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TFDi Design
QRH

Emergency

ALL ENGINE FLAMEOUT

NOTE

All engine flameout can be recognized by decrease in EGT, N2, and fuel flow. This will be followed closely by a decrease in N1.

1. ENG IGN OVRD SWITCH - OVRD ON

  • Move the ENG IGN OVRD switch to the OVRD ON position.

2. ADG - DEPLOY

  • Set the ADG to the DEPLOY position.

Air start envelope is 250 KIAS to VMO, SL to FL300. Control aircraft at an IAS to obtain a minimum N2 of 15% for air start.

MINIMUM AIRSPEED FOR CONTROLLABILITY (KIAS)

Gross Weight (1000 Kg)UP/RET0/EXT28/EXT
160188155155
180200161155
200209170157
230224182168
250234190176

NOTE

If desired, and time permits, CABIN PRESS system may be operated in MANUAL and outflow valve selected CLOSED to minimize cabin rate of climb until an engine restart is achieved. When an engine restarts, return system to automatic mode.

3. THROTTLES (ALL) - IDLE

  • Move all throttles to the IDLE position

NOTE

Airstarts, especially at high altitudes, may result in the engine(s) accelerating to idle very slowly. Slow acceleration may be incorrectly interpreted as a hung start or engine malfunction. If N2 is steadily increasing and EGT remains within limits, the start is progressing normally.

ANY ENGINE RESTARTS

IF NO ENGINE STARTS, SKIP TO STEP 8

4. ADG ELEC SWITCH - ON

  • Move the ADG ELEC switch to the ON position.

5. REMAINING ENGINES - RESTART

6. LAND AT NEAREST SUITABLE AIRPORT

  • Landing at the nearest suitable airport for aircraft repair.

TWO ENGINES DO NOT RESTART

IF TWO ENGINES RESTART, SKIP TO STEP 9

NOTES

  • With only one generator operating, bus splitting during autopilot ILS approach will not take place.
  • The ADG output will be lost during landing roll at approx. 80 KIAS. Consequently, RH EMER buses will become unpowered and F/O's DUs are lost.
  • To avoid bus splitting during ILS approach consider using LOC/TRK and FPA or do not use autopilot below 1.500 feet RA.

7. REFER TO TWO ENGINES INOPERATIVE.

[END OF TWO ENGINES DO NOT RESTART CHECKLIST]

ONE ENGINE DOES NOT RESTART

IF ONE ENGINE RESTARTS, END OF "ONE ENGINE DOES NOT RESTART" CHECKLIST

8. REFER TO ENGINE SHUTDOWN IN FLIGHT.

[END OF ONE ENGINE DOES NOT RESTART CHECKLIST]

9. FLAPS / SLATS - MAINTAIN

  • Maintain the last configured flap position, Do not attempt to reconfigure.

DITCHING REQUIRED

IF DITCHING IS NOT REQUIRED SKIP TO STEP 11

10. REFER TO ABNORMAL NON-ALERT PROCEDURE - DITCHING

[END OF DITCHING CHECKLIST]

11. REFER TO ABNORMAL NON-ALERT PROCEDURE - EMERGENCY LANDING ON TERRAIN

[END OF EMERGENCY LANDING ON TERRAIN CHECKLIST]

DITCHING

1. (SR.) PURSER AND PASSENGERS - INFORM

  • Inform purser and all passengers of the plan to ditch.

2. TRANSPONDER - SET 7700

  • Set the transponder to 7700.

3. ATC - ADVISE

  • Advise ATC of the planned ditching.

4. FUEL QUANTITY - REDUCE

  • Reduce the fuel quantity onboard.

5. VAPP - CHECKED MINIMUM 160 KIAS

  • Check that VAPP is a minimum of 160 KIAS

6. APU - VERIFY OFF

  • Verify the APU is OFF.

7. TERRAIN OVRD - OVRD

  • Set the TERRAIN OVRD switch to the OVRD position.

8. FIRST AID AND SURVIVAL EQUIPMENT / LOOSE EQUIPMENT - STOW

  • STOW all first aid and survival / loose equipment.

9. OBSERVERS SEAT (IF OCCUPIED) - FACING FORWARD

  • If the Observers seat is occupied ensure it is facing forwards.

10. NO SMOKE AND SEAT BELTS SWITCHES - ON

  • No smoking and seat belt signs set to ON position.

11. CREW LIFE VESTS, BELTS, HARNESSES - ON / FASTENED

  • Ensure all crew members have sufficient life vests, belts and harnesses ON AND FASTENED.

12. DITCHING SWITCH - ON

  • Set the DITCHING switch to the ON position.

