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1
Q

What is the correct ejection posture?

A
  1. Buttocks well back in seat.
  2. Back pressed firmly against the seat back and sitting as straight as possible.
  3. Press head firmly against headpad.
  4. Eyes closed.
  5. Legs forward with feet touching the rudder pedals to ensure optimum thigh support.
  6. Grip the ejection handle with the preferred hand. Use the other hand to grip the wrist of the pulling hand to prevent flailing at high speeds.
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2
Q

EMERGENCY EGRESS ON THE GROUND

A
  1. SEAT PIN - IN
  2. LEG RESTRAINTS - RELEASE
  3. SEAT HARNESS - RELEASE
  4. OXYGEN MASK HOSE - DISCONNECT
  5. MIC-TEL - DISCONNECT
  6. PSP - DISCONNECT
  7. CANOPY - OPEN

Warning:
Eject if circumstances dictate however do not attempt to eject if:
- The occupants are not correctly strapped in
- The canopy is not closed and locked
- The front cockpit CFS pin and seat pin or rear cockpit seat pin (when occupied) are not removed

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3
Q

What is the warning associated with gliding checks?

Hint: Same as warning for EFATO

A

Delaying ejection in a futile attempt to:
1. Restart the engine
2. Recover controlled flight
3. Reach an aerodrome
…may place the aircraft in marginal conditions for safe ejection. Eject if unable to carry out a forced landing safely.

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4
Q

EMERGENCY LANDING CHECKS

A
  1. AIRSPEED - BELOW 180KTS
  2. LDG GR HANDLE - DOWN
  3. EMERGENCY LDG GR HANDLE - PULL
  4. FLAPS AS REQUIRED
    When aircraft has stopped:
  5. BATT1 and BATT2 - OFF
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5
Q

ENGINE FIRE OR SMOKE AND FUMES (GROUND)

[FIRE]

A
  1. ACS SHUTOFF - PULL
  2. PCL - FUEL OFF
  3. FUEL-HYD CUTOFF - PULL
  4. BATTS AND GENS - OFF
  5. BREAKS - AS REQUIRED
  6. EMERGENCY EGRESS ON GROUND

Warning:
Activating the EO2 may lead to pure oxygen flowing into the cockpit during egress. However, operate the EO2 if incapacitation due to fumes is assessed to be a greater risk.

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6
Q

ENGINE FIRE (FLIGHT)

[FIRE]

A
  1. EO2 - PULL
  2. ACS SHUTOFF - PULL
  3. PCL - MINIMUM PRACTICAL
  4. PMS - MANUAL
  5. CHECK FOR FIRE
    If fire is not confirmed:
  6. LAND AS SOON AS POSSIBLE
    If fire is confirmed:
  7. PCL - FUEL OFF
  8. FUEL-HYD CUTOFF - PULL
  9. BATT1 - OFF
  10. GEN1 AND GEN2 - OFF
    If fire persists:
  11. EJECT

Warning:
Monitor EO2 contents and descend to safe altitude before EO2 is exhausted.

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7
Q

SMOKE OR FUMES IN THE COCKPIT (FLIGHT)

[FIRE]

A
  1. EO2 - PULL
  2. ACS SHUTOFF - PULL
  3. CABIN PRESS - RAM
    If fumes continue:
  4. GEN1 AND GEN2 - OFF

Warning:
Monitor EO2 contents and descend to safe altitude before EO2 is exhausted. Land as soon as possible following smoke or fumes in the cockpit.

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8
Q

ABORTED TAKE-OFF

A
  1. PCL - IDLE
  2. BRAKES - AS REQUIRED
    If aborting due to engine fire:
  3. ENGINE FIRE OR SMOKE AND FUMES (GROUND)

Warning:
Eject if there is likely risk of collision.

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9
Q

ENGINE FAILURE AFTER TAKE-OFF (EFATO)

A
  1. PCL - FUEL OFF
    If sufficient runway is available:
  2. FUEL-HYD CUTOFF - PULL
  3. EMERGENCY LANDING CHECKS

Warning:
Delaying ejection in a futile attempt to:
1. Restart the engine
2. Recover controlled flight
3. Reach an aerodrome
…may place the aircraft in marginal conditions for safe ejection. Eject if unable to carry out a force landing safely.

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10
Q

ENGINE MECHANICAL FAILURE

A
  1. PCL - FUEL OFF
  2. FUEL-HYD CUTOFF - PULL
  3. EO2 - PULL IF ABOVE 10 000FT

Warning:
Monitor EO2 contents and descend to safe altitude before EO2 is exhausted.

