T45 EPs Flashcards

1
Q

Clear Engine Procedure/Abnormal Start/TP Fire on Shutdown

A

Throttle - Off

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2
Q

Emergency Shutdown/Egress

A
  1. Throttle - Off
  2. Engine Switch - Off
  3. Fuel Shutoff handle - Down
  4. Ejection seats - Safe
  5. Batt Switches - Off
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3
Q

Engine Failure

A

If below 1500 feet AGL and airspeed below 180 KIAS:
1. Eject
Otherwise:
2. Execute Airstart

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4
Q

Airstart

A
  1. Emergency O2 green ring(s) - Pull
  2. Throttle - Off
    Simultaneously performs steps 3 and 4:
  3. GTS start button - Press
  4. Throttle - Idle
    If unsuccessful (no relight within 30 sec 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 steps 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 450 C for more than 6 sec at idle:
  3. Execute Engine Failure Procedure.
    If EGT responds normally:
  4. Throttle - Idle
  5. Minimize throttle movements.
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5
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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6
Q

BRAKE FAILURE - ASHORE / SKID CAUTION

A

If flyaway airspeed available:
1. GO-AROUND.
If flyaway airspeed not available, or during taxi:
2. THROTTLE - IDLE
3. BRAKES - RELEASE
4. ANTI-SKID SWITCH – OFF
5. BRAKES – APPLY GRADUALLY
If brakes still unavailable:
6. HOOK - DOWN (IF REQUIRED)
7. PARKING BRAKE HANDLE - PULL (IF REQUIRED)

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7
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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8
Q

ASYMMETRICAL FLAPS/SLATS

A
  1. FLAPS/SLATS LEVER - RETURN TO PREVIOUS SETTING
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9
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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10
Q

TOTAL ELECTRICAL FAILURE

A
  1. EMERGENCY OXYGEN RING(S) - PULL
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11
Q

ADVERSE PHYSICALOGICAL SYMPTOMS

A
  1. EMERGENCY OXYGEN RING(S) - PULL
  2. OBOGS FLOW SELECTOR(S) - OFF
  3. DECEND BELOW 10,000FEET CABIN ALTITUDE.
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12
Q

RAPID DECOMPRESSION

A
  1. EMERGENCY OXYGEN RING(S) - PULL
  2. OBOGS FLOW SELECTOR(S) - OFF
  3. DECEND BELOW 10,000FEET CABIN ALTITUDE.
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13
Q

ELECTRICAL FIRE

A
  1. GEN SWITCH - OFF
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14
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 OCCUPANT / SECURE LOOSE ITEMS.
  6. SEAT - LOWER
  7. MDC FIRING HANDLE - PULL
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15
Q

EGT/RPM WARNING LIGHT

A
  1. THROTTLE - IDLE
  2. EGT/RPM - CHECK
    If EGT is greater than 450 C for more than 6 seconds at IDLE:
  3. EXECUTE ENGIEN FAILURE PROCEDURE
    If EGT responds normally:
  4. THROTTLE - SLOWLY ADVANCE TO MINIMUM FOR SAFE FLIGHT
  5. MINIMIZE THROTTLE MOVEMENTS.
16
Q

FIRE

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 INDICATION 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.

17
Q

GTS FIRE

A

GROUND
1. EXECUTE EMERGENCY SHUTDOWN / EGRESS

IN-FLIGHT
1. ENGINE SWITCH - OFF

18
Q

OIL PRESS WARNING LIGHT

A
  1. THROTTLE - IMMEDIATLY SET MINIMUM POWER REQUIRED WITHIN THE RANGE 78 - 87% RPM.
  2. AVOID FURTHER POWER CHANGES.
19
Q

OXYGEN WARNING LIGHT

A

IN-FLIGHT
1. THROTTLE - SET MINIMUM 80% RPM.
2. EXECUTE ADVERSE PHYSIOLOGICAL SYMPTOMS (AS REQUIRED)

20
Q

TP HOT

A

GROUND
1. EXECUTE EMERGENCY SHUTDOWN/EGRESS

IN-FLIGHT
1. THROTTLE - MINMUM FOR SAFE FLIGHT