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Question 1

ENGINE FIRE DURING START

Answer 1

If fire light warning comes on, or there are other indications of fire, proceed as follows:
*1. Throttles – Off
If engine fails to shut down:
2. Fuel Shutoff Switches – Closed

Question 2

ABORT / ARRESTMENT

Answer 2

*1. Throttles – Idle
*2. Speed brakes - Extend
*3. Brakes – As Required
If required / conditions permitting:
*4. Chute – Deploy
*5. Hook Button – Push

Question 3

ENGINE FAILURE / FIRE WARNING DURING TAKEOFF

Answer 3

If takeoff is refused: 
*1. Abort
If takeoff is continued:
*2. Throttles – Max
*3. Stores – Jettison (if necessary)
4. At safe ejection altitude – Perform In-Flight Engine Fire Warning procedure

Question 4

ENGINE FAILURE AT LOW ALTITUDE

Answer 4

• 1. Throttles – Max
     
     2. Engine Instruments – Monitor

If both engines fail at low altitude, and with sufficient airspeed, zoom the aircraft to exchange airspeed for altitude and time. Try to airstart immediately. A/C attitude should not exceed 20⁰ nose-up. Ejection should be done while A/C is in a positive climb

Question 5

FIRE WARNING IN FLIGHT

Answer 5

*1. Throttle (affected engine) – Idle
If FIRE light goes out:
*2. FIRE lights – Test
If light(s) remain illuminated or lights test fails:
*3. Throttle (affected engine) – Off.
If light(s) remains illuminated or affected engine remains running:
*Fuel Shutoff Switch (affected engine) – Closed.
*5. If fire is confirmed – Eject.

Question 6

Erect PSG Recovery

Answer 6

*1. Stick – Forward as required
Warning: If stick position forward of trim does not produce immediate recovery indications, full forward stick should be applied without delay. Delay may result in spin entry.
*2. Ailerons and Rudder – Neutral
Warning: Failure to relax forward stick on recovery may cause the aircraft to enter an inverted PSG or inverted spin.

Question 6

BRAKE FAILURE

Answer 6

If detected after touchdown and flyaway airspeed available:
*1. Go Around
If brake failure occurs at slow speed or flyaway airspeed is not available:
*1. Brakes - Release
*2. ANTISKID Switch - Off
*3. Brakes - Apply

Question 7

ERECT SPIN RECOVERY

Answer 7

• 1. Stick – Full Forward
• 2. Aileron – Full in direction of spin (through the spring stop)
• 3. Rudder – Full opposite
• 4. Flaps – Auto (not to sacrifice stick position)

Question 9

INVERTED PSG / IPH / INVERTED SPIN

Answer 9

*1. Flaps – Up, (confirm up)
*2. Stick – Aft as required
*3. Ailerons and Rudder – Neutral
If spin is confirmed:
*4. Rudder – Full Opposite TN
*5. If control is not regained from an erect or inverted spin by 10K’ AGL solo or 15K’ AGL dual – Eject

Question 10

LOSS OF DIRECTIONAL CONTROL / BLOWN TIRE ON TAKEOFF OR LANDING

Answer 10

If flyaway airspeed available:
*1. Go around
If flyaway airspeed not available:
*1. Abort
*2. ANTISKID switch - Off.

Question 11

LOSS OF CABIN PRESSURIZATION / HYPOXIC SYMPTOMS

Answer 11

1. OXYGEN DILUTER LEVER - 100%

Question 12

Fake

Answer 12

Fake

Question 13

UNCOMMANDED PITCH/YAW

Answer 13

• 1. SAS Cutoff switch: Activate

2. Yaw and pitch damper switches: Confirm OFF