MEMO ITENS Flashcards
ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT
PL affected side ………………………. FI
CL affected side .FTR THEN FUEL SO
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
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 seconds
AGENT 2 affected side ………….. DISCH
ENG 1(2) FIRE AT TAKE OFF
- When airborne
LDG GEAR …………………………………… UP - At Acceleration Altitude
PWR MGT …………………………………. MCT - At VFTO
[] If normal condition FLAPS …… 0*
[] If icing condition. MAINTAIN 15*
PL affected side …………………………… FI
CL affected side …. FTR THEN FUEL SO
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
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
UP TRIM ………………………………. CHECK
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 Accelaration 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 FLAPS 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 COMUNICATIONS … 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
OXY MASKS/CREW COMUN … AS RQD
GOGGLES …………………………… AS RQD
DESCENT ………………………….. INITIATE
PL 1 + 2 ……………………………………….. FI
CL 1 + 2 ……………………….. 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 control wheel
and DISENGAGE
SEVERE ICING CONDITIONS… ESCAPE
ATC ………………………………………NOTIFY
RECOVERY AFTER STALL or
ABNORMAL ROLL CONTROLL
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 1500 ft
PITCH IMMEDIATELY ……………… 8*
ICING/VOLCANIC ASHES cond .. 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 side ………………… 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
VR, V2……SPD BUGS AUTOMATICALY INCREASE
[] If FLAPS UNLK during approach
GO AROUND procedure …………………….. APPLY
VGA ………………….. NOT LESS THAN Vmin OPS
PITCH DISCONNECT
FREE COLUMN(S) ……………………. IDENTIFY
PF ………….. FREE CONTROL COLUMN SIDE
IAS ………………………………………. 180 kt MAX
ELEVATOR JAM
CONTROL COLUMNS …………… UNCOUPLE
FREE COLUMN ………………………… IDENTIFY
IAS MAX ………………………………………. 180 kt
ENTERING INCING CONDITIONS
or
AT FIRST VISUAL INDICATION OF ICE ACCREATION AND AS LONG AS ICING CONDITIONS EXIST
MINIMUM Maneuver/Operating ICING SPEEDS ………………. OBSERVED