1/2 Flashcards

First part for AOI

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1
Q
Fire on the ground/ a/c departs prepared surface / emergency engine shutdown
1.
2.
3.
4.
5.
A
  1. PCL………………………………………………………..OFF
  2. Emergency firewall shutoff handle………PULL
  3. BAT, GEN, AUX BAT switchs…………………OFF
  4. Parking Brake………………………AS REQUIRED
  5. Emergency ground egress… AS REQUIRED
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2
Q
ABORT 
1.
2.
        Note
3,
A
  1. PCL……………………………….IDLE
  2. Wheel brakes……………..AS REQUIRED
    Note
    3, If fire present or departing prepared surface:
    CARRY OUT EMERGENCY ENGINE SHUTDOWN
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3
Q

EMERGENCY GROUND EGRESS

1. 
                      WARNING
If ejection seat pin cannot be properly inserted and                                                              
ground egress is essential, ejection may be required. 
Ensure canopy is closed/locked prior to ejection to
prevent seat from contacting frame.
2.
3.
4.
5.
6.
7.
8.
A
  1. ISS selector……………………………………………..SOLO
    WARNING
  2. Seat pin…………………………………….INSTALL (Both)
  3. Parachute riser releases…………RELEASE (both)
  4. Lap belt…………………………………….RELEASE (both)
  5. SSK fittings………………………DISCONNECT (Both)
  6. Leg lines…………………………………..RELEASE (both)
  7. Canopy………………….OPEN OR FRACTURE (both)
  8. ABANDON THE AIRCRAFT
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4
Q
Smoke or Fumes in the cockpit/ electrical fire
1.
2.
3.
4.
5.
If smoke severe:
6.
If smoke/fire persists:
7.
If smoke/fire ceases:
8.
9.
A

OBOGS…………………………………………………..MAX(both)
OBOGS pressure lever………..EMERGENCY (BOTH)
DESCEND BELOW 10,000 ft MSL….. INITIATE ( as required)
PRESSURIZATION switch……………………RAM/DUMP
BLEED AIR INFLOW switch……………………………OFF
if smokes severe:
FRACTURE CANOPY
if smoke/fire persists:
BAT,GEN,AUC BAT switches…………………………OFF
if smoke/fire ceases:
Essential electrics…………………………..RESTORE AS REQUIRED
LAND AS SOON AS POSSIBLE OR EJECT

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5
Q
Fire Warning in flight
1.
2.
If fire is not confirmed:
3.
4.
Time and conditions permitting:
5.
6.
7.
8.
9.
10.
If fire does not extinguish:
11.
If fire extinguishes:
12.
A

PCL…………………. RETARD (min practical for flight)
CHECK FOR FIRE
If fire is not confirmed;
TEST THE FIRE WARNING SYSTEM
CARRY OUT A PRECAUTIONARY EMERGENCY LANDING
FIRE CONFIRMED…………. CONSIDER EJECTION
If time and conditions permitting:
PCL…………………………………………………………..OFF
Emergency firewall shutoff handle………..PULL
Emergency oxygen handle…………………….PULL
above 10,000 feet MSL (Both)
Main oxygen supply hose………. DISCONNECT
BLEED AIR INFLOW switch……………………..OFF
OBOGS…………………………………………………….OFF

If fire does not extinguish:
EJECT
If fire extinguishes:
EJECT OR CARRY OUT A FORCED LANDING

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6
Q
SUSPECTED ENGINE MALFUNCTION
1.
2.
3.
4.
A
  1. Zoom………………………………………. IF POSSIBLE (wings level)
  2. PCL………………………………………….CURRENT POSITION
  3. Engine instruments…………………CHECK
  4. EJECT OR CARRY OUT APPROPRIATE EMERGENCY RESPONSE
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7
Q
ENGINE FAILURE IN FLIGHT
1.
2.
3.
4.
5.
6.
Time and conditions permitting:
7.
A
  1. PCL……………………………………………………………… OFF
  2. GLIDE………………………………………………………… 125 KIAS
  3. Emergency oxygen handle………………………. PULL
    above 10,000 ft MSL(both)
  4. Main oxygen supply hose……………………….. DISCONNECT (both)
  5. OBOGS……………………………………………………… OFF (Both)
  6. EJECT OR CARRY OUT A FORCED LANDING
    Time and conditions permitting:
  7. ATTEMPT AIRSTART
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8
Q
UNCOMMANDED POWER CHANGE / LOSS OF POWER /
UNCOMMANDED PROPELLER FEATHER
1.
2.
3.
4.
5.
If Power available is insufficint to complete PEL:
6.
If time and conditions permit:
7.
8.
A

PCL………………………………………………….MID RANGE
PMU………………………………………………………………OFF
PROP SYS C/B…………………Pull(if Np below 40%)
PCL……………………………………………….AS REQUIRED
PEL………………………………………………………EXECUTE

If power available is insufficient to complete PEL:
EJECT or
If time and conditions permit:
PROP SYS C/B……………………RESET( as required)
FORCED LANDING……………EXECUTE

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9
Q
COMPRESSOR STALL
1.
2.
3.
4.
If power available is not sufficient to complete PEL:
5.
A

PCL…..SLOWLY RETARD BELOW STALL THRESHOLD
DEFOG……………………………………………………………………..ON
PCL………………………………………………………….AS REQUIRED
PEL…………………………………………………………………EXECUTE

If power available is not sufficient to complete PEL:
EJECT OR CARRY OUT A FORCED LANDING

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10
Q

CHIP LIGHT / OIL SYSTEM MALFUNCTION
1.
2.

A

PCL……….MIN PRACTICAL, MINIMIZE PCL MOVEMENTS

PEL……………………………………………………………………EXECUTE

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11
Q
IMMEDIATE AIRSTART (PMU NORM)
1.
2.
3.
4.
If Airstart is unsuccessful
5.
6.
If Airstart is successful
7.
8.
9.
10.
A
  1. PCL……………………………………………………………….OFF
  2. STARTER SWITCH………………………..AUTO/RESET
  3. PCL……………………………………IDLE, ABOVE 13% N1
  4. Engine instruments……………………………….Monitor
    If Airstart is unsuccessful
  5. PCL……………………………………………………………….OFF
  6. EJECT OR CARRY OUT A FORCED LANDING
    If Airstart is successful
  7. PCL……….as required after N1 reaches idle RPM
  8. STARTER switch………………………………………NORM
  9. GEN Switch………….Verify ON, reset if necessary
  10. PEL……………………………………………………..EXECUTE
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