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 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 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 at TAKE OFF
*when airborne
LDG GEAR ————- UP
- at acceleration altitude
PWR MGT ————– MCT - at VFTO
- if normal condition
FLAP —————- 0 - if icing condition
FLAP —————- MAINTAIN 15
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 — DISCHBLEED ————————- OFF if necessary - if normal condition
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 up trim
PL 1+2 ---- ADVANCE TO THE RAMP
* when airbone
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 contition
SPD TGT --- CHECK VFTO
FLAPS --- 0
* if icing contition
SPD TGT --- CHECK VFTO ICING FLAP 15
FLAPS --- MAINTAIN 15 PL affected side --- FI
CL affected side --- FTR THEN FUEL SO
BLEED engine alive --- OFF if necessarySMOKE
CREW OXY MASKS ------------ ON / 100% GOOGLES ----------------------- 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 ---------------------- ONEmergency descent
OXYGEN MASKS / CREW COMMUNICATIONS --- AS RQD GOOGLES------------- AS RQD DESCENT ------------- INITIATE PL 1 + 2 --------------- FI CL 1 + 2 -------------- 100% OVRD
Severe ICING
MINIMUM ICING SPEED..INCREASE by 10
- PWR MGT …………………………………….MCT - CL1+2… ……………………………………… 100% OVRD
- PL1+2 ………………………………………… NOTCH
- AP (if engaged) …….. FIRMLY HOLD CONTROL WHEEL 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 --- NOTIFYUnreliable airspeed indication
AP/YD/FD — OFF/OFF/STBY
PITCH and TQ —————– MANTAIN
- If take off or GA below 1.500ft
PITCH IMMEDIATELY —– 8
ICING/VOLCANIC ASHES CONDITIONS — ESCAPE
Abnormal parameters during start
- If ITT tends do exceed 900, 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 400ft
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 --- Speed bugs automatically increased
* if FLAPS UNLK during approach
GO AROUND --- APPLY
VGA --- NOT less then Vmin OPSPitch disconnect
FREE COLUMN(S) — IDENTIFY
PF ——————— FREE CONTROL COLUMN SIDE
IAS ——————– 180kt MAX
Elevator JAM
CONTROL COLUMNS — UNCOUPLE
FREE COLUMN ———– IDENTIFY
IAS MAX ——————- 180kt
Entering ICING CONDITIONS
Minimum maneuver/operating icing speeds —– OBSERVED
At first visual indication of ice accretion and as long as icing conditions exist
Minimum maneuver/operating icing speeds —– OBSERVED
Leaving icing conditions
De-icing and anti-icing may be switched off
When the aircraft is visually verified clear of ice
Icing AOA caption may be cancelled and normal speeds may be used