LANDING ASPECTS

13. LANDING CONFIGURATION - GEAR UP / FLAPS 50

  • Plan the landing configuration to be gear UP and flaps 50.
  • Land parallel to the swell. Strong crosswind may require a compromise heading between wind direction and swell pattern. Decrab before contact, however keep wings level.
  • In stormy wind conditions without clearly defined swells, land into the wind.
  • Never land into the face of a swell.
  • Final rate of descent 500 ft/min when thrust is available.
  • Just prior to contact reduce rate of descent and maintain this attitude.
  • Keep thrust on until contact (If Applicable).
  • Do not stall.

14. CABIN READY REPORT - RECEIVED

  • Monitor and confirm the cabin ready report is received.

15. CABIN CREW PREPARE FOR LANDING - ANNOUNCED

  • Announce for Cabin Crew to prepare for landing.

AIR SYSTEM MANUAL

IF THE AIR SYSTEM IS IN AUTO, SKIP TO CABIN PRESSURIZATION MANUAL

16. AVNCS FAN SWITCH - OVRD

  • Set the AVNCS FAN switch to the OVRD position.

Wait until at or below 10000 feet

17. PACK AND BLEED SWITCHES - OFF

  • Set all packs and bleed switches to the OFF position.

CABIN PRESSURIZATION MANUAL

IF THE CABIN PRESSURIZATION IS IN AUTO, SKIP TO HYDRAULIC SYSTEM MANUAL

Wait until at or below 10000 feet

18. CABIN PRESS MANUAL RATE SELECTOR - CLIMB

  • Set the CABIN PRESS MANUAL RATE SELECTOR to the CLIMB position.

Wait until aircraft is depressurized (cabin differential pressure less than 0.5 psi)

19. CABIN PRESS MANUAL RATE SELECTOR - FULL DESC

  • Set the CABIN PRESS MANUAL RATE SELECTOR to the FULL DESC position.

HYDRAULIC SYSTEM MANUAL

IF THE HYDRAULIC SYSTEM IS IN AUTO, SKIP TO WHEN PASSING 2500 FEET RA / HAT

20. 1-3 AND 2-3 RMP'S - ON

  • Set 1-2 and 2-3 RMP's to the ON position.

Wait until passing 2500 feet RA / HAT

21. CABIN CREW TAKE YOUR SEATS - ANNOUNCED

  • Announce for Cabin crew to take their seats.

22. DUMP SWITCH - OFF

  • Set the dump switch to the OFF position

23. GEAR HANDLE / LIGHTS - UP / OFF

  • Ensure gear handle is in the UP position and lights are OFF.

Wait until passing 500 feet RA / HAT

24. BRACE FOR IMPACT - ANNOUNCE

  • Announce to brace for impact.

25. FLAP / SLAT HANDLE - 50 / EXT

  • Set the FLAP / SLAT handle to the 50 / EXT

NOTE

Possibility of continuous aural warnings.

Wait until aircraft has stopped

26. EVACUATE AIRCRAFT - ANNOUNCE

  • Announce to evacuate aircraft.

27. EVACUATION SIGNAL SWITCH - ON

  • Set the evacuation signal switch to the ON position.

NOTE

If time permits, prior to leaving aircraft, move all ENG FIRE handles DOWN.

[END DITCHING CHECKLIST]

EMERGENCY DESCENT

1. ALTITUDE SELECT KNOB - REDUCE / PULL

  • Initiate descent to 10000 feet or minimum safe altitude, whichever is higher.

2. SPOILER HANDLE - SPD BRK FULL

  • Move the spoiler to the SPD BRK FULL position

WARNING

If structural damage is suspected or turbulence present, do not exceed .82 Mach / 305 KIAS

3. IAS / MACH SELECT KNOB - SELECT .85 MACH / 320-350 KIAS

  • Change the IAS / MACH Select knob to 320-350 KIAS or .85 MACH.

4. DESCENT - MAX PITCH 10° / MAX BANK 30°

  • Monitor descent ensuring the aircraft does not pass a max pitch of 10° and a max bank rate of 30°.

5. TRANSPONDER (UNLESS OTHERWISE REQUIRED) - 7700

  • Set transponder code / squawk to 7700.

6. NO SMOKE AND SEAT BELT SWITCHES - ON

  • Set the NO SMOKE and SEAT BELT switches to the ON position.

Wait until after descent

CABIN ALTITUDE ABOVE 14000 FT

IF CABIN ALTITUDE IS BELOW 14000 FT, SKIP TO STEP 8

7. CABIN CREW AND PASSENGERS, KEEP MASKS ON - ANNOUNCED

  • Announce to Cabin Crew and Passengers to keep masks on.

