Monitor

Monitor fuel flow, ITT, and N H. If erratic, this indicates contamination has passed filter. Consider engine shutdown. 2)

Fuel Filter Impending Bypass Warning checklist ..................... Complete

FUEL TRANSFER FAILURE ►

1) On 2) 3)

If AUX PUMP does not come on automatically: Delivering AUX PUMP ......................................................................... On completion of fuel transfer: Delivering AUX PUMP ......................................................................... Off Fuel Transfer Failure checklist ................................................. Complete

►

If one or both Transfer Valves fail to open:

1) 2)

Transfer switch .................................................................................... Off Consideration should be given to the effects of fuel maximum lateral asymmetry or low fuel level.

Fuel maximum lateral asymmetry is 600 lbs. 3)

Fuel Transfer Failure checklist ................................................. Complete

ABNORMAL FUEL TEMPERATURE 1) 2) 3)

Appropriate AUX PUMP ...................................................................... On Continue flight, but maintain level attitude as much as possible. Monitor fuel temperature and fuel pressure.

If fuel temperature returns to normal: 4) Appropriate AUX PUMP ...................................................................... Off 5) Abnormal Fuel Temperature checklist...................................... Complete


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57

RAPID DEPRESSURIZATION 1) Flight Crew ................................................... Suit-up and Communicate On aircraft 914 thru 975, 837 & 838, with MASK selected, PA transmissions can be made with the captain’s side only using the interphone system. 2) Cabin Signs ....................................................................................... On 3) Emergency Lights.............................................................................. On 4) Rapid Depressurization checklist ........................................... Complete

EMERGENCY DESCENT The following procedure assumes structural integrity of the aircraft. If structural failure or damage is a possibility, limit speed as much as possible and avoid high maneuvering loads. 1) Power Levers.......................................................................... Flight Idle 2) Condition Levers ............................................................................. Max 3) Speed ............................................................................................. Vmo If an immediate descent to an altitude where oxygen is not required cannot be conducted; within 5 minutes of donning oxygen masks: ►

4) Oxygen Mask Control Knob .............................................................. NORM 5) Emergency Descent checklist ....................................................... Complete

CABIN PRESSURIZATION FAILURE CABIN PRESS or FAULT light illuminated on pressure control panel 1) 2) 3) 4) 5)

Cabin Altitude Indicator ..................................................................... Check Bleed Air 1 and 2.............................................................................On/Max Auto/Man/Dump Switch ....................................................................... Auto Manual Knob .......................................................... Fully counter-clockwise Forward Outflow Valve....................................................................... Norm

►

If control of pressurization is regained: Cabin Pressurization Failure checklist ......................................... Complete

6) ►

6) 7)

If control of pressurization is NOT regained: Auto/Man/Dump Switch ....................................................................... Man Manual Knob ..................................... As required (5.5 psi differential max)

Use cabin altitude differential placard to achieve appropriate cabin altitude in climb, cruise, or descent. Continued on next page

58


05/29/15

CABIN PRESSURIZATION FAILURE (Continued) (Continued) ►

If control of pressurization pressurization is regained:

Prior to landing: 8) Bleed Air 1 and 2..................................... .................................................................. ............................. Min/Off 9) Cabin Pressurization Pressurization Failure checklist ............................. Complete ►

If control of pressurization pressurization is NOT regained: 8) Descend to below 14,000 ft as soon as possible. 9) Proceed with the Unpressurized Unpressurized Flight checklist Flight checklist on Page 61. 61. 10) Cabin Pressurization Pressurization Failure Failure checklist checklist ............................. Complete


05/29/15

59

BLEED HOT #1 BLEED BLEED HOT or #2 BLEED BLEED HOT HOT If caution light continues to cycle on and off: 1) Affected Bleed Switch .................................... ......................................................................... ..................................... Off 2) Bleed Hot checklist.................................................................. .................................................................... ..Complete Complete

AIR CONDITIONING PACK HOT AIR COND PACK HOT If caution light continues to cycle on and off: 1) Both Bleeds ..................................... ............................................................................. .................................................... ............ Off

With Bleed 1 and Bleed 2 selected Off, de-ice pressure may be insufficient at low power power settings. Avoid icing conditions conditions if possible. possible. 2)

Descend below 14,000 ft as soon as possible. possible .

When cabin pressure differential has decreased to 0.5 psi or below, proceed with the RAM AIR VENTILATION checklist on Page 61. 61. 3) Air Conditioning Pack Hot checklist ....................................... .......................................... ...Complete Complete

CABIN OR FLIGHT COMPARTMENT DUCT HOT CABIN CABIN DUCT DUCT HOT or FLT COMPT COMPT DUCT DUCT HOT 1) 2)

Cabin or Flight Flight Comp Comp Auto/Man switch............................................. ............................................. Man Cabin or Flight Flight Comp Comp Cool/Warm switch ........................................ .......................................... ..Cool (Hold for 10 Seconds)

If caution light remains illuminated: illuminated: 3) Both Bleeds ..................................... .............................................................................. .................................................... ........... Off

With Bleed 1 and Bleed 2 selected Off, de-ice pressure may be insufficient at low power power settings. Avoid icing conditions conditions if possible. possible. 4)

Descend below 14,000 ft as soon as possible. possible .

