EP Flashcards

1
Q

CLEAR ENGINE PROCEDURE / ABNORMAL START / TP FIRE ON SHUTDOWN

A
  1. Throttle - OFF
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2
Q

EMERGENCY SHUTDOWN/EGRESS

A
  1. Throttle - OFF
  2. ENGINE switch - OFF
  3. FUEL SHUTOFF handle - PULL
  4. Ejection seats - SAFE
  5. BATT switches - OFF
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3
Q

ENGINE FAILURE

A

If below 1,500 feet AGL and airspeed below 180 KIAS:
1. Eject
Otherwise:
2. Execute AIRSTART

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4
Q

AIRSTART

A
  1. Emergency oxygen green ring(s) - PULL
  2. Throttle - OFF
    Simultaneously perform steps *3 and *4.
  3. GTS start button - PRESS
  4. Throttle - IDLE
    If unsuccessful (no relight within 30 seconds after moving throttle to idle or stabilized EGT exceeds limits):
  5. Throttle - OFF (allow 30 seconds to drain if practical)
    If above 13% RPM and 250 KIAS , repeat straps *3 and *4. Otherwise, proceed to step 6.
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5
Q

COMPRESSOR STALL OR EGT/RPM WARNING LIGHT

A
  1. Throttle - IDLE
  2. EGT/RPM - CHECK
    If EGT is greater than 450ºC for more than 6 seconds at idle:
  3. Execute Engine Failure procedure
    If EGT responds normally:
  4. Throttle - Slowly advance to minimum for safe flight
  5. Minimize throttle movements
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6
Q

ABORT

A
  1. Throttle - IDLE
  2. Speed brakes - EXTEND
  3. Brakes - APPLY
  4. Hook - DOWN (IF REQUIRED)
  5. BRAKES - Release prior to crossing the arresting gear
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7
Q

EMERGENCY CATAPULT FLYAWAY

A
  1. Throttle - MRT
  2. Maintain 24 units AOA
    If engine failed, or unable to stop settle:
  3. Eject
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8
Q

BRAKE FAILURE - ASHORE / SKID CAUTION

A

If flyaway airspeed available:
1. Go-around
If flyaway airspeed not available, or during taxi:
1. Throttle - IDLE
2. Brakes - RELEASE
3. Anti-skid switch - OFF
4. BRAKES - Apply Gradually
If brakes still unavailable:
5. Hook - DOWN (if required)
6. Parking brake handle - PULL (if required)

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9
Q

BRAKE FAILURE - AFLOAT

A
  1. Throttle - IDLE
  2. Parking brake handle - PULL
  3. Hook - DOWN
  4. Transmit
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10
Q

LOSS OF DIRECTIONAL CONTROL

A

If flyaway airspeed available:
1. Go-around
If flyaway airspeed not available:
2. Abort
If blown tire suspected:
3. BRAKES - RELEASE
4. Anti-skid switch - OFF
5. BRAKES - Apply Gradually
If NWS failure suspected:
6. Paddle switch - PRESS

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11
Q

ASYMMETRIC FLAPS/SLATS

A
  1. FLAPS/SLATS leverage - RETURN TO PREVIOUS SETTING
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12
Q

DEPARTURE/SPIN PROCEDURE

A
  1. Controls - NEUTRALIZE / FORCIBLY
    CENTER RUDDER PEDALS
  2. Speed brakes - RETRACT
  3. Throttle - IDLE
  4. Check altitude, AOA, airspeed, and turn needle
    If spin confirmed:
    INVERTED (AOA pegged at 0 units):
  5. Rudder pedal - FULL OPPOSITE TURN NEEDLE
  6. Lateral stick - FULL OPPOSITE TURN NEEDLE
  7. Longitudinal stick - NEUTRALIZE
    UPRIGHT (AOA above 28 units):
  8. Rudder pedal - FULL OPPOSITE TURN NEEDLE
  9. Lateral stick - FULL WITH TURN NEEDLE
  10. Longitudinal stick - NEUTRALIZE
    If recovery indicated or airspeed increasing through 160 KIAS:
  11. Lateral stick - NEUTRALIZE
    When recovery indicated:
  12. Rudder pedals - SMOOTHLY CENTER
    If out of control passing through 10,000 feet AGL
  13. EJECT
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13
Q

TOTAL ELECTRICAL FAILURE

A
  1. Emergency oxygen green ring(s) - PULL
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14
Q

ADVERSE PHYSIOLOGICAL SYMPTOMS

A

If above 10,000 feet cabin altitude:
1. Emergency oxygen green ring(s) - PULL
2. OBOGS FLOW selector(s) - OFF
3. Descend below 10,000 feet cabin altitude

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15
Q

RAPID DECOMPRESSION

A
  1. Emergency oxygen green ring(s) - PULL
  2. OBOGS FLOW selector(s) - OFF
  3. Descend below 10,000 feet cabin altitude
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16
Q

ELECTRICAL FIRE

A
  1. GEN switch - OFF
17
Q

SMOKE OR FUMES IN COCKPIT

A
  1. Mask - ON/TIGHT
  2. Initiate controlled descent to below 18,000 feet MSL
  3. AIR FLOW knob - OFF (below 18,000 feet MSL if possible)
    If unable to clear smoke or unable to see:
  4. Airspeed - REDUCE (as practical)
  5. Warn other cockpit occupants / secure loose items
  6. Seat - LOWER
  7. MDC firing handle - PULL
18
Q

FIRE WARNING LIGHT

A

GROUND
1. Execute Emergency Shutdown / Egress
TAKEOFF
If decision is made to stop:
1. Abort
If fire is confirmed and unable to abort:
2. Eject
IN-FLIGHT
1. Throttle - MINIMUM FOR SAFE FLIGHT
2. Check for secondary indications of fire
If fire confirmed or flight control lost:
3. Eject
If fire not confirmed and control effectiveness remains:
4. Land as soon as possible

19
Q

GTS FIRE WARNING LIGHT

A

GROUND
1. Execute Emergency Shutdown / Egress
IN-FLIGHT
1. ENGINE switch - OFF

20
Q

OIL PRESS WARNING LIGHT

A
  1. Throttle - Immediately set minimum power required within the range 78 to 87% rpm
  2. Avoid further power changes
21
Q

OXYGEN WARNING LIGHT

A

IN-FLIGHT
1. Throttle - Set minimum 80% rpm
2. Execute Adverse Physiological Symptoms (as required)

22
Q

TP HOT CAUTION LIGHT

A

GROUND
1. Execute Emergency Shutdown / Egress
IN-FLIGHT
1. Throttle - MINIMUM FOR SAFE FLIGHT