8. CABIN CREW AND PASSENGERS, TAKE MASKS OFF - ANNOUNCED

  • Announce to Cabin Crew and Passengers to take masks off.

CAUTION

Cabin crew should be briefed to keep passengers away from the cabin doors as these can be opened in flight with differential pressure less than 1 psi.

9. OXYGEN MASK DOORS - CLOSE

  • CLOSE the oxygen mask doors.

10. PRESS TO TEST AND RESET LEVER - PUSH

  • PUSH the press to test and reset lever.

[END OF EMERGENCY DESCENT CHECKLIST]

EMERGENCY LANDING ON TERRAIN

1. (SR.) PURSER AND PASSENGERS - INFORM

  • Inform purser and all passengers of the plan to ditch.

2. TRANSPONDER - SET 7700

  • Set the transponder to 7700.

3. ATC - ADVISE

  • Advise ATC of the planned ditching.

4. FUEL QUANTITY - REDUCE

  • Reduce the fuel quantity onboard.

5. VAPP - CHECKED MINIMUM 160 KIAS

  • Check that VAPP is a minimum of 160 KIAS

6. APU - VERIFY OFF

  • Verify the APU is OFF.

7. TERRAIN OVRD - OVRD

  • Set the TERRAIN OVRD switch to the OVRD position.

8. FIRST AID AND SURVIVAL EQUIPMENT / LOOSE EQUIPMENT - STOW

  • STOW all first aid and survival / loose equipment.

9. OBSERVERS SEAT (IF OCCUPIED) - FACING FORWARD

  • If the Observers seat is occupied ensure it is facing forwards.

10. NO SMOKE AND SEAT BELTS SWITCHES - ON

  • No smoking and seat belt signs set to ON position.

11. CREW LIFE VESTS, BELTS, HARNESSES - ON / FASTENED

  • Ensure all crew members have sufficient life vests, belts and harnesses ON AND FASTENED.

12. DITCHING SWITCH - ON

  • Set the DITCHING switch to the ON position.

LANDING ASPECTS

13. LANDING CONFIGURATION - GEAR DOWN SUBJECT CAPTAIN'S DISCRETION (SCD) / FLAPS 50

  • Plan the landing configuration to be gear DOWN and flaps 50.

CAUTION

Do not use center gear when landing on terrain.

14. CABIN READY REPORT - RECEIVED

  • Monitor and confirm the cabin ready report is received.

15. CABIN CREW PREPARE FOR LANDING - ANNOUNCED

  • Announce for Cabin crew to prepare for landing.

16. CTR GEAR NORM / UP SWITCH - UP

  • Set the CTR GEAR NORM / UP switch to the UP position.

AIR SYSTEM MANUAL

IF THE AIR SYSTEM IS IN AUTO, SKIP TO CABIN PRESSURIZATION MANUAL

17. AVNCS FAN SWITCH - OVRD

  • Set the AVNCS FAN switch to the OVRD position.

Wait until at or below 10000 feet

18. PACK AND BLEED SWITCHES - OFF

  • Set all packs and bleed switches to the OFF position.

CABIN PRESSURIZATION MANUAL

IF THE CABIN PRESSURIZATION IS IN AUTO, SKIP TO HYDRAULIC SYSTEM MANUAL

Wait until at or below 10000 feet

19. CABIN PRESS MANUAL RATE SELECTOR - CLIMB

  • Set the CABIN PRESS MANUAL RATE SELECTOR to the CLIMB position.

Wait until aircraft is depressurized (cabin differential pressure less than 0.5 psi)

20. CABIN PRESS MANUAL RATE SELECTOR - FULL DESC

  • Set the CABIN PRESS MANUAL RATE SELECTOR to the FULL DESC position.

HYDRAULIC SYSTEM MANUAL

IF THE HYDRAULIC SYSTEM IS IN AUTO, SKIP TO WHEN PASSING 2500 FEET RA / HAT

21. 1-3 AND 2-3 RMP'S - ON

  • Set 1-2 and 2-3 RMP's to the ON position.

If alternate gear extension is required:

22. SPEED - MAX 230 KIAS

  • Ensure speed does not pass 230 KIAS.

23. ALTERNATE GEAR EXTENSION LEVER - RAISE / LATCH

  • Set the alternate gear extension lever to the RAISE / LATCH position.

Wait until passing 2500 feet RA / HAT

24. CABIN CREW TAKE YOUR SEATS - ANNOUNCE

  • Announce for Cabin crew to take their seats.

25. DUMP SWITCH - OFF

  • Set the dump switch to the OFF position

26. GEAR UP OR DOWN

  • Set the gear to either UP or DOWN as the situation requires.

