INFLIGHT ENG FIRE

OR SEVERE MECHANICAL DAMAGE

PL affected side......................................FI

CL affected side..............FTR THEN FUEL SO

FIRE HANDEL affected side...................PULL

If conditions persist after 10 seconds

FIRST AGENT affected side................DISCH

If conditions persist after 30 seconds

SECOND AGENT affected side............DISCH

ON GROUND ENG 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

     FIRST AGENT affected side........................DISCH

   If condition persist after 30 seconds

     SECOND AGENT affected side....................DISCH

When airborne

    LDG GEAR.................................................UP

At Acceleration Altitude

    PWR MGT...............................................MCT

At VFTO

    If normal condition

        FLAPS...................................................0^o

    If icing condition

        FLAPS..................................MAINTAIN 15^o

    PL affected side..........................................FI

    CL affected side..................FTR THEN FUEL SO

    FIRE HANDLE illuminated.........................PULL

    If fire persist after 10 seconds

       FIRST AGENT affected side.................DISCH

    If fire persist after 30 seconds

       SECOND AGENT affected side.............DISCH

    BLEED engine alive.................OFF if necessary

PL 1+2...................................................................FI

IF NH drops below 30%(no automatic relight)

    CL 1+2.......................................FTR THEN FUEL SO

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

    PL 1+2....................................IN THE NOTCH

    PWR MGT...............................................MCT

    IAS........................................................SET

    If normal condition

        FLAPS...................................................0^o

    If icing condition

        FLAPS..................................MAINTAIN 15^o

    PL affected side..........................................FI

    CL affected side..................FTR THEN FUEL SO

    BLEED engine alive.................OFF if necessary

CREW OXY MASKS...............................ON/100%

GOGGLES..............................................AS RQD

CREW COMMUNICATIONS...................ESTABLISH

RECIRC FANS 1+2........................................OFF

AP...............................................................ON

DC GEN 1+2.......................................OFF then ON

If no generator recovered

    HYD GREEN PUMP........................................OFF

    TRU............................................................ON

OXYGEN MASKS/CREW COMUNICATIONS.............AS RQD

GOOGLES.........................................................AS RQD

DESCENT........................................................INITIATE

PL 1+2.....................................................................FI

CL 1+2......................................................100% OVRD

MINIMUM ICING SPEED.......INCREASE RED BUG BY 10 KT

PWR MGT..............................................................MCT

CL/PL..........................................................100%/MCT

AP(if engaged)..........FIRMLY HOLD CONTROL WHEEL AND DISANGAGE

SEVERE ICING CONDITIONS...............................ESCAPE

ATC.................................................................NOTIFY

RECOVERY AFTER STALL

OR ABNORMAL ROLL CONTROL

CONTROL WHEEL......................................PUSH FIRMLY

If flaps 0^oconfiguration

FLAPS....................................................................15^o

PWR MGT..............................................................MCT

CL/PL..........................................................100%/MCT

ATC.................................................................NOTIFY

If flaps extended

PWR MGT..............................................................MCT

CL/PL..........................................................100%/MCT

ATC.................................................................NOTIFY

AP/YD/FD BARS......................................OFF/OFF/STBY

PICTH AND TQ.............................................MAINTAIN

If at take off or GA below 1500 ft:

    PICTH IMMEDIATELY............................................8^o

ICING/VOLCANIC ASHES CONDITIONS...............ESCAPE

If ITT tends to exceed 900^oc, or no ITT, or no NH

    CL affected side............................................FUEL SO

    ENG START ROTARY SELECTOR........OFF/START ABORT

LOOP affected......................................................OFF

PL affected side......................................................FI

If NH drops below 30%(no immediate relight)

    CL affected side..........................FTR THEN FUEL SO

If in short final approach (below 400 ft RA)

   GO AROUND procedure....................................APPLY

PL affected side.........................................................FI

CL affected side.................................FTR THEN FUEL SO

If before V1

   TAKE OFF.....................................................ABORT

IF after V1

   VR, V2.......................................INCREASE BY 10 KT

If alarm occurs during approach

   GO AROUND procedure...................................APPLY

   VGA..........................................INCREASE BY 10 KT

CONTROL COLUMNS....................................UNCOUPLE

If ROL, PIT, ATT, HDG cautions appears on EFIS

    BOTH EADI, STBY HORIZON...................CROSSCHECK

    WRONG INSTRUMENT................................INDENTIFY

    ATT/HDG PB affected side.............................DEPRESS