When cabin pressure differential has decreased to 0.5 psi or below, proceed with the RAM AIR VENTILATION checklist on Page 61. 61. 5) Cabin or or Flight Compartment Compartment Duct Hot checklist checklist ......................Complete

60


05/29/15

UNPRESSURIZED UNPRESSURIZED FLIGHT 1) 2) 3)

Auto/Man/Dump Auto/Man/Dump switch .................................. .................................................................. ................................ Dump Bleeds.................................. ....................................................................... ................................................................ ........................... On Oxygen ...................................... .............................................................................. ........................................... ... As Required

For flight with bleed-air supply selected off, proceed with the RAM AIR VENTILATION checklist on this page. 4)

Unpressurized Unpressurized Flight checklist....................................... .................................................. ........... Complete Complete

RAM AIR VENTILATION 1) 2)

RECIRC Fan................................... ......................................................................... ..................................................... ............... Off Both Bleeds ................................... ........................................................................... ...................................................... .............. Off

With Bleed 1 and Bleed 2 selected Off, de-ice pressure may be insufficient at low power power settings. Avoid icing conditions conditions if possible. 3) 4) 5)

Auto/Man/Dump Auto/Man/Dump switch ................................................................... ..................................................................... .. Man Manual Control Knob.............................. Fully Clockwise(towards Clockwise(towards INCR) Fwd Outflow Valve..................................................................... ........................................................................... ...... Open

Ram ventilation is most effective at speeds above 150 KIAS. 6)

Ram Air Ventilation checklist .................................................... .................................................... Complete Complete

ALTERNATE PRESSURIZATION MODES Cab Set Mode: 1) Auto/Man/Dump Auto/Man/Dump switch .................................. .................................................................... .................................. Auto 2) Cab Set/Norm switch ...................................... ................................................................... .............................Cab Cab Set 3) Altitude Knob ...................................... Set enroute Cabin Altitude as per Cabin Altitude/Differential Placard 4) Rate Knob................................... ........................................................................ .......................................... ..... As Required Required At commencement commencement of descent: 5) Altitude Knob ........................................... ................................................... ........ Set Destination Elevation 6) Barometer Knob ....................................... ......................................................... .................. Set to Local Value 7) Rate Knob................................... ........................................................................ .......................................... ..... As Required Required 8) Alternate Pressurization Pressurization Modes checklist................................. checklist................................. Complete Manual Mode: 1) Manual Knob ....................................... Increase to avoid pressure bump 2) Auto/Man/Dump Auto/Man/Dump switch ................................................................... ..................................................................... .. Man 3) Manual Knob ..................................Adjust enroute Cabin Altitude as per per Cabin Altitude/Differential Placard

Do not exceed differential pressure of 5.5 PSI 4)

Alternate Pressurization Pressurization Modes checklist................................. checklist................................. Complete


05/29/15

61

AIRFRAME DEICING SYSTEM AIR SUPPLY FAILURE DE-ICE PRESS 1) 2) 3) 4) 5)

Airframe Auto Selector........................................................................ Off Boot Air switch ................................................................................... ISO De-ice Press Indicator .......................................... Check for Pressure in Left or Right System Engine Intake Bypass Doors .......................................................... Open Ignition switches........................................................................... Manual

Do not select the outer two wing positions (1 & 2) during manual deicing of the tail and engine intake. The engine intake boot on the side with normal pressure can be de-iced as follows: • To de-ice the left side, select positions 6,5,4 • To de-ice the right side, select positions 6,5,3

The dwell time at each Tail and Engine intake position should be 6 seconds. The engine intake boot on the side with normal pressure can be deiced. 6)

Exit Icing Conditions if Possible.

For Holding, Approach, and Landing phases: 7) Hold at 160 KIAS minimum. 8) For Approach and Landing, use flaps 15° maximum, at a speed of Vref + 15 kts. 9) Add 15 kts to all go-around speeds. 10) Landing Distance Factor ................................................... (1.66)Flaps 15 11) General Landing Distance ........................................ 3752 Dry/4878 Wet 12) Airframe Deicing System Air Supply Failure checklist ..............Complete

62


05/29/15

ELEVATOR HORN HEAT FAILURE L ELEV HORN HEAT or R ELEV HORN HEAT 1)

Exit or avoid Icing Conditions if possible.

If Icing Conditions cannot be avoided: 2) Flaps ..................................................................................................... 0° 3) Minimum Airspeed.................................................................... 173 KIAS For Holding, Approach, and Landing Phases in Icing Conditions: 4) 5) 6) 7) 8) 9)

Hold at 173 KIAS minimum. Use flaps 15° maximum, at a speed of Vref + 15 Add 15 kts to all go-around speeds. Landing Distance Factor .................................................. (1.66)Flaps 15 General Landing Distance ........................................ 3752 Dry/4878 Wet Elevator Horn Heat Failure checklist ........................................ Complete

AIRFRAME BOOT FAILURE If affected deice boot advisory light is illuminated continuously, comply with steps 2 through 6 below. If affected advisory light does not illuminate during boot cycle: 1) Test Advisory Lights If the affected deice boot advisory light illuminates: 2) Exit Icing Conditions if possible. For Holding, Approach, and Landing Phases: 3) 4) 5) 6) 7) 8)

Hold at 160 KIAS minimum. For Approach and Landing, use flaps 15° maximum, at a speed of Vref + 15 kts. Add 15 kts to all go-around speeds. Landing Distance Factor .................................................. (1.66)Flaps 15 General Landing Distance ........................................ 3752 Dry/4878 Wet Airframe Boot Failure checklist................................................. Complete

PROPELLER DEICING SYSTEM FAILURE If Propeller Advisory Lights fail to illuminate in sequence: 1) Test Advisory Lights If all Propeller Advisory Lights illuminate: 2) Prop timer selector ............................................ Select alternate position 3) Check illumination of Propeller Advisory Lights. If fault is not corrected: 4) Propellers ...................................................... Operate at up to 1200 rpm 5) Exit Icing Conditions if possible. 6) Propeller Deicing System Failure checklist .............................. Complete


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63

ENGINE INTAKE BOOT FAILURE For the remainder of the flight: 1) Engine Intake Bypass Door ............................................................ Open 2) Ignition.......................................................................................... Manual 3) Exit Icing Conditions if possible. 4) Engine Intake Boot Failure checklist .........................................Complete