Wait until passing 500 feet RA / HAT

27. BRACE FOR IMPACT - ANNOUNCE

  • Announce to brace for impact.

Wait until aircraft has stopped

28. EVACUATE AIRCRAFT - ANNOUNCE

  • Announce to evacuate aircraft.

29. EVACUATION SIGNAL SWITCH - ON

  • Set the evacuation signal switch to the ON position.

NOTE

If time permits, prior to leaving aircraft, move all ENG FIRE handles DOWN.

[END EMERGENCY LANDING ON TERRAIN CHECKLIST]

EVACUATION

After aircraft has stopped

1. OUTFLOW VALVE - VERIFY OPEN

  • Verify that the outflow valve is OPEN.

2. PARK HANDLE - PARK

  • Set the park brake handle to the PARK position.

3. SPOILER HANDLE - RET

  • Set the Spoiler handle to the RET position.

4. FUEL SWITCHES - OFF

  • Set the fuel switches to the OFF position.

5. EVACUATE AIRCRAFT - ANNOUNCE

  • Announce to evacuate aircraft.

6. EVACUATION SIGNAL SWITCH - ON

  • Set the EVACUATION SIGNAL switch to the ON position.

7. ENG FIRE HANDLES - DOWN / DISCHARGE

  • Set the ENG FIRE HANDLES to the DOWN / DISCHARGE position.

8. APU FIRE HANDLE - PULL / ROTATE

  • PULL / ROTATE the APU FIRE HANDLE.

9. ATC - INFORM

  • Inform ATC of evacuation.

10. EMER PWR SELECTOR - OFF

  • Set the EMER PWR SELECTOR to the OFF position.

11. BAT SWITCH - OFF

  • Set the BAT switch to the OFF position.

NOTES

  • Inform ATC by distress call. Conditions permitting, this call can be given earlier in sequence.
  • Manual operation of crew seats required.
  • In order to prevent confusion in the cabin, in principle no announcements will be made by the cockpit crew regarding exits to be used and/or exits not to be used during the evacuation. In case of a cabin fire, opening of as many exits as possible gives a better chance for survival due to the fact that more fresh (breathing) air enters the cabin.
  • Any additional crewmember must leave the cockpit immediately.
  • Only AGT LOW lights of engine 2 will illuminate.

[END EVACUATION CHECKLIST]

RTO FOLLOW-UP

If it is decided not to evacuate, depending on circumstances:

  • Start APU.
  • Consider to vacate the runway.
  • Inform ATC accordingly, request technical assistance, stairs and chocks.
  • Inform (Sr.) purser and passengers.
  • Shut down engines.
  • Switch off BCN and HI-INT lights.
  • Perform the Normal Procedures.
  • Consider towing the aircraft to a parking position and/or disembark passengers via stairs.
  • Pull COCKPIT VOICE RECORDER circuit breaker on the overhead panel (F20).

[END RTO FOLLOW-UP CHECKLIST]

TWO ENGINES INOPERATIVE

ON FINAL APPROACH WITH GEAR DOWN

IF GEAR FAILS TO COME DOWN OR NOT ON FINAL APPROACH, SKIP TO STEP 4

1. THRUST - AS REQUIRED

  • Set thrust to where it is required

2. FLAPS - 28

  • Flaps set to the 28 postion

3. SPEED - VREF (28) + 5

  • Monitor speed ensuring it is VREF + 5

NOTES

  • Continue approach.
  • Move GWPS Switch to FLAP OVRD, conditions permitting.

[END OF TWO ENGINES INOPERATIVE CHECKLIST]

4. THRUST - MCT

  • Set thrust to the MCT position

5. FLAPS - ZERO

  • Set the flaps to ZERO position

6. SPEED - DRIFTDOWN OR UP / RET VMIN + 30

  • Allow speed to driftdown or up / retard VMIN + 30

NOTE

Delay gear retraction until flaps are zero.

7. GEAR - UP

  • Move the gear into the UP position.

8. SLATS - RET

  • Set the slats to retract.

9. ENG IGN OVRD SWITCH - OVRD ON

  • Set the engine ignition switch to the OVRD ON postion

10. LAND AT NEAREST SUITABLE AIRPORT

  • Landing at the nearest suitable airport for aircraft repair.

