Emergencies (800XP) Flashcards

1
Q

Aborted Takeoff

A

Thrust Levers ……………………………………….CLOSE
Brakes ……………………………………………APPLY
Airbrakes …………………………………………DEPLOY
Thrust Reversers ……………………………………DEPLOY

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2
Q

Engine Failure Above V1

A

At Positive Rate of Climb:
LANDING GEAR Lever …………………………………..UP
MAIN AIR VLVs ……………………………………..CLOSE
F/DK VLV ………………………………………….CLOSE

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3
Q

Double Engine Failure

A

ENG IGNITION 1 and 2 …………………………………..ON
Thrust Levers …………………………………….. CLOSE
Crew Oxygen …………………. DON MASKS IF ABOVE 15,000 FT

NOTE: Headsets and hats must be removed before donning oxygen mask.

Mic Selector ……………………….. MASK IF ABOVE 15,000 FT
Engine Indications ……………………………….. MONITOR

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4
Q

Oil Low Pressure

*Illuminates to indicate oil pressure has dropped below 23 psi

A

Oil Pressure ………………………….CHECK GAUGE READING

If below 25 PSI:
HP Cock (affected engine) ....................................CLOSE
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5
Q

Engine Fire On Ground

A

START PWR Switch (starting only) ……………….PUSH FOR ABORT

HP Cock (affected engine) ………………………………CLOSE

LP Cock (affected engine) ………………………………CLOSE

ENG EXT (affected engine) …………………………….SHOT 1

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6
Q

Engine Fire Below V1

A

Thrust Levers ……………………………………….CLOSE
Brakes ……………………………………………APPLY
Air Brakes ………………………………………….OPEN
Thrust Reverser …………………………………….DEPLOY

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7
Q

Engine Fire Above V1

A

At Positive Rate of Climb:
LANDING GEAR Lever …………………………………..UP
MAIN AIR VLV …………………………………CLOSE BOTH
F/DK VLV ………………………………………….CLOSE

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8
Q

Engine Fire in Flight

A
Thrust Lever (affected engine) ................................CLOSE
If fire warning persists:
HP Cock (affected engine) ....................................CLOSE
LP Cock (affected engine) ....................................CLOSE
ENG EXT ................................................SHOT 1

If engine shutdown occurs during initial climb:
MAIN AIR VLVs 1 and 2. . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE
F/DK VLV ………………………………………….CLOSE

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9
Q

APU Fire (Honeywell GTCP 36-50 (W) APU )

*Over temperature is sensed.

A

STOP Switch ……………………………PUSH MOMENTARILY
MASTER Switch ………………………………………OFF
FIRE EXT Switch ………………………LIFT GUARD/SELECT ON

If fire warning persists:
4. APU FIRE WARN CB ………………………….PULL (DA-D, N6)

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10
Q

Inadvertent Thrust Reverser Deployment - Takeoff Aborted

A

Below V1 – Takeoff Aborted:
Thrust Levers ……………………………………….CLOSE
Brakes ……………………………………………APPLY
Air Brakes ………………………………………..DEPLOY
Thrust Reversers ……………………………………DEPLOY

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11
Q

Inadvertent Thrust Reverser Deployment - Takeoff Continued

A

After V1 – Takeoff Continued:
LANDING GEAR Lever …………..UP (when positive climb established)
MAIN AIR VLVs ………………………………..CLOSE BOTH
F/DK VLV ………………………………………….CLOSE

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12
Q

Inadvertent Thrust Reverser Deployment - In Flight

A

HP COCK (affected engine) …………………………….CLOSE

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13
Q

Depressurization

A

Crew Oxygen …………………………………DON MASKS

MIC Selector …………………………….MASK

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14
Q

Emergency Descent

A

Thrust Levers …………………………………….. CLOSE
Speed ………………………………………….. MMO/VMO(unless structural damage is suspected)
AIRBRAKE ……………………………………….. OPEN

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15
Q

Fuselage Fire or Smoke

A

Crew Oxygen …………………….. DON MASKS (100% EMERG)
MIC Selector ………………………………………. MASK
Smoke Goggles ……………………………… DON and VENT
Cabin Notices ………………………………………… ON

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16
Q

Smoke from A/C Ducts

A

Crew Oxygen …………………….. DON MASKS (100% EMERG)
MIC Selector ………………………………………. MASK
Smoke Goggles ……………………………… DON and VENT
Cabin Notices ………………………………………… ON

17
Q

High Pressure Air Overheat (HP AIR 1 OVHT)

*Indicates that HP bleed air between the associated main air valve and the fow control valve has reached or exceeded 290ºC (554ºF).

A

MAIN AIR VLV (affected engine) ……………………….. CLOSE
F/DK VLV ……………………………………….. CLOSE

18
Q

Rear Equipment Bay Overheat

Rear Bay OVHT

  • Indicates any of the six thermally operated switches has detected an overheat condition (100°C or 212°F)
A

Main Air VLVs 1 and 2 …………………………………….CLOSE
F/DK VLV …………………………………….OPEN FULLY

19
Q

Electrical Fire or Smoke

A

Crew Oxygen ……………………… DON MASKS/100% EMERG
MIC Selector ………………………………………..MASK
Smoke Goggles ……………………………… DON and VENT
Cabin Notices …………………………………………ON

20
Q

Battery Overheat (NiCad only)

BATT 1 OVHT
BATT 1 OVHT

• Indicates that the temperature of the associated battery is approximately 71ºC (160ºF).

A

In Flight: BATT ……………………………………………EMERG

On Ground: BATT ………………………………………………OFF

21
Q

Brake Failure

A

Brake Pedals ……………………………………..RELEASE
WHEEL BRAKE Lever ………………………………EMERGY
Brake Pedals ………………………………. APPLY GENTLY

Use one continuous application if possible

22
Q

Emergency Evacuation

A

Airplane ……………………………………………STOP
WHEEL BRAKE Lever ………………………………….PARK
HP Cocks ………………………………………….CLOSE
LP Cocks ………………………………………….CLOSE
EMERG LIGHTS (if required) ……………………………..MAN
PA …………………………………..ORDER EVACUATION
DUMP VALVE ……………………………………….OPEN
BATT ………………………………………………OFF