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22 Cards in this Set

  • Front
  • Back

ENG 1/2 FIRE OR SEVERE MECHANICAL DMG IN FLT

PL affected side --- FI


CL affected side --- FTR then FUEL SO


▪ If condition persists after 10 secs


AGENT 1 affected side --- DISCH




▪ If condition persists after 30 secs


AGENT 2 affected side --- DISCH



ENG 1/2 FIRE OR SEVERE MECHANICAL DMG ON GND

PL 1+2 --- GI / REVERSE AS RQD

• When A/C stopped

PARKING BREAK --- ENGAGE


CL 1+2 --- FTR THEN FUEL SO


▪ If condition persists


AGENT 1 affected side --- DISCH


▪ If condition persists after 30 secs


AGENT 2 affected side --- DISCH

ENG 1/2 FIRE AT TAKE OFF

• When airborne


LDG GEAR --- UP


• At Acceleration Alt


PWR MGT --- MCT


• At Vfto


▪ If normal condition


FLAPS --- 0°


▪ If icing condition


FLAPS --- MAINTAIN 15°


PL affected side --- FI


CL affected side --- FTR


FIRE HANDLE illuminated --- PULL


▪ If condition persists after 10 secs


AGENT 1 affected side --- DISCH


▪ If condition persists after 30 secs


AGENT 2 affected side --- DISCH


BLEED engine alive ---- OFF if necessary

BOTH ENG 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

UPTRIM --- CHECK


AUTO FTR --- 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


PL 1+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 15°


FLAPS --- MAINTAIN 15°




PL affected side --- FI


CL affected side --- FTR then FUEL SO


BLEED engine alive --- OFF if necessary

SMOKE

CREW OXY MASKS --- ON / 100%


GOGGLES --- SET


CREW COMMUNICATIONS --- ESTABLISH


RECIRC FANS 1+2 --- OFF


AP --- ON

DUAL DC GEN LOSS

PF --- CAPT


DC GEN 1+2 --- OFF then ON


▪ If no generator recovered


HYD GREEN PUMP --- OFF


TRU --- ON

EMERGENCY DESCENT

OXYGEN MASKS / CREW COMMS --- AS RQD


GOGGLES --- AS RQD


DESCENT --- INITIATE


PL --- FI


CL --- 100% OVRD

SEVERE ICING

MINIMUM ICING SPEED --- INCREASE by 10kt


PWR MGT --- MCT


CL 1+2 --- 100% OVRD


PL 1+2 --- NOTCH


AP (if engaged) --- FIRMLY HOLD CONTRL


and DISENGAGE


SEVERE ICING CONDITIONS --- ESCAPE


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

AP/YD/FD --- OFF/OFF/STBY


PITCH AND TQ --- MAINTAIN


▪ If at take off or GA below 1,500 ft


PITCH IMMEDIATELY --- 8°




ICING / VOLCANIC ASH 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 ROTERY SLTR --- OFF / START ABRT

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

PL affected side --- FI


CL affected side --- FTR then FUEL SO

FLAPS UNLK

▪If before V1


TAKE OFF --- ABORT


▪If after V1


V2, VR --- SPEED BUGS AUTOMATIC INCREASED


▪If FLAPS UNLK during approach


GO AROUND procedure --- APPLY


VGA --- NOT LESS THAN Vmin OPS

PITCH DISCONNECT

FREE COLUMN --- IDENTIFY


PF --- FREE CONTROL COLUMN SIDE


IAS --- 180 kt MAX

ELEVATOR JAM

CONTROL COLUMNS --- UNCOUPLE


FREE COLUMN --- IDENTIFY


IAS MAX --- 180

VOLCANIC ASH ENCOUNTER

ITEMS HAVE TO BE APPLIED WHILE MAKING A 180° TURN AND STARTING DESCENT (IF MSA PERMITS)

ENTERING ICING CONDITIONS

ANTI-ICING (PROP-HORNS-SIDE WINDOWS) - ON


ANTI-\DE-ICING MODE SEL --- AUTO


MINIMUM MANEUVER/


OPERATING ICING SPEEDS --- OBSERVED


ICE ACCRETION --- MONITOR IEP

AT FIRST VISUAL INDICATION OF ICE ACCRETION AND AS LONG AS ICING CONDITION EXIST

ANTI-ICING (PROP-HORNS-SIDE WINDOWS)


--- CONFIRM ON


ANTI-\DE-ICING MODE SEL --- CONFIRM AUTO


ENG DE-ICING --- ON


AIRFRAME DE-ICING --- ON


MINIMUM MANEUVER/OPERATING ICING SPEEDS --- OBSERVED