DRIFTDOWN REQUIRED

IF DRIFTDOWN IS NOT REQUIRED, SKIP TO STEP 14

DRIFTDOWN

ALT (1000 FT)UNITSINITIAL GROSS WEIGHT (1000 KG)
140160180200220240260
40Kt227245249Start of Driftdown Speed
Ft254542213019292Max 1 Eng Alt (Airfoil & Engine A-Ice ON, reduce by 1500ft)
NMi348376387Distance to Bottom of Driftdown
Kg426551175802Fuel Burned to Bottom of Driftdown
Kt216230244Bottom of Driftdown Speed 1 Eng Altitude
Kg/Hr463853116033Fuel Flow at 1 Engine Altitude
35Kt224241257272279
Ft2540622095192651632813623
NMi307342361393407
Kg39744878560366607410
Kt216230244256268
Kg/Hr46495320603966727348
30Kt221238253268282296309
Ft2531222031192121628513588106887482
NMi249296323360379427483
Kg34104448529163677184871010613
Kt217231244256268279289
Kg/Hr4670533660506682735679538493
25Kt235250265278292304
Ft21887191131621213528106317421
NMi218269316342393453
Kg3482466358716791837310335
Kt231245257269279289
Kg/Hr537260716699736979648500
20Kt248262276288301
Ft188361606613421105387323
NMi156248291351416
Kg28964882609778159888
Kt246257269279289
Kg/Hr61316732739179818511
15Kt273286298
Ft13142103447141
NMi192284365
Kg428466609060
Kt270280290
Kg/Hr745180178531
10Kt284296
Ft97866733
NMi120277
Kg29837203
Kt282291
Kg/Hr81418577

11. MINIMUM SAFE ALTITUDE / RANGE CAPACITY - DETERMINE

  • Minimum safe altitude and range capacity to be determined.

12. FUEL DUMP - CONSIDER

  • Consider the option of dumping fuel.

13. DRIFTDOWN ALTITUDE - SELECT

  • Select driftdown altitude as necessary.

At bottom of driftdown:

  • Level off at maximum one engine altitude
  • Maintain altitude and allow aircraft to accelerate to 290 KIAS as gross weight is reduced by fuel burn
  • Maintain 290 KIAS for curise / climb (autothrottles may be used).

14. APPROPRIATE ENGINE SHUTDOWN PROCEDURE - COMPLETE

  • Complete the engine shutdown procedure as is required.

NOTE

Consider fuel dump to reduce gross weight to minimum practical.

15. AUTOTHROTTLES - AS REQUIRED

  • Set the autothrottles as is required for the current situation.

16. ALTIMETERS - SET / CROSS CHECKED

  • Ensure the altimeters are set and cross checked.

17. GPWS - FLAP OVRD

  • Set the GPWS switch to the FLAP OVRD position.

NOTE

If deemed necessary to start APU for electrical back-up, use the APU START/STOP switch on the APU panel. With one (or more) engine generator operating do not connect APU generator to busses to prevent undesirable electrical system behaviour.

Wait until at or below 10,000 feet MSL

AIR SYS MANUAL

IF AIR SYS IS IN AUTO, SKIP TO HYDRRAULIC SYSTEM MANUAL

PACK SWITCHES (ALL) - OFF

  • Move all pack switches to the OFF position.

HYDRAULIC SYSTEM MANUAL

IF HYDRAULIC SYSTEM IS IN AUTO, SKIP TO APPROACH ASPECTS

18. 1-3 / 2-3 RMP's - ON

  • Move the 1-3 / 2-3 RMP's to the ON position.

APPROACH ASPECTS

  • Maintain clean configuration and UP/RET Vmin + 30 until maneuvering has been completed.
  • Use normal descent and approach checklists.
  • Landing configuration is with Slats extended only.
  • Plan for a long final approach.
  • Check VMIN for approach configurations:
WEIGHT (1000 KG)150160170180190200210220
UP/RET VMIN + 30211217223228234240245250
0/EXT VMIN + 30177182187191196200204208
0/EXT VMIN + 15162167172176181185189193
  • Check calculated landing distance (m):
WEIGHT (1000 KG)150160170180190200210220
Braking Action Good20802170227023602470256026602760
Braking Action Medium29003030319033303520365038003950
VAPP per kt above VMIN + 15+50
Per 1,000ft press altitude+130
Per 10°C above ISA+130
Per 0.1% UP / DOWN slope-25 / +65
Per kt HEAD / TAIL wind-20 / +40

When established on final

  • Slats Extend.
  • Speed VMIN + 30.
  • Landing clearance received.

At glide slope intercept

  • Maintain VMIN + 30 for go-around protection until committed to land (1,000 feet AGL)

NOTE

At 1,200 feet AGL the gear warning horn will sound.

At 1,000 feet AGL

  • Gear Down.