WINDSHIELD OVERHEAT L WSHLD HOT or R WSHLD HOT 1) 2) 3)

Windshield Heat switch .................................................. Select Warm-up Exit or Avoid Icing Conditions if possible. Windshield Overheat checklist ..................................................Complete

SIDE WINDSHIELD OVERHEAT SIDE WDO HOT 1) 2)

PLT WDO/HT switch ........................................................................... Off Side Windshield Overheat checklist..........................................Complete

PITOT HEAT FAILURE #1 PITOT HEAT or #2 PITOT HEAT 1)

Appropriate pitot heat switch..................................................... Check on

If switch is on: 2) When in icing conditions or precipitation, rely on the flight instruments on the opposite side. 3) Pitot Heat Failure checklist .......................................................Complete

64


05/29/15

APU FIRE 1) 2) 3) 4) 5) 6) 7) 8) 9) 10)

Parking Brake ................................................................................. Set Power Levers ........................................................................ Flight Idle Condition Levers...................................................................... Fuel Off APU Power Switch........................................................................... Off APU Extinguishing Switch ................................................... Extinguish ATC/Cabin ................................................................................... Notify DC External Power .......................................................................... Off Battery Master Switch ...................................................................... Off Evacuate ........................................................................... As Required APU Fire checklist ................................................................ Complete

APU STARTER CONTACTOR FAILURE APU RUN + APU STARTER 1) 2) 3) 4) 5) 6) 7)

APU Generator switch ......................................................................... Off Main Battery Switch ............................................................................. Off DC External Power switch ................................................................... Off #1 and #2 DC Generator switches ...................................................... Off #1 and #2 AC Generator switches ...................................................... Off APU Power switch ............................................................................... Off APU Starter Contactor Failure checklist................................... Complete

APU GENERATOR OVERHEAT APU GEN OHT For Model 8099 APU (Aircraft 914-975HA): 1) APU Generator switch ......................................................................... Off If Overheat light extinguishes: 2) APU Generator switch ......................................................................... On 3) APU Generator Overheat checklist .......................................... Complete For 1) 2) 3)

Model 8155 APU (Aircraft 837-839EX and 804-816EX): Automatic APU Shutdown will occur. APU Power Switch .............................................................................. Off APU Generator Overheat checklist .......................................... Complete

APU REARBAY OVERHEAT APU + APU RBY OHT For Model 8099 APU (Aircraft 914-975HA): 1) APU Power switch ............................................................................... Off 2) APU Rearbay Overheat checklist ............................................. Complete For 1) 2) 3)

Model 8155 APU (Aircraft 837-839EX and 804-816EX): Automatic APU Shutdown will occur. APU Power Switch .............................................................................. Off APU Rearbay Overheat checklist ............................................. Complete


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65

APU BLEED AIR OVERHEAT FLT COMP DUCT HOT or CABIN DUCT HOT or AIR COND PACK HOT 1)

APU Bleed Air switch .......................................................................... Off 2) APU Bleed Air Overheat checklist ............................................Complete

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PASSENGER OR BAG DOOR WARNING PASS DOOR or BAG DOOR If on the ground: 1) Inspect and secure the affected door. If in flight:

Do not attempt to secure the door 1) 2) 3) 4)

Turn on FASTEN SEAT BELT and NO SMOKING signs. Land as soon as possible. Use the UNPRESSURIZED FLIGHT checklist on Page 61. Passenger or Bag Door Warning checklist .............................. Complete

CRACKED WINDSHIELD If in 1) 2) 3) 4)

pressurized flight: Airspeed .................................................................. Reduce to 180 KIAS Cabin differential pressure .................................. Reduce to 2.5 - 3.0 psi Descend to below 14,000 ft as soon as practicable. Cracked Windshield checklist................................................... Complete

LEFT OR RIGHT STALL WARNING FAILURE L STALL WARNING or R STALL WARNING 1)

Stall Warn heat switch .............................................................. Check on

If switch is on: 2) Maintain at or above minimum operational airspeeds.

With Left or Right Stall Warning Caution Light illuminated, spurious stall warning indications may occur in flight in icing conditions which are inconsistent with airspeed and flight conditions. 3)

Left or Right Stall Warning Failure checklist ............................ Complete

ABNORMAL INDICATIONS OF AIRSPEED, ALTITUDE, AND VERTICAL SPEED 1)

Appropriate static source selector .................................. Select Alternate

If switching the STATIC SOURCE selector to ALTERNATE does not correct the abnormal indications: 2) 3) 4)

Rely on the flight instruments on the opposite side. Land as soon as practicable. Abnormal Indications of Airspeed, Altitude, and Vertical Speed checklist .................................................................................... Complete


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67

AUTOPILOT AFCS MALFUNCTIONS Auto-pilot (AFCS) Malfunctions For most AFCS malfunctions, an automatic transfer to the other system will occur, and an appropriate failure message will appear on the ID-802 panel. If transfer cannot be accomplished, the autopilot will passively disengage, the A/P DISENG annunciators will illuminate and flash and the flying pilot must resume manual control.

HSI Transfer The following advisory display messages require HSI transfer to be selected on the AFCS controller, and the reselection of desired flight director modes: FD DADC DATA INVLD FD NAV DATA INVLD

KNS MESSAGES 1)

KNS 660 MSG key .......................................................................... Press

If no action required: 2) KNS 660 MSG key ............................ Press and return to previous page

-

-

3)

If crew action is required to maintain valid navigation guidance, perform the necessary action. Monitor the accuracy of position and navigation data. If the message indicates a system failure, invalid sensor, invalid navigation operation, or the entering of DR-mode, de-select the KNS 660 and utilize remaining navigation equipment.

