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T-45 > Critical Action Memory Items > Flashcards

Critical Action Memory Items Flashcards

1
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
If GTS no longer required:
7. ENGINE switch-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
6. PARKING BRAKE handle-PULL
7. Canopy-OPEN
If canopy cannot be opened:
8. MDC firing handle-PULL
To evacuate with survival kit:
9. Upper Koch fittings-RELEASE
10. Manual Override Handle-PULL
To evacuate without survival kit:
11. Koch fittings-RELEASE UPPER AND LOWER
12. Manual Override Handle-PULL
13. Oxygen/communications hose-DISCONNECT

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3
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)
8. External lights-ON
9. Transmit to GND/TOWER
10. Throttle-OFF (prior to impact or departing paved surface)
If airborne:
11. ANTI-SKID switch-OFF
12. Attempt a Short Field Arrestment
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4
Q

Brakes failure-afloat

A
  • Throttle-IDLE
  • Parking brake handle-PULL
  • Hook-DOWN
  • Transmit
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5
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
8. Engine instruments-MONITOR
9. Refer to procedure for blown tire(s) at field or NWS/NWS AUG caution light
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6
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
      1. Transmit your intentions
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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

Blown tire(s) at the carrier

A

*1. Gear and flaps-DO NOT REPOSITION
2. Engine instruments-MONITOR
3. HYD 1 Pressure-MONITOR
4. Obtain visual inspection, if practical
If decision to divert is made:
5. Flaps-As Required
6. Execute appropriate BINGO profile to designated divert field with operable arresting gear
7. Comply with Landing with Blown Tire(s) Procedure
If decision to perform shipboard landing is made:
8. Perform a Normal Carrier Approach
Immediately upon touchdown simultaneously perform the following:
9. Throttle-MRT
10. Speedbrakes-RETRACT
11. Rudder-AS REQUIRED TO COUNTER SWERVE
12. Control stick-SMOOTHLY APPLY UP TO FULL BACK STICK
If the aircraft bolters:
13. Rudder pedals-CENTER (NEUTRALIZE) ONCE AIRBORNE AND SET FLYAWAY PITCH ATTITUDE

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9
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

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10
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.
If within assisted airstart envelope (below 15,000 feet MSL, 165-250 KIAS):
7. GTS start button-PRESS
When RPM drops below 20% N2 and GTS advisory light illuminates:
8. ENGINE switch-START
9. Throttle-IDLE
If unsuccessful (no relight within 30 seconds after moving throttle to idle or EGT exceeds limits) and altitude/airspeed available:
10. Reattempt Airstart procedure
If engine will not start and MFCDs needed:
11. GEN switch-RESET
12. DISPLAY POWER switch-ORIDE
If successful:
13. Execute Successful Airstart procedure

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11
Q

Compressor stall or EGT/RPM warning light

A

*1. Throttle-IDLE
*2. EGT/RPM-Check
If EGT is greater than 450 degrees C 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. Land as soon as possible

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12
Q

Electrical fire

A

*1. GEN switch-OFF
2. Non-essential electrical equipment-OFF
If fire out:
3. Land as soon as practical
If fire persists:
4. Proceed to VMC as soon as possible
5. BATT switches-OFF
6. Emergency oxygen green ring(s)-PULL
7. Land as soon as possible
8. Landing gear-EMERGENCY EXTENE
9. Plan a no-flap approach and arrested landing, if available. Recommended a Short Field Arrestment due to loss of NWS

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13
Q

Smoke or fumes in the cockpit

A

*1. Altitude-DESCENT BELOW 18,000 FEET (if practical)
*2. AIR FLOW knob-OFF
If unable to clear smoke or unable to see:
*3. Airspeed-REDUCE (As practical)
*4. Warn other cockpit occupants/secure loose items
*5. Seat-LOWER
*6. MDC firing handle-PULL
7. Land as soon as possible

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14
Q

Low/no mask flow/O2 PRES caution light-inflight

A

If low/no mask flow is evident and/or suspected or if the O2 PRES caution light illuminates, proceed as follows:
*1. Throttle-Increase RPM above 75% (80% above FL300)
If low/no mask flow or low mask flow continues and/or O2 PRES caution light remains illuminates 10 seconds after increasing RPM:
*2. Emergency oxygen green ring(s)-PULL
*3. OBOGS FLOW selector(s)-OFF
*4. Initiate rapid descent to below 10,000 feet MSL or minimum safe altitude
5. Control rate and depth of breathing
6. Check OBOGS system integrity
a. Mask integrity
b. Hose connections
If obvious cause of low/no mask flow and/or source of O2 PRES caution light illumination is identified and corrected:
7. Consider resetting emergency oxygen system and resuming normal OBOGS operation
Otherwise:
8. Maintain below 10,000 feet cabin pressure altitude prior to emergency oxygen depletion (3-20 minutes)
9. Consider removing mask and resetting emergency oxygen system
10. Land as soon as practical, using remaining emergency oxygen for approach and landing as required