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11
Q

ENGINE FLAMEOUT

  • Loss of power
  • ITT < 400C
  • NG < 80% (PMS AUTO) or 70% (PMS MAN)
A
  1. PCL - IDLE

2. IGNITERS - ON

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12
Q

ENGINE SURGE

  • Loss of power
  • ITT excessively high or fluctuating
  • Unusual engine noise
A
  1. PCL - IDLE

2. LAND AS SOON AS POSSIBLE

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13
Q

PMS FAILURE

[PMS MANUAL]

A
  1. PCL - CONTROL ENGINE LIMITS MANUALLY
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14
Q

ENGINE TORQUE

[ENG TORQUE]

A
  1. PCL - MINIMUM PRACTICAL
    If warning or caution remains:
  2. LAND AS SOON AS POSSIBLE
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15
Q

PROPELLER SPEED

[PROP SPEED]

A

NP above 2200RPM:

  1. PCL - MINIMUM PRACTICAL
  2. AIRSPEED - REDUCE
  3. LAND AS SOON AS POSSIBLE
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16
Q

ENGINE TEMPERATURE (GROUND)

[ENG ITT]

A

If ITT rapidly increases towards and exceeds 750C in ground idle with warning displayed:
1. PCL - FUEL OFF

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17
Q

ENGINE TEMPERATURE (FLIGHT)

[ENG ITT]
[ITT > 860C]

A

ITT above 860C:
1. PCL - MINIMUM PRACTICAL
If warning remains or warning was on, even though extinguished:
2. LAND AS SOON AS POSSIBLE

18
Q

ENGINE SPEED

[ENG NG]
[NG < 50.7%]
[NG > 104%]

A

NG < 50.7% (Caution):

  1. IGNITERS - ON
  2. PCL - SLOWLY INCREASE POWER

NG > 104% (Warning):
1. PCL - MINIMUM PRACTICAL
If warning remains:
2. LAND AS SOON AS POSSIBLE

19
Q

OIL PRESSURE OUT OF LIMITS

[OIL PRESS]

A

If warning or caution remains indicated:
1. PCL - MINIMUM PRACTICAL
If warning is indicated:
2. LAND AS SOON AS POSSIBLE

Note: Oil pressure may be as low as 40 psi during aerobatics if recovery is within 20 seconds. Hence why boldface is conducted only if warning/caution remains.

20
Q

OIL TEMPERATURE HIGH (GROUND)

[OIL TEMP]

A

OIL TEMP warning:
1. PCL - FUEL OFF

Note: If only a caution is displayed the aircraft can be turned into wind to increase airflow over the oil cooler.

21
Q

OIL TEMPERATURE HIGH (FLIGHT)

[OIL TEMP]

A

OIL TEMP warning:

  1. PCL - MINIMUM PRACTICAL
  2. LAND AS SOON AS POSSIBLE

Note: Similar to on the ground, if only a caution is displayed then just monitor the oil temperature.

22
Q

METAL PARTICLES DETECTED IN GEARBOX

[CHIP PROP]
[CHIP AGB]

A
  1. PCL - MINIMUM PRACTICAL
  2. LAND AS SOON AS POSSIBLE

Note: Minimise power changes.

23
Q

UNCOMMANDED POWER CHANGES

A
  1. PCL - IDLE
  2. PMS - MANUAL
  3. PCL - AS REQUIRED
24
Q

OXYGEN SYSTEM OFF (BOTH COCKPITS)

[OXY OFF]
[NO ANTI G]

A
  1. OXYGEN - ON. CHECK FLOW, CONNECTIONS, MASK.
    If above 10 000ft cabin altitude and problem persists:
  2. EO2 - PULL
  3. DESCEND BELOW 10 000ft CABIN ALTITUDE
25
Q

OBOGS COMPUTER BIT FAILURE

[OXY]
[OXY BIT]

A
  1. OXYGEN - ON. CHECK FLOW, CONNECTIONS, MASK.
    If above 10 000ft cabin altitude and problem persists:
  2. EO2 - PULL
  3. DESCEND BELOW 10 000ft CABIN ALTITUDE
26
Q

OBOGS FAILURE

[OXY]
[NO ANTI G] + [OXY FAIL]

A
  1. OXYGEN - OFF (BOTH COCKPITS)
    If above 10 000ft cabin altitude:
  2. EO2 - PULL
  3. DESCEND BELOW 10 000ft CABIN ALTITUDE
27
Q