KNS Messages checklist ..........................................................Complete

FLIGHT DATA RECORDER FAILURE FLT DATA RECORDER 1)

Anti-Collision Light ...........................................................RED or WHITE

Illumination of the Flight Data Recorder caution light requires a maintenance action prior to the next flight. 2)

Flight Data Recorder Failure checklist......................................Complete

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TCAS FAILURE TCAS FAIL Annunciation on VSI/TRA ►

If Transponder Fail Light is Illuminated:

1)

2)

Select MODE S ON or STBY on TCAS/Mode S Control Panel. If unrecoverable, select alternate transponder (for single Mode S installations TCAS will no longer be operable; for dual Mode S installations TCAS should function normally). TCAS Failure checklist ............................................................. Complete

►

If RAD ALT or DADC are no longer available:

1) 2)

Select MODE S ON. TCAS is no longer available. TCAS Failure checklist ............................................................. Complete

►

If RA FAIL or TCAS FAIL is annunciated on one side, or a total failure of one side occurs, the opposite side display may be used.

1)

TCAS Failure checklist ............................................................. Complete

With the TA DSPLY control switch set to OFF, when the TCAS aural advisory of TRAFFIC occurs, an intruder aircraft is within 40 seconds of closest approach to your aircraft.

SAHS FAILURE ATT FAIL advisory light SAHS attitude gyro has failed. CMPS WARN advisory light SAHS directional gyro has failed. SAHS Failure checklist ..................................................................... Complete


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AHRS FAILURES Primary Heading Data Failure Indications: HDG flag appears on affected HSI Off flag appears on opposite side RMI SLAVE advisory light on AHRS controller illuminates

  

If Standby Attitude/Heading System (SAHS) is installed: SAHS control panel ...................................... Press GYRO 1 or GYRO 2 Check that the failure indications cancel. Check that displayed data is consistent with the opposite side.

►

1) 2) 3)

-

Compass synchronization information for the affected HSI is now displayed on the SAHS unit. With both AHRS failed the Flight Director/Autopilot will be inoperative.

4) 5)

Disengage the autopilot. AHRS Failure checklist .............................................................Complete

►

If Standby Attitude/Heading System (SAHS) is not installed:

1) 2)

Affected AHRS controller HDG/DG switch ..................................... Press Ensure DG advisory light illuminates, SLAVE advisory light remains illuminated and HDG and OFF flags disappear.

At intervals not greater than 5 minutes: 3) Using DG slew knob, select or + to align the HSI heading with either the RMI heading or magnetic compass heading, as appropriate. 

When operating in DG mode, the HSI heading must be aligned with the RMI heading at anytime the HSI HDG MISMATCH message is presented on the advisory display. 4)

AHRS Failure checklist .............................................................Complete

Attitude Failure Indications: ATT flag appears on ADI BASIC illuminates on AHRS controller ID-802 panel may display ADI ROLL MISMATCH or PITCH MISMATCH   

If Standby Attitude/Heading System (SAHS) is installed: 1) SAHS control panel ........................................ Press GYRO 1 or GYRO 2 2) Check that the failure indications cancel. 3) Check that displayed data is consistent with the opposite side.

With both AHRS failed the Flight Director/Autopilot will be inoperative. 4) Disengage the autopilot. 5) AHRS Failure checklist...............................................................Complete

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AHRS PRIMARY POWER SOURCE FAILURE AUXPR advisory on AHRS Controller No crew action is required. 1)

AHRS Primary Power Source Failure checklist ....................... Complete

UNS MALFUNCTION ►

If the UNS CDU and glareshield message (MSG) annunicators illuminate:

1) 2)

5)

Press MSG on UNS CDU to display message page. Refer to the UNS-1B/UNS-1C (as appropriate) Operators Manual Section IX Messages for appropriate messages. Pilot’s actions where applicable must be accomplished in response to annunciated messages. Some of the messages in Section IX describe malfunctions or degradation of Flight Management System capability. IFR FMS operations must be discontinued upon display of such messages. UNS Malfunction checklist ....................................................... Complete

►

If the GPS INTEG annunciator illuminates:

1)

3)

If on an IFR approach, terminate the GPS based approach and execute a missed approach as required. If in the enroute or terminal environment, continue to navigate using the UNS or revert to an alternate means of navigation. When continuing to use GPS navigation, position must be verified every 15 minutes using other approved navigation systems. UNS Malfunction checklist ....................................................... Complete

►

If there is a loss of FMS Remote Status Annunciation:

1) 2)

Discontinue IFR GPS operations. UNS Malfunction checklist ....................................................... Complete

3) 4)

2)


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71

EMERGENCY OPENING OF FLIGHT DECK DOOR If the flight deck door is jammed: 1) 2) 3) 4)

Unlock the deadbolt. Open upper release mechanism. Open release handle mechanism. While still holding onto the release handle, push door AFT to clear threshold. Place door against adjacent lavatory wall. Exit flight deck.

Do not block aircraft emergency exits

72


05/29/15

INCAPACITATED FLIGHT ATTENDANT The Flight Crew should establish communications with the cabin (initially by selecting Cabin PA) and solicit the help of an able-bodied person (ABP). Have the ABP accomplish the following:    

Assess the condition of the flight attendant Ask passengers for medical assistance Inform the PIC of the situation Secure the cabin for landing

The ABP will secure the cabin by accomplishing the following:      



Ensure all passengers are seated with seatbelts fastened Secure beverage cart in galley Collect and dispose of all trash Secure all galley latches and equipment If possible, ensure flight attendant is restrained The incapacitated flight attendant must be secured in a nonemergency exit seat The ABP must be seated in the flight attendant jumpseat for landing and taxi

The Flight Crew will make the following required PA announcements:    

All passengers are seated with seatbelts fastened All electronic devices are off All tray tables are up and locked All personal items brought on board are stowed in the overhead bins or under the seat in front of the passenger

Notify ATC of intentions and SBY FDC if time allows. After engine shutdown, the SIC will enter the cabin, open the boarding door and ensure all passengers remain seated until the appropriate medical personnel have arrived to assist the flight attendant.


