QRH Memory Items Flashcards

1
Q

L (R) ENG FIRE

A

1- *POWER LEVER ………………………………………………….. FLT IDLE
2- *CONDITION LEVER ……………………………………………. FUEL OFF
- Retard CL without delay.
3- *FIRE HANDLE ………………………………………………………….. PULL
4- *FIRE EXTG switch …………………………………………………………ON
- If fire indication still ON after 30 seconds, discharge FIRE EXTG

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2
Q

AIR CONDITIONING SMOKE

A

1- *OXYGEN MASKS and REGULATORS …………….. ON and 100%
2- *SMOKE GOGGLES ………………………………………………………. ON
3- *COMMUNICATION ………………………………………….. ESTABLISH

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3
Q

AVIONIC SMOKE or ELECTRICAL
SMOKE or FIRE

A

1- *OXYGEN MASKS and REGULATORS ………………. ON and 100%
2- *SMOKE GOGGLES …………………………………………………………. ON
3- *COMMUNICATION …………………………………………….. ESTABLISH

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4
Q

L (R) TAIL P HOT

A

1- *POWER …………………………………………………………. REDUCE TO 20 – 30%

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5
Q

CARGO SMOKE

A

1- *CARGO FIRE EXTG 1 switch ……………………………………………………… ON

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6
Q

RAPID DEPRESSURISATION /
EMERGENCY DESCENT

A

1- *OXYGEN MASKS and REGULATORS …………….. ON and 100%
2- *COMMUNICATION ………………………………………….. ESTABLISH

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7
Q

BOTH ENGINES FLAME OUT

A

1- *POWER LEVERS (both) …………………………………………………. FLT IDLE
2- *CONDITION LEVERS (both) ………………………………………….. FUEL OFF
3- *AIRSPEED……………………………………………………………………… 130 KIAS
4- *BAT switches (both) …………………………………………………………… OVRD
5- *FUEL STBY PUMP switches (both) ……………………………………… OVRD
6- *AUTO-COARSEN ………………………………………………………………….. OFF
7- *LEFT CONDITION LEVER …………………………………………………… START
8- *START switch ……………………………………………………………………………..L

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8
Q

ENGINE FAILURE

A

1- *POWER LEVER ……………………………………………… FLT IDLE
2- *CONDITION LEVER ………………………………………… FUEL OFF
- Retard CL without delay.

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9
Q

ELEVATOR SYSTEM JAMMED

A

1- *AUTOPILOT……………………………………………….. DISENGAGE
-Be prepared for trim transients.
2- *INTERCONNECT UNIT ……………………………… OVERPOWER
-Both pilots shall act on the controls. The pilot on the side NOT failed can, by
overpowering the interconnect unit, control the aircraft.
3- *PITCH DISCONNECT HANDLE …………………………….. PULL
-The pilot on the side NOT failed can control the aircraft.

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10
Q

AILERON SYSTEM JAMMED

A

1- *AUTOPILOT………………………………………………… DISENGAGE
2- *INTERCONNECT UNIT ……………………………….. OVERPOWER
- Both pilots shall act on the controls. The pilot on the side NOT jammed can, by
overpowering the interconnect unit or the aileron centering springs, control the aircraft.
3- *ROLL DISCONNECT HANDLE ………………………………… PULL
-The pilot on the side NOT jammed can control the aircraft.

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11
Q

LOSS OF BOTH GENERATORS
(Both engines running)

A

1- *BUS TIE switch …………………………………………………………………… SPLIT
2- *LEFT GEN switch …………………………………………….. RESET then ON
-Maximum two reset attempts.
3- *RIGHT GEN switch ………………………………………….. RESET then ON
- Maximum two reset attempts.

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12
Q

EMERGENCY EVACUATION

A

CAPTAIN or LP:
1- *Parking Brake ……………………………………………………………. SET
2- *&laquo_space;EVACUATION&raquo_space; ……………………………………………… ORDER
3- *Tower / Ground Crew ……………………………………………. NOTIFY
4- * BAT switches (Both)………………………………………………….. OFF
FIRST OFFICER or RP:
1- *Condition Levers (Both) …………………………………….. FUEL OFF
2- *EMERGENCY Panel Switches (All) ………………………………… ON
3- *Fire Handles (Both) ………………………………………………….. PULL
4- *FIRE EXTG switches (Both) ………………………………………….. ON

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13
Q

FLAP FAULT or FLAPS LIGHT ON

A

FLAPS SPLIT
1- *The split may be reduced by reselecting previous flap setting

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14
Q

HYDR LIGHT ON

A

1- *HYDR PUMP switch ……………………………………………………………… OFF
2- *Check HYDRAULIC INDICATORS.
EMER and MAIN pressure are BOTH LOW
CAUTION
Leave Flaps in their present position
SPEED BELOW 200 KIAS
3- *LANDING GEAR handle ……………………………………………………. DOWN
4- *EMER LDG handle …………………………………………………………….. PULL

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15
Q

HYDRAULIC FLUID LOSS

A

1- HYDR PUMP switch …………………………………………………… OFF

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16
Q

NO LIGHT UP, START SEQUENCE
INTERRUPTED, HUNG START, HOT
START

A

1- *CONDITION LEVER ……………………………………………………. FUEL OFF
2- *IGN switch ……………………………………………………………………………OFF
3- *MOTOR ENGINE to ITT below 175° C or for minimum 10 seconds,
but not more than 30 seconds.

17
Q

ENGINE SHUT DOWN

A

1- *POWER LEVER (affected engine) ………………………… FLT IDLE
2- *CONDITION LEVER (affected engine) ………………… FUEL OFF
- Retard CONDITION LEVER without delay.

18
Q

COMPRESSOR STALL

A

1- *CTOT ………………………………………………………………………. OFF
- Turn CTOT knob gently counter clockwise then select CTOT switch OFF
2- *POWER LEVER (affected engine) ……………… REDUCE to 20 – 30%
- Retard power lever slowly.

19
Q

UNCOMMANDED ENGINE
OPERATION

A

IN FLIGHT
1- *POWER …………………………………………………………. REDUCE (Set 20 – 30%)
- If TRQ indication is lost or unreliable, set POWER LEVER approx. ½
inch above FLT IDLE.
CAUTION
Keeping Condition Lever in T/M position will cause a small amount of
fuel to be vented overboard. Make sure that the Condition Lever is
positively returned into Min-Max range and does not remain above Max
gate.
2- *CONDITION LEVER ……………………………………………………….. T/M then SET
3- *AUTO-COARSEN …………………………………………………………………………. OFF

20
Q

UNRELIABLE SPEED AND / OR
ALTITUDE INDICATIONS

A

1- *AUTOPILOT………………………………………………….. DISENGAGE
2- *FLIGHT PATH ………………………………………………….. STABILIZE
3- *POWER SETTING ……………………………………………. TAKE-OFF