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15
Q

Hypoxia/OBOGS contamination

A

If hypoxia symptoms are evident and/or suspected, proceed as follows:
*1. Emergency oxygen green ring(s)-PULL
*2. OBOGS FLOW selector(s)-OFF
*3. Initiate rapid descent to below 10,000 feet MSL OR MINIMUM SAFE ALTITUDE
4. Control rate and depth of breathing
Once below 10,000 feet MSL:
5. AIR FLOW knob-OFF
6. Remain on emergency oxygen until emergency oxygen supply is depleted
7. Oxygen Mask-REMOVE
8. Land as soon as possible

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16
Q

Total electrical failure

A
    1. Emergency oxygen green ring(s)-PULL
      1. Proceed to VMC as soon as possible
      2. Attempt to reset generator/check BATT switches-ON
      3. Land as soon as practical
      4. Landing gear-EMERGENCY EXTEND. (Retraction is not available)
      5. Plan a no-flap/slat approach
      6. Make a short field arrestment if available due to loss of NWS and anti-skid
17
Q

Uncommanded roll/yaw

A

*1. FLAPS/SLATS lever-RETURN TO PREVIOUS SETTING
If trim failure suspected:
2. Execute Trim Failure procedure
If trim failure not suspected:
3. Controllability check-PERFORM AS REQUIRED
4. Land as soon as practical

18
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 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

19
Q

EGT/RPM warning in flight

A

*1. Throttle-IDLE
*2. EGT/RPM-Check
If EGT is greater than 450 degrees C 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. Land as soon as possible

20
Q

FIRE warning on the ground

A

*1. Execute Emergency Shutdown/Egress

21
Q

FIRE warning on takeoff

A

If the decision is made to stop:
*1. Abort
If fire is confirmed and unable to abort:
*2. Eject

22
Q

FIRE warning in flight

A

*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

23
Q

GTS FIRE warning on the ground

A

*1. Execute Emergency Shutdown/Egress

24
Q

GTS FIRE warning in flight

A

*1. ENGINE switch-OFF
2. Check for secondary indications of fire
If fire confirmed or flight controls lost:
Eject
3. If fire not confirmed and control effectiveness remains:
4. Land as soon as possible

25
Q

OIL PRESS warning light

A
    1. Throttle-MINIMUM FOR SAFE FLIGHT
    1. Minimize throttle movements
      1. Land as soon as possible (Precautionary Approach recommended)
26
Q

OXYGEN warning light in-flight/landing/post-flight

A

*1. Emergency oxygen green ring(s)-PULL
*2. OBOGS FLOW selector(s)-OFF
*3. Initiate rapid descent to below 10,000 feet MSL or minimum safe altitude
4. Control rate and depth of breathing
Once below 10,000 ft MSL:
5. AIR FLOW knob-OFF
6. Remain on emergency oxygen until emergency oxygen supply is depleted
7. Oxygen Mask-REMOVE
If hypoxia symptoms exist or OXYGEN light remains illuminated:
8. Land as soon as possible
If no hypoxia symptoms exist and OXYGEN light is extinguished
9. Land as soon as practical

27
Q

BRK PRESS caution light on catapult

A

*1. Suspend launch

28
Q

O2 PRESS caution light in-flight

A

*Throttle-Increase RPM above 75% (80% above FL300)
If low/no mask flow continues and/or O2 PRESS caution light remains illuminated 10 seconds after increasing RPM:
*2. Emergency oxygen green ring(s)-PULL
*3. OBOGS FLOW selector(s)-OFF
*4. Initiate rapid descent to below 10,000 feet MSL or minimum safe altitude
5. Control rate of breathing
6. Check OBOGS system integrity
a. Mask integrity
b. hose connections
If obvious cause of low/no mask flow and/or source of O2 PRES caution light illumination is identified and corrected:
7. Consider resetting emergency oxygen system and resuming normal OBOGS operation
Otherwise:
8. Maintain below 10,000 feet cabin pressure altitude prior to emergency oxygen depletion (3-20 minutes)
9. Consider removing oxygen mask and resetting emergency oxygen system
10. Land as soon as practical, using remaining emergency oxygen for approach and landing as required

29
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
If airborne:
5. ANTI-SKID switch-OFF
6. Make Short Field Arrestment
30
Q

TP HOT caution light on the ground

A

*1. Execute Emergency Shutdown/Egress

31
Q

TP HOT caution light in-flight

A

*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

T-45 (11 decks)

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