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FORCED LANDING WITH BOTH ENGINES OPERATING 1) Cabin ..............................................................................................Secure If possible ensure no passengers are seated in the plane of the propellers. 2) EGPWS ANNUC CB (B3) & EGPWS COMP CB (A3, H3, J3, or M3 on Left Main DC) ...................................................................................... Pull 3) Emergency lights .................................................................................. On 4) Auto/Man/Dump Switch ................................................................... Dump 5) ELT ....................................................................................................... On 6) Shoulder harness .............................................................................. Lock IF planning landing with landing gear EXTENDED: When airplane comes to a stop: 7) Emergency brake ................................................................................. On 8) Condition levers............................................................................ Fuel Off 9) Pull Fuel Off Handles........................................................................... Pull 10) Battery Master ...................................................................................... Off 11) Evacuate 12) Forced Landing with Both Engines Inoperative Checklist .......... Complete IF planning landing with landing gear RETRACTED: 7) Landing gear horn CB (E5 –Left Main DC) ......................................... Pull 8) Flap ........................................................................................................ 35   

Maintain VREF until immediately prior to flare. DO NOT exceed 5° nose up during flare. Touch down with minimum speed and minimum rate of descent without stalling.

After ground contact: 9) Condition levers............................................................................ Fuel Off 10) Pull Fuel Off Handles........................................................................... Pull 11) Battery Master ...................................................................................... Off After airplane comes to stop: 12) Evacuate 13) Forced Landing with Both Engines Inoperative Checklist .......... Complete

74


05/29/15

FORCED LANDING WITH BOTH ENGINES INOPERATIVE After all attempts to achieve a successful airstart have failed proceed as follows: 1) Flaps ................................................................................... 0° (if possible) 2) Airspeed ........................................................... Vref speed for flap setting

With 0° flap, propellers feathered and landing gear retracted, under zero wind conditions, 2.5 nautical miles can be traveled for every 1000 feet of altitude lost. This distance will increase in a tailwind and decrease in a headwind. 3) Cabin.............................................................................................. Secure 4) MAIN and AUX BATT switches ............................................................ Off 5) BATTERY MASTER switch .................................................................. On The following services will be inoperative: Hydraulic:      

Flaps Roll Spoilers Rudder Anti-skid Landing Gear Nose Wheel Steering

Electric:  

All Variable Frequency AC Services All Non-essential DC Services (see BATTERY ESSENTIAL SERVICES checklist Page 30)

Pneumatic:  

6) 7) 8) 9) 10)

Airframe De-icing Pressurization

EGPWS........................................................................ TERRAIN INHIBIT Cabin signs ........................................................................................... On Emergency lights .................................................................................. On ELT ....................................................................................................... On Shoulder harness ........................................................................... Locked

Make the approach and landing into the wind. Extending the gear will steepen glide angle and decrease horizontal glide distance. Allow sufficient time for gear to extend. IF planning landing with landing gear EXTENDED: If the available surface is appropriate extend landing gear allowing sufficient time for alternate gear extension. 

Maintain VREF for appropriate flap setting until immediately prior to flare. Continued on next page


05/29/15

75

FORCED LANDING WITH BOTH ENGINES INOPERATIVE (Continued) (Continued) 



Commence flare to achieve zero vertical velocity immediately prior to ground contact. Touchdown with minimum speed and minimum rate of descent without stalling.

11) Landing gear............................................. Extend (checklist on Page 38.) Prior to touchdown: 12) Battery Master ...................................................................................... Off After touchdown: 13) Emergency brake ....................................................... Apply Intermittently When aircraft comes to a stop: 14) Evacuate 15) Forced Landing with Both Engines Inoperative checklist ...........Complete

IF planning landing with landing gear RETRACTED: 



 

Maintain VREF for appropriate flap setting until immediately prior to flare. Commence flare to achieve zero vertical velocity immediately prior to ground contact. DO NOT exceed 6° nose up during flare. Touchdown with minimum speed and minimum rate of descent without stalling.

Prior to touchdown: 10) Battery Master ...................................................................................... Off When aircraft comes to a stop: 11) Evacuate 12) Forced Landing with Both Engines Inoperative checklist ...........Complete

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05/29/15

EMERGENCY LANDING PROCEDURES When it is known that a landing must be performed which could be identified as an emergency landing due to the presence of factors which introduce a hazard to the airplane and its occupants, the following points should be addressed as applicable: • • • • • • • •

• • • •

Instruct flight attendant to brief and prepare passengers as appropriate to the emergency. If possible, ensure that no passengers are seated in the rotational plane of the propellers. Secure all loose items in the flight compartment and cabin. Complete all necessary radio communications concerning the intended landing with ground support personnel. Review the procedures to be followed, covering all aspects of crew actions and coordination. Consider the suitability of a practice approach. Ensure that both pilots’ shoulder harnesses are secure and locked. Deactivate the GPWS by pulling EGPWS ANNUC circuit breaker B3 and EGPWS COMP (A3, H3, J3 or M3) on the left main circuit breaker panel. Cabin altitude Auto/Man/Dump switch........................................ Dump Emergency light switch .................................................................... On Battery Master switch ...................................................................... Off Emergency Landing Procedures checklist ........................... Complete


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77

AIRCRAFT DITCHING IF both engines are OPERATIVE: 1)

Accomplish FORCED LANDING WITH BOTH ENGINES OPERATING checklist on Page 73.

Landing Considerations 

  

 



In rolling swell surface conditions attempt to ditch along and parallel to the crests as much into wind as swell line permits. In other water surface conditions land into wind. Maintain VREF until immediately prior to flare. Set rate of descent to 200 to 300 FPM. Commence flare to achieve zero vertical velocity immediately prior to water contact. Maintain pitch attitude of 10° nose up. Touchdown with minimum speed and minimum rate of descent without stalling. A transient nose-up pitching motion may result following touchdown. Overcorrection of this tendency could result in porpoising or nosing in.

