Memory Items Flashcards
IN-FLIGHT FIRE OR SEVERE MECHANICAL DAMAGE
PL affected side………………………………………………………..FI
CL affected side…………………………….FTR then FUEL SO
FIRE HANDLE affected side………………………………..PULL
•if condition persist after 10 seconds
AGENT 1 affected side……………………………………DISCH
♦if condition persist after 30 seconds
AGENT 2 affected side…………………………………..DISCH
ON GROUND FIRE
OR SEVERE MECHANICAL DAMAGE
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 persist
AGENT 1 affected side………………………………….DISCH
♦if condition persist after 30 seconds
AGENT 2 affected ide…………………………………..DISCH
ENG FIRE AT TAKE OFF
•When airborne
LDG GEAR ……………………………………………………………UP
•At acceleration altitude
PWR MGT ………………………………………………………….MCT
•AT VFTO
♦If normal conditionsFLAPS …………………………………………………………………..0°
♦If icing conditions
FLAPS ………………………………………………MAINTAIN 15°
PL affected side ……………………………………………………FI
CL affected side ……………………..FTR THEN FUEL SO
FIRE HANDLE Illuminated …………………………………Pull
♦If fire persist after 10 seconds
AGENT 1 affected side ………………………………..DISCH
♦If fire persist 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 immediate relight)
CL 1 + 2 ……………………………………….FTR THEN FUEL SO
ENGINE FLAME OUT AT TAKEOFF
UPTRIM …………………………………………………………..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 acceleration altitude
ALT ……………………………………………………………………..SET
•AT VFTO
PWR 1 + 2 ………………………………………..IN THE NOTCH
PWR MGT …………………………………………………………MCT
IAS ……………………………………………………………………..SET
♦If normal conditions
FLAPS ……………………………………………………………………0°
♦If icing conditions
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 ………………………………………………………………..ON
CREW COMMUNICATIONS ………………………ESTABLISH
RECIRC FANS 1 + 2 ………………………………………………..OFF
AP …………………………………………………………………………….ON
DUAL DC GEN LOSS
DC GEN 1 + 2 …………………………………………..OFF then ON
♦If no generator recovered
HYD GREEN PUMP ………………………………………………OFF
TRU …………………………………………………………………………ON
EMERGENCY DESCENT
OXYGEN MASKS/CREW COMMUNICATIONS ……………….AS REQ
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
ADNORMAL 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 BARS …………………………………..OFF/OFF/STBY
PITCH AND TQ ……………………………………………..MAINTAIN
♦If take off or GA below 1500 ft
PITCH IMMEDIATELY ………………………………………………….8°
ICING VOLCANIC ASHES CONDITIONS ………..ESCAPE
ABNORMAL PARAMETERS DURING START
♦If ITT trends to exceed 900°C, or no ITT, or no NH
CL affected side ……………………………………………FUEL SO
ENG START ROTARY SELECTOR …………OFF / START ABORT
ENGINE LOOP FAULT
LOOP AFFECTED ……………………………………………………OFF
ENGINE FLAME-OUT
PL affected side ………………………………………………………….FI
♦If NH drops below 30% (no immediate relight)
CL affected side …………………………FTR THEN FUEL SO
PEC FAULT
If in short final approach (below 400 ft RA)
GO AROUND PROCEDURE (2.02.10 P36) …………APPLY