LANDING ASPECTS

  • At approx. 500 feet AGL:
    • Rudder trim zero.
  • Between 1,000 feet and 50 feet AGL:
    • Reduce speed slowly to reach VMIN + 15 approx. at 50 feet AGL.
    • Use only a slight flare. Excessive flare will result in float, excessive use of runway and possible tail strike.
    • Reduce thrust to idle at touchdown.
  • At main gear touchdown:
    • Pull reverse levers to the interlock.
    • Positively lower nose gear to runway.

ROLL-OUT ASPECTS

  • Select reverse thrust within controllable limits.
  • Check spoilers extend.

NOTE

Auto ground spoilers will not deploy until nose gear touchdown.

  • Apply manual braking

GO-AROUND ASPECTS

CAUTION

Do not attempt a go-around under any of the following conditions:

  • Altitude less than 1,000 feet AGL.
  • Airspeed below 0/EXT VMIN + 30.
  • Gear is extended.
  • Hydraulic system 1 or 3 failed. Outboard slats will not retract. “SLAT DISAG” alert will be displayed when flap/slat handle is in the UP/RET position.
  • GW in excess of that shown in the following chart.

MAX WGT FOR TWO ENGINES INOPERATIVE MISSED APPROACH

PRESS ALT

TEMPERATURE MAXIMUM WEIGHT (1000 KG)

STD TEMP

S.L.-65°C-45°C-25°C-5°C15°C25°C35°C45°C55°C
235237239240241242222206189
2000 FT-69°C-49°C-29°C-9°C11°C21°C31°C41°C51°C
227229231232233233214198182
4000 FT-73°C-53°C-33°C-13°C7°C17°C27°C37°C47°C
221222223222222221207190175
6000 FT-77°C-57°C-37°C-17°C3°C13°C23°C33°C43°C
211211211211210209201185169
8000 FT--61°C-41°C-21°C-1°C9°C19°C29°C39°C
-199198197195195194179162
10000 FT--65°C-45°C-25°C-5°C5°C15°C25°C35°C
-185184183182181180172159

NOTE

Packs off, engine and airfoil ice protection off

When initiating missed approach

19. GO-AROUND THRUST - SET

  • Set Go-Around thrust for the missed approach

20. SPEED - UP / RET VMIN + 30

  • UP/RET VMIN + 30

21. FLAP / SLAT HANDLE - UP / RET

  • Move the Flap / slat handle to the UP/RET position.

QRH LANDING CHECKLIST

Sterile Cockpit
Chime
Fuel Dump
Check Off
Spoilers
Armed
Autobrake
Off
Altimeters
Set Local QNH
Flaps
0 / EXT
EAD
Checked
FCP
Set

When passing 1000 ft AGL, after selecting gear down

VAPP
VMIN + 15
Rudder Trim
Zero
Gear
Down, Confirm All Green

[END OF TWO ENGINES INOPERATIVE CHECKLIST]

CARGO DOOR

SINGLE ALERT DISPLAYED

IF MORE OR LESS THEN A SINGLE ALERT IS DISPLAYED, SKIP TO OBSERVE AIR SYNOPTIC

Observe MISC synoptic

1. CARGO DOOR TEST SWITCH - PUSH AND HOLD

  • PUSH AND HOLD the cargo door test switch.

2. CARGO DOOR ALERT - CHECK

  • CHECK to see if the cargo door alert is still displayed

3. CARGO DOOR TEST SWITCH - RELEASE

  • RELEASE the cargo door test switch.

OTHER SENSOR OF AFFECTED DOOR ALSO DISPLAYED ON SYNOPTIC DURING TEST

IF OTHER SENSOR OF AFFECTED DOOR DID NOT DISPLAY ON SYNOPTIC DURING TEST, SKIP TO OBSERVE AIR SYNOPTIC

No further crew action required. Make log entry.

[END CARGO DOOR CHECKLIST]

Observe AIR synoptic.

4. CABIN PRESS SYSTEM SELECT SWITCH - MANUAL

  • Set the CABIN PRESS SYSTEM SELECT switch to the MANUAL position.

Rotate CABIN PRESS manual rate selector towards climb and observe indicator moves toward OP.

Descend aircraft to 15000 feet or minimum safe altitude whichever is higher

Reduce cabin differential pressure to 2 psi or less.

NOTE

An aircraft altitude of 15,000 feet provides 9,500-feet cabin altitude at 2-psi differential pressure.

5. LAND AT NEAREST SUITABLE AIRPORT

  • Landing at the nearest suitable airport for aircraft repair.

[END CARGO DOOR CHECKLIST]

SEVERE DAMAGE TO COCKPIT OVERHEAD STRUCTURE

This procedure is to be used any time the cockpit overhead structure is struck by a foreign object.