After water contact: 2) 3) 4)

Condition levers .......................................................................... Fuel Off Pull Fuel Off Handles ......................................................................... Pull Battery Master..................................................................................... Off

When airplane comes to a stop: 5)

Evacuate

Do not open the front door on the lower side.

The airplane will float with one wing in the water. The exits on the high side of the cabin should be used for evacuation. 6)

Aircraft Ditching checklist..........................................................Complete

IF both engines are INOPERATIVE: 1)

Accomplish FORCED LANDING WITH BOTH ENGINES INOPERATIVE checklist on Page 75.

Landing Considerations  



DO NOT select landing gear down. In rolling swell surface conditions attempt to ditch along and parallel to the crests as much into wind as swell line permits. In other water surface conditions land into wind. Maintain VREF until immediately prior to flare. Continued on next page

78


05/29/15

AIRCRAFT DITCHING (Continued) (Continued) 

 



Commence flare to achieve zero vertical velocity immediately prior to water contact. Maintain pitch attitude of 10° nose up. Touchdown with minimum speed and minimum rate of descent without stalling. A transient nose-up pitching motion may result following touchdown. Overcorrection of this tendency could result in porpoising or nosing in.

After water contact: 2)

Battery Master ..................................................................................... Off

When airplane comes to a stop: 3)

Evacuate

Do not open the front door on the lower side.

The airplane will float with one wing in the water. The exits on the high side of the cabin should be used for evacuation

4)

Aircraft Ditching checklist ......................................................... Complete


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79

OBSERVER’S JUMPSEAT BRIEFING CARD Welcome Aboard. To enhance your safety and the safety of this flight, review this card covering required flightdeck briefing items. If you have questions on this material, please ask your pilot to further explain the system or procedure. In case of an emergency, you will be expected to assist in any way deemed consistent with your capabilities. Do not hesitate to call the crew’s attention to anything out of the ordinary – your extra set of eyes and ears are invaluable to us. Thank you for your assistance. Glad to have you along. Smoking Policy. Piedmont Airlines prohibits smoking anywhere on the aircraft. Sterile Flighdeck. All non-essential conversations or tasks are prohibited during critical phases of flight. Ensure cell phone(s)/PEDs are off. Life Vests. The flightdeck life vests are yellow. Your life vest is located in a storage compartment above the jumpseat. Seatbelt/Shoulder Harness. The lap belt and shoulder harness use a single quick-release buckle. To release the buckle, lift up on the faceplate. Fasten seat belt for takeoff, landing, and turbulence. Fasten the shoulder harness for takeoff and landing. Exception: shoulder harness may be unfastened if it interferes with the performance of duties. Jumpseat. The jumpseat is stowed when not in use. Ask your pilot how to operate the seat if you are unfamiliar. Audio Panel/Headset. VHF-1 is normally used for all ATC communications. Please do not use the microphone for any interphone/radio transmissions. Your audio selector panel is to the right of the jumpseat on the observer’s station. The headset is located in a box on the wall behind the first officer’s head. Oxygen Mask/Smoke Goggle. A full face oxygen mask is located in a pouch on the wall behind the first officer’s seat.

Operation. Remove the mask from the pouch. Position the mask over your head and comfortably locate over nose and mouth. You will have to lean forward as the oxygen line is not long enough to sit upright in the jumpseat. Turn the knob on the oxygen cylinder COUNTERCLOCKWISE to begin the flow of oxygen. Cockpit Door. The cockpit door is secured using the deadbolt lock. Continued on next page

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05/29/15

OBSERVER’S EMERGENCY BRIEFING CARD (Continued) (Continued) Emergency Exits. Unless the captain indicates otherwise…

Primary. Your primary exit is either the forward airstair door or the forward cabin emergency exit door. Al tern ate. If evacuation is not possible through the cabin, the alternate emergency exit is the flight compartment emergency hatch. In Case of an Emergency Evacuation. As soon as possible after the aircraft has come to a complete stop… 1. Stow the jumpseat. 2. Proceed to the cabin and exit the aircraft as directed by the flight attendant. If unable to evacuate out of cabin . Follow either the captain or first officer down the escape rope… 1. Move handle of emergency exit hatch counterclockwise to vent position. Hatch opens inward. 2. Pull handle down to remove hatch. Place hatch against door. 3. Remove the cover on the emergency escape rope (located on left side of emergency exit hatch). 4. Pull the rope out and throw out to the left or right side of aircraft. 5. Use the center console and/or the captain and first officer’s arm rests to exit the emergency hatch. 6. Hold onto the escape rope and slide down the aircraft. 7. After reaching the ground, clear the area. If you do not understand the preceding procedures, please ask the captain or first officer to review them with you. 8. If the preceding procedures are understood, please inform the captain with statement: “The jumpseat briefing is understood.”


