MEMO ITEMS Flashcards
DC GEN 1+2 FAULT
PF —————— CPT
DC GEN1 ——– RESET
DC GEN2 ——– RESET
If one generator recovered
DC GGEN 1(2) FAULT procedure (A24.15) —– APPLY
If no generator recovered
HYD GEREEN PUMP —– OFF
TRU ————————— ON
If no TRU arrow light
MAX IMC FLIGHT TIME : 30min
TRU ————————- OFF
LAND ASAP
SMOKE
If smoke / fumes in the cockpit
CREW OXI MASKS ————— DON / 100%
GOGGLES ————————– SET
CREW COMMUNICATIONS — ESTABLISH
RECIRCULATION FANS 1+2 —– OFF
AP ————————————– ON
ENG 1(2) FIRE AT TAKEOFF
When airbone
LDG GEAR —- UP
At acceleration altitude
PWR MGT — MCT
At VFTO
If normal conditions
FLAPS —- 0
If icing conditions
FLAPS —- MANTAIN 15
PL (affected side ENG) —– FI
CL (affected side ENG) —– FTR THEN FUEL S.O.
FIRE HANDLE (red light on) —– PULL
If fire lersists after 10s
AGENT 1 (affected side ENG) —– DISCH
If fire lersists after 30s
AGENT 2 (affected side ENG) —– DISCH
ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT
PL (affected ENG) —– FI
CL (affected ENG) —– FTR THEN FUEL S.O
FIRE HANDLE (affected ENG) —– PULL
If fire persists after 10s
AGENT 1 (affected ENG) —– DISCH
If fire persists after 30S
AGENT 2 (affected ENG) —– DISCH
ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE ONGROUND
AIRCRAFT —– STOP
BRAKE HANDLE —– PARKING
CL 1+2 —– FTR THEN FUEL S.O.
FIRE HANDLE (affected ENG) —– PULL
If fire persists
AGENT 1 (affected ENG) —– DISCH
If fire persists after 30s
AGENT 2 (affected ENG) —– DISCH
ENG 1(2) FLAME OUT AT TAKEOFF
▶ AUTOFEATHER…………………………………………………………………….CHECK
▶ UPTRIM………………………………..………………………………………CHECK
■ If no UPTRIM
▶ PL 1 + 2………………………………………………….ADVANCE TO THE RAMP
● WHEN AIRBORNE
▶ LDG GEAR……………………………………………………………….UP
■ If NO BLEEDS 1 + 2 FAULT
▶ BLEEDS 1 + 2……………………………………………………………..OFF
● AT ACCELERATION ALTITUDE
▶ ALT MODE……………………………………………………………SET
● AT VFTO
▶ PL 1 + 2………………………………………………………………….IN THE NOTCH
▶ PWR MGT ………………………………….. ……………………………………. MCT
■ If normal conditions
▶ FLAPS…………………………………………………………………………..0°
▶ SPD TGT …………………………………………………………….CHECK VFTO
■ If icing conditions
▶ FLAPS : MAINTAIN 15°
▶ SPD TGT ……………………………………..CHECK VFTO ICING FLAPS 15°
▶ IAS MODE……………………………………………………………………………SET
▶ PL (affected eng)……………………………………………………………………. FI
▶ CL (affected eng)……………………..……………………. FTR THEN FUEL S.O
ENG 1+ 2 FLAME OUT
▶ PF ……………………………………………………………………………………….CAPT
▶ PL 1 + 2………………………………………….……………………………………….. FI
■ If NH drops below 30 %
▶ CL 1 + 2 ………………………………………………………. FTR THEN FUEL S.O.
▶ OPTIMUM SPEED……………………………….………………………………VmHB
SEVERE ICING
▶ IAS : ICING BUG + 30 kt (or ICING BUG IF FLAPS 15 EXTENDED)
▶ PWR MGT ……………………………………………………………………………… MCT
▶ PL 1+2………………………………………………………………………………..ADJUST
▶ CL 1+2………………………………………………………………………… 100 % OVRD
STALL
CONTROL COLUM —– PUSH
ENGINE POWER ——– INCREASE
If flaps 0
FLAPS ——————— EXTEND TO 15
BANK ——————— WINGS LEVEL
STALL
▶CONTROL COLUMN………………………………………………………………..PUSH
▶ENG PWR ……………………………………………………………………….INCREASE
■If FLAPS 0
▶FLAPS……………………………………………………………………EXTEND TO 15 ▶BANK…………………………………………………………………………WINGS LEVEL
UNRELIABLE AIRSPEED INDICATION
▶AP/YD ……………………………………………………………………………………OFF ▶FD ………………………………………………………………………………………. STBY
▶PITCH : MAINTAIN
▶TQ : MAINTAIN
■If at takeoff or GA below 1 500 ft
▶PITCH……………………………………………………………….. 8 ° IMMEDIATELY
▶ICING CONDITIONS………………………………………………………………ESCAPE
▶VOLCANIC ASHES CONDITIONS…………………………………………….ESCAPE
EMERGENCY DESCENT
▶ CREW OXY MASKS……………………….AS RQRD
▶ CREW COMMUNICATIONS…………..AS RQRD
▶ GOGGLES……………………………………AS RQRD
▶ DESCENT…………………………………….INITIATE
▶ PL 1+2……………………………………….. FI
▶ CL 1+2…………………………………………100% OVRD
PITCH CONTROL JAM AT TAKEOFF OR LANDING
▶ MAX IAS : 180 kt
▶ CONTROL COLUMNS..UNCOUPLE
▶ FREE CTRL COLUMN…….IDENTIFY
▶ PF……….FREE CTRL COLUMN SIDE
FLAPS UNLK
●Before V1
▶TAKEOFF………………………….ABORT
●After V1
VR & V2 SPEED BUGS AUTOMATICALLY INCREASED
●If FLAPS UNLK during approach
▶GO-AROUND……………….PERFORM
▶VGA ..NOT LESS THAN Vmin OPS
PITCH DISCONNECT
▶FREE CONTROL COLUMN(S)………………………………………………..IDENTIFY
▶PF ……………………………………………………FREE CONTROL COLUMN SIDE
▶MAX IAS : 180 kt