NOTE

A severe blow to the fuselage structure in the area of the cockpit overhead could result in a loss of all primary electrical power, and all hydraulic power, and all hydraulic system status indications on the EAD and/or hydraulic system display (synoptic) and/or HYD control panel (forward overhead panel).

1. HYD CUE SWITCH - PUSH

  • PUSH the HYD CUE switch.

SYNOPTIC LINES OR SYSTEM PRESSURE DISPLAYED AND INDICATE NORMAL OPERATION OF HYDRAULIC PUMPS

IF SYNOPTIC LINES OR SYSTEM PRESSURE DISPLAYED AND DO NOT INDICATE NORMAL OPERATION OF HYDRAULIC PUMPS, SKIP TO STEP 2

No further crew action required.

[END SEVERE DAMAGE TO COCKPIT OVERHEAD STRUCTURE CHECKLIST]

2. ADG - DEPLOY

  • Set the ADG to the DEPLOY position.

3. ENG HYD PUMP CONTROL LEFT (A2) AND RIGHT (A3) CIRCUIT BREAKERS (LEFT OVERHEAD) - PULL

  • PULL the ENG HYD PUMP CONTROL LEFT and RIGHT circuit breakers.

NOTE

Removing electrical power from ENG HYD PUMPS control will cause the associated engine driven hydraulic pumps to come on.

4. ADG ELEC SWITCH - ON

  • Set the ADG ELEC switch to the ON position.

NOTE

If electric power is not available, engine 2 may flame out.

CAUTION

Do not dump fuel. If necessary, perform an overweight landing.

[END SEVERE DAMAGE TO COCKPIT OVERHEAD STRUCTURE CHECKLIST]

SEVERE TURBULENCE AND / OR HEAVY RAIN INGESTION

NOTE

In areas of turbulence, fly the FMS optimum altitude when possible. Buffet margin and economy will be enhanced. Descend if necessary to improve buffet margin.

1. SEAT BELTS - ON

  • Ensure seat belts are on.

2. CABIN CREW AND PASSENGERS TAKE YOUR SEATS - ANNOUNCE

  • ANNOUNCE to the cabin crew and passengers to take their seats.

3. TURBULENCE PENETRATION SPEED - 290 KIAS - 305 KIAS OR .80 - .83 MACH WHICHEVER RANGE IS LOWER

  • Ensure to stay in range of speed for Turbulence.

NOTE

Below 10,000 feet, the greater of 250 KIAS or CLIMB SPEED may be used.

4. ENG IGN OVRD SWITCH - OVRD ON

  • Set the ENG IGN OVRD switch to the OVRD ON position.

5. AUTOTHROTTLES - OFF

  • Set the autothrottles to OFF

NOTE

Adjust throttles only if necessary to correct excessive airspeed variation or to avoid exceeding redline limits. Do not chase airspeed.

6. ANTI-ICE SYSTEM SWITCH - MANUAL

  • Set the ANTI-ICE SYSTEM switch to the MANUAL position.

7. ENG, WING AND TAIL ANTI-ICE SWITCHES - ON

  • Set the ENG, WING AND TAIL ANTI-ICE switches to the ON position.

8. ECON SWITCH - OFF

  • Set the ECON switch to the OFF position.

9. AUTOPILOT - MONITOR

  • MONITOR the autopilot.

Use the autopilot in turbulence.

Closely monitor autopilot operation and be prepared to disconnect the autopilot only if the aircraft does not maintain an acceptable attitude. If the autopilot disconnects the pilot should smoothly take control and stabilize the pitch attitude. Fly attitude as the primary pitch reference. Sacrifice altitude to maintain attitude. Disregard the flight director pitch bar. Do not trim manually. After recovery, the autopilot should be reengaged if available. If the autopilot is engaged outside the capture zone of the FCP altitude, a new altitude will be automatically commanded and smoothly captured.

NOTE

Because the autopilot cannot respond correctly when inputs are made to the control wheel or column, it is designed to disconnect automatically if there are sustained pilot inputs. However, the pilot should never make control inputs when the autopilot is engaged, because at disconnect there will be a sudden and abrupt movement of some flight control surfaces with an associated but unpredictable aircraft response.

Wait until severe turbulence and/or heavy rain no longer exist

10. ECON SWITCH - ON

  • Set the ECON switch to the ON position.

11. ANTI-ICE SYSTEM SWITCH - AUTO

  • Set the ANTI-ICE SYSTEM switch to the AUTO position.

12. AUTOTHROTTLES - ON

  • Set the Autothrottles to the ON position

13. ENG IGN OVRD SWITCH - OFF

  • Set the ENG IGN OVRD switch to the OFF position.