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81


82


05/29/15

UNFACTORED LANDING LANDING DISTANCE – INFLIGHT USE ONLY Dry Runway DHC-8-102 Flaps 15 Dry Runway Landing Distance (ft) Landing Weight (1000 lbs) P.A P.A

25.0 26.0 27.0 28.0 29.0 30.0 31.0 32.0 33.0 34.0 34.5

1617 10000 1617

1656 656 1694 1694 1733 733 1771 1771 1810 810 184 1848 1887 1887 192 1925 1964 1964 196 1967

1605 9500 1605

1643 643 1681 1681 1719 719 1757 1757 1795 795 183 1833 1871 1871 190 1909 1947 1947 196 1966

1593 9000 1593

1630 630 1668 1668 1705 705 1743 1743 1780 780 181 1817 1855 1855 189 1892 1930 1930 194 1948

1581 8500 1581

1618 618 1654 1654 1691 691 1728 1728 1765 765 180 1802 1839 1839 187 1876 1913 1913 193 1931

1568 8000 1568

1605 605 1641 1641 1677 677 1714 1714 1750 750 178 1787 1823 1823 185 1859 1896 1896 191 1914

1554 7500 1554

1590 590 1626 1626 1662 662 1698 1698 1734 734 177 1770 1806 1806 184 1842 1878 1878 189 1896

1540 7000 1540

1576 576 1611 1611 1647 647 1683 1683 1718 718 175 1754 1789 1789 182 1825 1861 1861 187 1878

1526 6500 1526

1561 561 1597 1597 1632 632 1667 1667 1702 702 173 1737 1773 1773 180 1808 1843 1843 186 1861

1512 6000 1512

1547 547 1582 1582 1617 617 1652 1652 1686 686 172 1721 1756 1756 179 1791 1826 1826 184 1843

1500 5500 1500

1534 534 1568 1568 1603 603 1637 1637 1671 671 170 1706 1740 1740 177 1774 1809 1809 182 1826

1487 5000 1487

1521 521 1555 1555 1589 589 1622 1622 1656 656 169 1690 1724 1724 175 1758 1791 1791 180 1808

1475 4500 1475

1508 508 1541 1541 1575 575 1608 1608 1641 641 167 1675 1708 1708 174 1741 1774 1774 179 1791

1462 4000 1462

1495 495 1528 1528 1561 561 1593 1593 1626 626 165 1659 1692 1692 172 1725 1757 1757 177 1774

1448 3500 1448

1481 481 1514 1514 1546 546 1579 1579 1612 612 164 1645 1677 1677 171 1710 1743 1743 175 1759

1434 3000 1434

1466 466 1499 1499 1532 532 1565 1565 1597 597 163 1630 1663 1663 169 1695 1728 1728 174 1745

1419 2500 1419

1452 452 1485 1485 1518 518 1550 1550 1583 583 161 1616 1648 1648 168 1681 1714 1714 173 1730

1405 2000 1405

1438 438 1470 1470 1503 503 1536 1536 1568 568 160 1601 1634 1634 166 1666 1699 1699 171 1715

1393 1500 1393

1426 426 1458 1458 1490 490 1522 1522 1555 555 158 1587 1619 1619 165 1652 1684 1684 170 1700

1381 1000 1381

1413 413 1445 1445 1477 477 1509 1509 1541 541 157 1573 1605 1605 163 1637 1669 1669 168 1685

1369 500 1369

1401 401 1433 1433 1464 464 1496 1496 1527 527 155 1559 1590 1590 162 1622 1653 1653 166 1669

1358 0 1358

1389 389 1420 1420 1451 451 1482 1482 1513 513 154 1545 1576 1576 160 1607 1638 1638 165 1654

Adjustments Condition Headwind (20 kts max credit) Tailwind (10 kts max) Upslope (up to 2.00% max)

Instructions:

Correction -10 ft/kt +30 ft/kt -90 ft per 1%

Condition Downslope (up to -2.00% max) Wet Runway De-ice system ON

Correction +230 ft per 1% x 1.30 X 1.16

1. Determine landing distance from table. 2. Correct for winds and any other applicable adjustments 3. Multiply distance by the landing distance correction factor found in the appropriate checklist.

General Landing Distances are calculated using: 34,500 lbs. 2500 Pressure Altitude 1% Downslope 10 Knot Tailwind


05/29/15

83

UNFACTORED LANDING DISTANCE – INFLIGHT USE ONLY Dry Runway DHC-8-102 Flaps 35 Dry Runway Landing Distance (ft) Landing Weight (1000 lbs) P.A P.A

25.0 26.0 27.0 28.0 29.0 30.0 31.0 32.0 33.0 34.0 34.5

1529 10000 1529

1532 1532 1558 1558 1592 1592 1613 1613 1632 1632 165 1651 1655 1655 165 1655 1655 1655 1655 655

1516 9500 1516

1519 1519 1545 1545 1579 1579 1599 1599 1618 1618 163 1636 1653 1653 165 1653 1653 1653 1653 653

1503 9000 1503

1506 1506 1531 1531 1566 1566 1585 1585 1604 1604 162 1622 1640 1640 165 1659 1659 1659 1659 659

1490 8500 1490

1492 1492 1518 1518 1552 1552 1572 1572 1589 1589 160 1607 1625 1625 165 1657 1663 1663 1663 663

1477 8000 1477

1479 1479 1505 1505 1539 1539 1558 1558 1575 1575 159 1592 1610 1610 164 1641 1667 1667 1667 667

1464 7500 1464

1467 1467 1492 1492 1525 1525 1545 1545 1562 1562 157 1579 1596 1596 162 1627 1658 1658 1674 674

1452 7000 1452

1455 1455 1479 1479 1511 1511 1533 1533 1549 1549 156 1565 1582 1582 161 1613 1644 1644 1659 659

1440 6500 1440

1443 1443 1466 1466 1497 1497 1520 1520 1536 1536 155 1552 1568 1568 159 1599 1629 1629 1644 644

1428 6000 1428

1430 1430 1453 1453 1482 1482 1507 1507 1522 1522 153 1538 1554 1554 158 1584 1615 1615 1630 630

1416 5500 1416

1418 1418 1441 1441 1470 1470 1493 1493 1509 1509 152 1525 1541 1541 157 1570 1600 1600 1614 614

1403 5000 1403

1406 1406 1429 1429 1458 1458 1479 1479 1495 1495 151 1511 1528 1528 155 1556 1585 1585 1599 599

1391 4500 1391

1393 1393 1417 1417 1446 1446 1465 1465 1482 1482 149 1498 1515 1515 154 1542 1570 1570 1584 584

