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T-45 > New EP > Flashcards

New EP Flashcards

1
Q

Cabin Alt Warning light in flight

A

*1. Mask – ON/TIGHT

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2
Q

COMPRESSOR STALL OR EGT/RPM WARNING LIGHT

A

IN-FLIGHT
*1. Throttle - IDLE
*2. EGT/RPM - Check
If EGT is greater than 450 oC 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

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3
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
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4
Q

GTS FIRE WARNING LIGHT

A

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

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5
Q

OIL PRESS WARNING LIGHT

A
    1. Throttle – MINIMUM FOR SAFE FLIGHT

* 2. Minimize throttle movements

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6
Q

OXYGEN WARNING LIGHT

A

AFTER TAKEOFF:

*1. Throttle – Increase N2 rpm above 75% (80% above FL300)

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7
Q

BRK PRESS CAUTION LIGHT

A

CATAPULT

*1. Suspend launch

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8
Q

CANOPY CAUTION LIGHT

A

CANOPY control lever – CHECK LOCKED

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9
Q

SKID CAUTION LIGHT

A 
*1. Go-around if practical
If go-around not practical:
*2. Brakes – RELEASE
*3. ANTI-SKID switch - OFF
*4. Brakes – Apply gradually
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10
Q

TP HOT CAUTION LIGHT

A

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

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11
Q

CLEAR ENGINE PROCEDURE/ABNORMAL START/TP FIRE ON SHUTDOWN

A

*1. Throttle - OFF
*2. ENGINE switches - ON
*3. FUEL SHUTOFF handle - DOWN
*4. GTS - START
*5. IGNITION switch - ISOLATE
When rpm below 20 percent and GTS advisory light illuminates:
*6. ENGINE switch - START

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12
Q

EMERGENCY SHUTDOWN/EGRESS

A
    1. Throttle - OFF
    1. ENGINE switch - OFF
    1. FUEL SHUTOFF handle - PULL
    1. Ejection seats - SAFE
    1. BATT switches - OFF
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13
Q

BRAKE FAILURE — ASHORE

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. Attempt braking
If brakes still unavailable:
*6. Hook – DOWN (if required)
*7. Parking brake handle – PULL (if required)
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14
Q

BRAKE FAILURE — AFLOAT

A
    1. Throttle - IDLE
    1. Parking brake handle - PULL
    1. Hook - DOWN
    1. Transmit
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15
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
If NWS failure suspected:
*6. Paddle switch - PRESS
If airborne:
*7. Gear and flaps – DO NOT REPOSITION
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16
Q

ABORT

A
    1. Throttle - IDLE
    1. Speed brakes - EXTEND
    1. Brakes - APPLY
    1. Hook – DOWN (if required)
    1. Release brakes prior to crossing the arresting gear
17
Q

EMERGENCY CATAPULT FLYAWAY

A

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

18
Q

ENGINE FAILURE DURING CATAPULT LAUNCH

A

*1. Eject

19
Q

BLOWN TIRE(S) AT THE CARRIER

A

*1. Gear and flaps – DO NOT REPOSITION

20
Q

ENGINE FAILURE

A

If below 1,500 feet AGL and airspeed below 180 KIAS:
*1. Eject
If above 1,500 feet AGL or airspeed greater than 180 KIAS:
*2. Execute Airstart

21
Q

AIRSTART

A

*1. Emergency oxygen green ring(s) - PULL
*2. Throttle - OFF
Simultaneously perform steps *3. and *4.
*3. GTS start button – PRESS AND HOLD
*4. Throttle - IDLE
If unsuccessful (no relight within 30 seconds after moving throttle to idle or EGT exceeds limits):
*5. Throttle – OFF (allow 30 seconds to drain if practical)
If within windmill airstart envelope (below 25,000 feet MSL, minimum 13% N2 RPM, recommended minimum 250 KIAS):
*6. Repeat steps *3. And *4.

22
Q

ELECTRICAL FIRE

A

*1. GEN switch - OFF

23
Q

SMOKE OR FUMES IN THE 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

24
Q

RAPID DECOMPRESSION

A

*1. Mask – ON/TIGHT
*2. Initiate controlled descent to lowest safe altitude below 18,000 feet MSL
If rapid decompression results in cabin altitude above 18,000 feet:
*3. Emergency oxygen green ring(s) - PULL
*4. OBOGS FLOW selector(s) - OFF

25
Q

LOW/NO MASK FLOW

A

FLIGHT:
*1. Throttle – Increase N2 rpm above 75% (80% above FL300)
If low/no mask flow continues 10 seconds after increasing N2 rpm:
If cabin altitude above 10,000 feet:
*2. Emergency oxygen green ring(s) - PULL
*3. OBOGS FLOW selector(s) - OFF

26
Q

ADVERSE PHYSIOLOGICAL SYMPTOMS

A

*1. Initiate controlled descent to below 10,000 feet cabin altitude (approximately 15,000 feet MSL)
*2. Control rate and depth of breathing (approximately one breath every 5 seconds)
When cabin altitude below 10,000 feet:
*3. Mask – OFF (affected cockpit)
*4. OBOGS FLOW selector – OFF (affected cockpit)
*5. Continue controlling rate and depth of breathing with mask off

27
Q

TOTAL ELECTRICAL FAILURE

A

*1. Emergency oxygen green ring(s) - PULL

28
Q

UNCOMMANDED ROLL/YAW

A

*1. FLAPS/SLATS lever – RETURN TO PREVIOUS SETTING

29
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

T-45 (11 decks)

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