Memo Itens Flashcards

1
Q

ENG 1 (2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT

A

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

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2
Q

ENG 1 (2) FIRE OR SEVERE MECHANICAL DAMAGE ON GROUND

A

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

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3
Q

ENG 1 (2) FIRE AT TAKE OFF

A

When airborne
LDG GEAR……………..UP

At Acceleration Altitude
PWR MGT……………..MCT

At VFTO
    If normal condition
        FLAPS............0
    If icing condition
        FLAPS............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
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4
Q

BOTH ENGINE S FLAME OUT

A

PL 1 + 2………….FI
If NH drops below 30% ( no automatic relight)
CL 1 + 2……FTR THEN FUEL SO

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5
Q

ENG 1(2) FLAME OUT AT TAKE OFF

A

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 Acceleration Altitude
ALT.........................SET
    At VFTO
    PL 1 + 2..................IN THE NOTCH
    POWER MGT.........MCT
    IAS  -  SET
        If normal condition
        SPD TGT...........CHECK VFTO
        FLAPS..............0
        If ice 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
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6
Q

SMOKE

A

CREW OXY MASKS………………..ON / 100%
GOGGLES……………………………..SET
CREW COMMUNICATIONS……..ESTABLISH
RECIRC FANS 1 + 2…………………OFF
AP…………………………………………ON

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7
Q

DUAL DC GEN LOSS

A

PF……………………………………CAPT
DC GEN 1 + 2……………………OFF THEN ON
If no generator recovered
HYD GREEN PUMP…………………OFF
TRU………………………………………ON

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8
Q

EMERGENCY DESCENT

A

OXYGEN MASKS / CREW COMMUNICATION…………..AS RQD
GOGGLES…………………………………………………………….AS RQD
DESCENT……………………………………………………………..INITIATE
PL 1 + 2…………………………………………………………………FI
CL 1 + 2…………………………………………………………………100% OVRD

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9
Q

SEVERE ICING

A

MINIMUM ICING SPEED…………………INCREASE by 10 kt
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

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10
Q

RECOVERY AFTER STALL or ABNORMAL ROLL CONTROL

A

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
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11
Q

UNRELIABLE AIRSPEED INDICATION

A

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 CONDITIONS………………….ESCAPE

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12
Q

ABNORMAL PARAMETERS DURING START

A

If ITT tends to exceed 900C, or no ITT, or no NH
CL affected side…………………………………..FUEL SO
ENG START ROTARY SELECTOR…………..OFF / START ABORT

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13
Q

FIRE LOOP 1A (2B) (2A) (2B) FAULT

A

LOOP affected…………………………………….OFF

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14
Q

ENG 1 (2) FLAME OUT IN FLIGHT

A

PL affected side………………………………………..FI

If NH drops below 30% (no immediate relight)
CL affected side…………………………………….FTR THEN FUEL SO

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15
Q

PEC 1 (2) FAULT

A

If below 400 ft

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

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16
Q

LO PITCH IN FLIGHT

A

PL affected side………………………………………..FI
CL affected side………………………………………..FTR THEN FUEL SO

17
Q

FLAPS UNLK

A

If before V1
TAKE OFF………………………………FI

If after V1
VR, V2………………………..SPEED BUGS AUTOMATICALLY INCREASED

If FLAPS UNLK during approach
GO AROUND procedure…………………………………..APPLY
VGA…………………………………………………….NOT LESS THAN Vmin OPS

18
Q

PITCH DISCONNECT

A

FREE COLUMN(S)………………………………………IDENTIFY
PF………………………………………….FREE CONTROL COLUMN SIDE
IAS……………………………………………………………180 kt MAX

19
Q

ELEVATOR JAM

A

CONTROL COLUMNS………………………………………..UNCOUPLE
FREE COLUMN………………………………………………….IDENTIFY
IAS MAX……………………………………………………………180 KT

20
Q

ENTERING ICING CONDITIONS

A

MINIMUM MANEUVER / OPERATING ICING SPEEDS…………………………………OBSERVED

21
Q

AT FIRST VISUAL INDICATION OF ICE ACCRETION AND AS LONG AS ICING CONDITIONS EXIST

A

MINIMUM MANEUVER / OPERATING ICING SPEEDS………………………………..OBSERVED