1379 4000 1379

1381 1381 1405 1405 1434 1434 1452 1452 1468 1468 148 1485 1502 1502 152 1528 1555 1555 1568 568

1370 3500 1370

1371 1371 1394 1394 1422 1422 1440 1440 1456 1456 147 1473 1489 1489 151 1515 1541 1541 1555 555

1360 3000 1360

1362 1362 1384 1384 1410 1410 1428 1428 1444 1444 146 1461 1477 1477 150 1502 1528 1528 1541 541

1351 2500 1351

1353 1353 1373 1373 1398 1398 1416 1416 1432 1432 144 1448 1465 1465 148 1489 1515 1515 1527 527

1342 2000 1342

1344 1344 1362 1362 1386 1386 1404 1404 1420 1420 143 1436 1453 1453 147 1476 1501 1501 1514 514

1330 1500 1330

1332 1332 1352 1352 1377 1377 1394 1394 1409 1409 142 1425 1441 1441 146 1464 1489 1489 1502 502

1318 1000 1318

1320 1320 1341 1341 1367 1367 1383 1383 1398 1398 141 1413 1428 1428 145 1451 1477 1477 1491 491

1306 500 1306

1308 1308 1331 1331 1357 1357 1372 1372 1387 1387 140 1402 1416 1416 143 1439 1466 1466 1479 479

1294 0 1294

1296 1296 1321 1321 1347 1347 1362 1362 1376 1376 139 1390 1404 1404 142 1427 1454 1454 1467 467

Adjustments Condition Headwind (20 kts max credit) Tailwind (10 kts max) Upslope (up to 2.00% max)

Instructions:

Correction -10 ft/kt +30 ft/kt -80 ft per 1%

Condition Downslope (up to -2.00% max) Wet Runway De-ice system ON

Correction +200 ft per 1% x 1.30 X 1.10

1. Determine landing distance from table. 2. Correct for winds and any other applicable adjustments 3. Multiply distance by the landing distance correction factor found in the appropriate checklist.

General Landing Distances are calculated using: 34,500 lbs. 2500 Pressure Altitude 1% Downslope 10 Knot Tailwind

84


05/29/15

D A S H 8 1 0 2 E m e r g e n c y / N o n -N o r m a l C h e c k l i s t 0 5 / 2 9 / 1 5

8 5

Runway Slope In Percent

M a x i m u m S l o p e + / 2 . 0 %

Runway Length (Feet)

Difference Between Threshold Elevations (FT) 10

20

30

40

50

60

70

80

90

100

110

120

12,000

0.1

0.2

0.3

0.3

0.4

0.5

0.6

0.7

0.8

0.8

0.9

1.0

11,000

0.1

0.2

0.3

0.4

0.5

0.5

0.6

0.7

0.9

0.9

1.0

1.1

10,000

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

1.0

1.0

1.1

1.2

9,000

0.1

0.2

0.3

0.4

0.6

0.7

0.8

0.9

1.1

1.1

1.2

1.3

8,000

0.1

0.3

0.4

0.5

0.6

0.8

0.9

1.0

1.3

1.3

1.4

1.5

7,000

0.1

0.3

0.4

0.6

0.7

0.9

1.0

1.1

1.4

1.4

1.6

1.7

6,000

0.2

0.3

0.5

0.7

0.8

1.0

1.2

1.3

1.7

1.7

1.8

2.0

5,000

0.2

0.4

0.6

0.8

1.0

1.2

1.4

1.6

2.0

2.0

2.2

2.4

4,000

0.3

0.5

0.8

1.0

1.3

1.5

1.8

2.0

2.5

2.5

2.8

3.0

3,000

0.3

0.7

1.0

1.3

1.7

2.0

2.3

2.7

3.0

3.3

3.7

4.0

R u n w a y S l o p e I n P e r c e n t C h a r t

Record of Revisions Baseline: 26 OCT 11 Revision

Initials

Revision

Number

Date

Number

1

10/26/11

PUBS

26

2

02/08/12

PUBS

27

3

06/04/12

PUBS

28

4

12/20/12

PUBS

29

5

02/12/13

PUBS

30

6

06/03/13

PUBS

31

7

04/23/14

PUBS

32

8

07/11/14

PUBS

33

9

11/14/14

PUBS

34

10

05/29/15

PUBS

Date

35

11

36

12

37

13

38

14

39

15

40

16

41

17

42

18

43

19

44

20

45

21

46

22

47

23

48

24

49

25

50

86

Initials


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List of Effective Pages

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45 ...... 29MAY15 46 ...... 29MAY15 47 ...... 29MAY15 48 ...... 29MAY15 49 ...... 29MAY15 50 ...... 29MAY15 51 ...... 29MAY15 52 ...... 29MAY15 53 ...... 29MAY15 54 ...... 29MAY15 55 ...... 29MAY15 56 ...... 29MAY15 57 ...... 29MAY15 58 ...... 29MAY15 59 ...... 29MAY15 60 ...... 29MAY15 61 ...... 29MAY15 62 ...... 29MAY15 63 ...... 29MAY15 64 ...... 29MAY15 65 ...... 29MAY15 66 ...... 29MAY15 67 ...... 29MAY15 68 ...... 29MAY15 69 ...... 29MAY15 70 ...... 29MAY15 71 ...... 29MAY15 72 ...... 29MAY15 73 ...... 29MAY15 74 ...... 29MAY15 75 ...... 29MAY15 76 ...... 29MAY15 77 ...... 29MAY15 78 ...... 29MAY15 79 ...... 29MAY15 80 ...... 29MAY15 81 ...... 29MAY15 82 ...... 29MAY15 83 ...... 29MAY15 84 ...... 29MAY15 85 ...... 29MAY15 86 ...... 29MAY15 87 ...... 29MAY15 88 ...... 29MAY15 iii ........ 29MAY15 iv ....... 29MAY15


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