QRH Memory Items Flashcards
ENG 1 (2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT
(1). PL affected side ……….. FI.
(2). CL affected side ………. FTR THEN FUEL SO.
(3). FIRE HANDLE affected side……..PULL.
» If condition persists after 10 seconds, AGENT 1 affected side……. DISCH.
» If condition persists after 30 seconds, AGENT 2 affected side…….. DISCH
ENG 1 (2) FIRE OR SEVERE MECHANICAL DAMAGE ON GROUND
(1). PL 1 + 2………..GI / REVERSE AS RQD.
» When aircraft stopped,
**PARKING BRAKE …… ENGAGE.
**CL 1 + 2 ….. FTR THEN FUEL SO.
**FIRE HANDLE affected side……..PULL.
»If condition persists, AGENT 1 affected side……. DISCH.
»If condition persists after 30 second, AGENT 2 affected side……. DISCH.
EMER EVACUATION ON GROUND
(1). AIRCRAFT/PARKING BRAKE ……. STOP/ENGAGE.
(2). AUTO PRESS……… DUMP.
(3). ATC (VHF 1) ………. NOTIFY.
(4). CL 1 + 2 …….. FTR THEN FUEL SO.
(5). MIN CAB LIGHT…….ON.
(6). CABIN CREW (PA)………NOTIFY.
(7). FIRE HANDLES 1 + 2………..PULL.
(8). AGENTS ………DISCH AS RQD.
(9). ENG START ROTARY SELECTOR….OFF/START ABORT.
(10). FUEL PUMPS 1 + 2……OFF.
(11). EVACUATION (PA) …….INITIATE.
»Before leaving aircraft, BAT……..OFF.
ENG 1 (2) FIRE AT TAKE OFF
(1). When airborne, LDG GEAR………..UP.
(2). At Acceleration Altitude, PWR MGT……….MCT.
(3). At VFTO, If normal condition, FLAPS……….. 0°.
If icing condition, FLAPS……….MAINTAIN 15°.
(4). PL affected side…….. FI.
(5). CL affected side………. FTR THEN FUEL SO.
(6). FIRE HANDLE illuminated………PULL, If fire persists after 10 seconds, AGENT 1 affected side……DISCH.
If fire persists after 30 seconds, AGENT 2 affected side…….DISCH.
(7). BLEED engine alive………… OFF if necessary.
BOTH ENGINES FLAME OUT
PL 1+2………FI.
»If NH drops below 30% (no automatic relight),
CL 1+2…..FTR THEN FUEL SO.
ENG 1(2) FLAME OUT AT TAKE OFF
(1). UPTRIM……….CHECK.
(2). AUTOFEATHER…….CHECK.
»If no UPTRIM: PL 1+2…….. ADVANCE TO THE RAMP.
**When airborne: LDG GEAR…….UP, BLEED 1+2……OFF IF NOT FAULT.
»At Acceleration Altitude: ALT…….SET.
»At VFTO: PL1+2…..IN THE NOTCH, PWR MGT…..MCT,
IAS….SET.
**If normal condition: SPD TGT……CHECK VFTO, FLAPS……0°.
**If icing condition: SPD TGT…….CHECK VFTO ICING FLAPS 15°, FLAPS……..MAINTAIN 15°.
(3). PL affected side…….FI.
(4). CL affected side……..FTR THEN FUEL SO.
(5). BLEED engine alive…….OFF if necessary.
SMOKE
(1) . CREW OXY MASKS…….ON / 100%.
(2) . GOGGLES………SET.
(3) . CREW COMMUNICATIONS……….ESTABLISH.
(4) . RECIRC FANS 1+2………… OFF.
(5) . AP………ON.
DUAL DC GEN LOSS
(1). PF…….. CAPT.
(2). DC GEN 1+2………OFF then ON.
» If no generator recovered:
*HYD GREEN PUMP…..OFF,
*TRU……..ON.
EMERGENCY DESCENT
(1) . OXYGEN MASKS/CREW COMMUNICATIONs……AS RQD.
(2) . GOGGLES………..AS RQD.
(3) . DESCENT…………INITIATE.
(4) . PL 1+2…….FI.
(5) . CL 1+2…………100% OVRD.
SEVERE ICING
(1) . MINIMUM ICING SPEE………. INCREASE by 10 kt.
(2) . PWR MGT………….MCT.
(3) . CL 1+2…………100% OVRD.
(4) . PL 1+2………..NOTCH.
(5) . AP (if engaged)……..FIRMLY HOLD CONTROL WHEEL and DISENGAGE.
(6) . SEVERE ICING CONDITIONS………..ESCAPE.
(7) . ATC…………NOTIFY.
RECOVERY AFTER STALL
or ABNORMAL ROLL CONTROL
CONTROL WHEEL............ PUSH FIRMLY. >>If flaps 0° configuration: *FLAPS............. 15°. *PWR MGT.................MCT. *CL 1 + 2..............100% OVRD. *PL 1 + 2...............NOTCH. *ATC............NOTIFY. >>If flaps are extended: *PWR MGT...............MCT. *CL 1 + 2..........100% OVRD. *PL 1 + 2..............NOTCH. *ATC............NOTIFY.
UNRELIABLE AIRSPEED INDICATION
(1). AP/YD/FD……….OFF/OFF/STBY.
(2). PITCH AND TQ………….MAINTAIN.
»If at take off or GA below 1500 ft:
PITCH IMMEDIATELY……….8°.
(3). ICING / VOLCANIC ASHES CONDITIONS……ESCAPE.
ABNORMAL PARAMETERS
DURING START
If ITT tends to exceed 900°C, or no ITT, or no NH.
- *CL affected side …….FUEL SO.
- *ENG START ROTARY SELECTOR…..OFF / START ABORT.
FIRE LOOP 1A (1B) (2A) (2B) FAULT
LOOP affected…………………….. OFF
ENG 1 (2) FLAME OUT IN FLIGHT
PL affected side ……………FI.
»If NH drops below 30 % (no immediate relight).
CL affected side………..FTR THEN FUEL SO.
PEC 1(2) FAULT
If below 400 ft:
GO AROUND procedure ……APPLY.
LO PITCH IN FLIGHT
(1) . PL affected side……………… FI.
(2) . CL affected side…………….FTR THEN FUEL SO.
FLAPS UNLK
(1). If before V1, TAKE OFF …………..ABORT.
(2). If after V1, VR, V2……..SPEED BUGS AUTOMATICALLY INCREASED.
(3). If FLAPS UNLK during approach,
GO AROUND procedure …………APPLY,
VGA ………….NOT LESS THAN Vmin OPS.
PITCH DISCONNECT
(1) . FREE COLUMN(S) ………IDENTIFY.
(2) . PF ……..FREE CONTROL COLUMN SIDE.
(3) . IAS ………….180 kt MAX.
ELEVATOR JAM
(1) . CONTROL COLUMNS ……..UNCOUPLE.
(2) . FREE COLUMN…………IDENTIFY.
(3) . IAS MAX …………….180 KT.