14. SEAT BELTS - AS REQUIRED

  • Set the seat belts as is required.

[END SEVERE TURBULENCE AND / OR HEAVY RAIN INGESTION CHECKLIST]

TAIL CONE UNLOCK

AIRCRAFT ON GROUND

IF MISC ALERTS ARE NO LONGER DISPLAYED, SKIP TO MISCELLANEOUS ALERTS AND SYSTEMS DISPLAY WILL OPERATE NORMALLY

1. CONTACT MAINTENANCE

  • Contact maintenance for aircraft repairs.

NOTE

Aircraft may be dispatched with this alert provided maintenance verifies that tailcone and number 2 engine service platform (patio) doors are locked in accordance with the MEL. The Level 1 alert “DOOR OPEN” will remain displayed until after engine start.

[END TAIL CONE UNLOCK CHECKLIST]

AIRCRAFT DISPLAYS BUFFETING OR CONTROL COLOUM PULSES

IF MISC ALERTS ARE NO LONGER DISPLAYED, SKIP TO MISCELLANEOUS ALERTS AND SYSTEMS DISPLAY WILL OPERATE NORMALLY

Reduce airspeed to low cruise and make log entry.

[END TAIL CONE UNLOCK CHECKLIST]

Continue normal operations and speed.

Make log entry.

[END TAIL CONE UNLOCK CHECKLIST]

VOLCANIC ASH

If a volcanic ash cloud is inadvertently entered during flight, depart the area by the shortest route possible. Consider a descending 180 degree turn.

Do not use windshield wipers.

CAUTION

If airspeed indications are abnormal, refer to Emergency Non-Alert procedure - AIRSPEED: LOST, SUSPECT OR ERRATIC for pitch guidance information.

Perform the following actions as rapidly as possible:

1. AUTOTHROTTLES - DISENGAGE

  • Disengage the autothrottles.

2. THROTTLES (ALL) - IDLE

  • Set all the throttles IDLE.

3. ENG IGN OVRD SWITCH - OVRD ON

  • Move the ENG IGN OVRD switch to the OVRD ON position.

4. ECON SWITCH - OFF

  • Set the ECON switch to the OFF position.

5. ANTI-ICE SYSTEM MANUAL SWITCH - MANUAL

  • Set the ANTI-ICE MANUAL switch MANUAL

6. ENG ANTI-ICE SWITCHES - ON

  • Set the ENG ANTI-ICE switches ON

7. WING AND TAIL ANTI-ICE SWITCHES - ON

  • Set WING and TAIL ANTI-ICE switches to the ON position.

8. TRANSPONDER - 7700

  • Set the transponder to 7700

9. EXTERIOR LIGHTS - ON

  • Set the exterior lights to the ON position.

ENGINE(S) FLAMED OUT OR STALLED OR EGT BEYOND LIMITS OR INCREASING RAPIDLY TOWARD LIMITS

IF ENGINE(S) ARE / IS NOT FLAMED OUT OR STALLED OR EGT BEYOND LIMITS OR INCREASING RAPIDLY TOWARD LIMITS, SKIP TO WHEN CLEAR OF VOLCANIC ASH CLOUD AND ENGINE(S) RESTARTED

10. FUEL SWITCH (AFFECTED ENGINE[S]) - OFF

  • Set the fuel switch of the affected engine(s) to the OFF position.

Time and conditions permitting, leave fuel switch in the OFF position for 15 to 30 seconds to allow engine to cool.

NOTE

Allowing engine hot section to cool before restart may enhance shedding of accreted molten volcanic ash material from Nozzle Guide Vanes.

11. FUEL SWITCH (AFFECTED ENGINE[S]) - ON

  • Set the fuel switch of the affected engine(s) to the ON position.

N2 RPM LESS THAN 15%

IF N2 RPM IS MORE THAN 15%

12. ENG START SWITCH - PULL

  • PULL the ENG START switch.

Monitor start.

NOTES

Engines accelerate to idle very slowly at high altitudes. This may be incorrectly interpreted as a hung start or an engine malfunction not caused by volcanic ash.* If an engine fails to start, repeated attempts should be made immediately. A successful start may not be possible until clear of volcanic ash cloud and airspeed and altitude are within the normal range.*

Wait until clear of volcanic ash cloud and engine(s) restarted

  • Avoid rapid throttle movement. Maximum thrust may not be available.
  • Do not use windshield wipers.
  • Consider an autoland when forward vision is impaired.

13. LAND AT NEAREST SUITABLE AIRPORT

  • Landing at the nearest suitable airport for aircraft repair.

REFERENCES

[END VOLCANIC ASH CHECKLIST]

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