OXYGEN PRESSURE OR OXYGEN CONCENTRATION LOW

[OXY]
[ANTI G] + [LOW OXY]

A
  1. OXYGEN - ON. CHECK FLOW, CONNECTIONS, MASK.
  2. PCL - INCREASE IF POSSIBLE
    If above 10 000ft cabin altitude and problem persists:
  3. EO2 - PULL
  4. DESCEND BELOW 10 000ft CABIN ALTITUDE
28
Q

OXY FLOW WARNING

[OXY FLOW]

A
  1. OXYGEN - ON. CHECK FLOW, CONNECTIONS, MASK.
    If rear cockpit affected:
  2. INSTRUCTOR SWITCH - FRONT OR REAR SELECTED
    If above 10 000ft cabin altitude and problem persists:
  3. EO2 (AFFECTED COCKPIT) - PULL
  4. DESCEND BELOW 10 000ft CABIN ALTITUDE
29
Q

CABIN ALTITUDE ABOVE 25 000FT

[CAB ALTITUDE]

A
  1. DESCEND TO 25 000FT CABIN ALTITUDE OR BELOW
30
Q

AIRCRAFT ALTITUDE ABOVE 26 000FT

[ACFT ALT]

A
  1. DESCEND TO 25 000FT AIRCRAFT ALTITUDE OR BELOW
31
Q

CABIN OVERPRESSURE WARNING

[CAB HI PRESS]
[OVPR]

A
  1. CABIN PRESS - PRESS DUMP

2. PCL - MINIMUM PRACTICAL

32
Q

FUEL PRESSURE LOW

[FPR FUEL PRESS]
[FPR]

A
  1. FUEL PUMPS - ON
  2. PCL - MINIMUM PRACTICAL
    If warning remains:
  3. LAND AS SOON AS POSSIBLE
33
Q

What is the warning associated with a fuel imbalance?

A

The aircraft will tend to roll towards the heavy wing and aileron deflection will increase with increasing fuel imbalance and with reducing speed.
Do not reduce speed below that which requires half aileron deflection.
Perform a handling check prior to landing to determine safe approach and landing speeds.

34
Q

TRIM RUNAWAY

A
  1. TRIM/AIL PWR - OFF
35
Q

AILERON CONTROL SYSTEM MALFUNCTION

A
  1. TRIM/AIL PWR - OFF
36
Q

FLAP FAILURE

[FLAP]

A
  1. AIRSPEED - BELOW 180KTS
37
Q

GEAR RETRACTION FAILURE

[GEAR]

A
  1. AIRSPEED - BELOW 180KTS
38
Q

GEAR LOWERING FAILURE

[GEAR]

A
  1. AIRSPEED - BELOW 180KTS
39
Q

UNCOMMANDED OXYGEN OVERPRESSURE MALFUNCTION

A
  1. OXYGEN - OFF (AFFECTED COCKPIT)
    If above 10 000ft cabin altitude:
  2. EO2 - PULL
  3. DESCEND BELOW 10 000FT CABIN ALTITUDE
40
Q

What are the non-boldface ejection checks?

A

Carry out as many of the following checks as time permits:

  1. Harness - Secured and locked
  2. PSP - Connected
  3. Helmet - Visors down, chin-strap secured
  4. Seat pin - Removed
  5. Location - Suitable
  6. Height - Ideally 2000ft AGL
  7. Airspeed - 150-250KTS
  8. Trim - 1/3 aileron trim
  9. Attitude - Wings level, climbing
  10. PCL - IDLE, friction tight
41
Q

HYPOXIA

A
  1. EO2 - PULL
  2. DESCEND BELOW 10 000FT AIRCRAFT ALTITUDE
  3. OXYGEN OFF (BOTH COCKPITS)
    When at or below 10 000ft aircraft altitude:
  4. ACS SHUTOFF - PULL
  5. CABIN PRESS - RAM

If symptoms persist and incapacitation is likely:
9. EJECT

42
Q

BRAKE FAILURE

A
  1. BRAKES RELEASE - IF REQUIRED
  2. DIRECTIONAL CONTROL - ESTABLISH
  3. SERVICABLE BRAKE - APPLY
  4. RUDDER - AS REQUIRED
    If risk of collision exists or departing a runway / taxiway sealed surface:
  5. PCL - FUEL OFF
  6. FUEL-HYD CUTOFF - PULL

2FTS (11 decks)

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