Emergency Procedures (NATOPS) Flashcards

1
Q

EGT/RPM WARNING LIGHT OR COMPRESSOR STALL

A

IN-FLIGHT
Simultaneously perform steps 1. and 2.

    1. Throttle - Minimum for safe flight
    1. Controls - Neutralize
    1. EGT/RPM - Monitor

IF EGT is greater than 450C for more than 6 seconds after throttle IDLE:

*4. Execute Airstart

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2
Q

GINA FAILURE

A

IN-FLIGHT

*1. Revert to standby instruments

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3
Q

BRAKE FAILURE

A

If flyaway airspeed available:
*1. Go-Around

If flyaway airspeed unavailable:

    1. Throttle - IDLE
    1. Brakes - RELEASE
    1. Anti-Skid Switch - OFF
    1. Attempt Braking

If brakes still unavailable:

    1. Hook - DOWN (if required)
    1. Parking brake handle - PULL (if required)
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4
Q

HYPOXIA/OBOGS CONTAMINATION

A

If hypoxic symptoms are evident and/or suspected, proceed as follows:

    1. Emergency oxygen green ring(s) - PULL
    1. OBOGS flow selector(s) - OFF
    1. Initiate rapid descent to below 10,000’ MSL or minimum safe altitude.
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5
Q

BRAKE FAILURE - AFLOAT

A
    1. Throttle - IDLE
    1. Parking brake handle - PULL
    1. Hook - DOWN
    1. Transmit
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6
Q

BRK PRESS CAUTION LIGHT

A

CATAPULT

*1. Suspend Launch

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7
Q

UNASSISTED AIRSTART (immediate/windmill)

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

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8
Q

ENGINE FAILURE

A

If below 1,500’ AGL and airspeed below 180 KIAS:
*1. EJECT

If above 1,500’ AGL or airspeed greater than 180 KIAS:
*2. Execute Airstart

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9
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. Secondary Indications - Check
If secondary indications exist or fire confirmed:
*3. Eject
If fire not confirmed and control effectiveness remains:
*4. Land as soon as possible

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10
Q

SKID CAUTION LIGHT

A
*1. Go-around if practical
If go-around is not practical
*2. Brakes - Release
*3. Anti-skid switch - OFF
*4. Attempt braking
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11
Q

ENGINE FAILURE DURING CATAPULT LAUNCH

A

*1. Eject

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12
Q

UNCOMMANDED ROLL/YAW

A

If rolling and yawing is experienced during operation of the wing flaps or while the flaps are extended, an asymmetric wing flaps condition probably exists:
*1. FLAPS/SLATS lever - return to previous setting

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13
Q

GTS FIRE WARNING LIGHT

A

GROUND
*1. Execute emergency shutdown/egress
IN-FLIGHT
*1. Engine switch - OFF

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14
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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15
Q

AIRCRAFT SETTLING OFF CATAPULT

A

*1. Throttle - CHECK FULL FORWARD
*2. Maintain 24 units AOA
If settle not stopped
*3. Eject

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16
Q

DEPARTURE/SPIN PROCEDURE

A
    1. Controls - neutralize/forcibly center rudder pedals
    1. Speed brakes - RETRACT
    1. Throttle - IDLE
    1. Check altitude, AOA, airspeed, turn needle.

If spin confirmed:
INVERTED (AOA pegged at 0 units)
*5. Rudder pedals - Full opposite turn needle
*6. Lateral stick - Full opposite turn needle
*7. Longitudinal stick - Neutralize
UPRIGHT (AOA above 28 units)
*8. Rudder pedals - Full opposite turn needle
*9. Lateral stick - Full with turn needle
*10. Longitudinal stick - Neutralize

If recovery indicated or airspeed increasing through 160kias:
*11. Lateral stick - Neutralize
When recovery indicated:
*12. Rudder pedals - Smoothly center

If out of control passing through 10,000’ AGL:
*13. Eject

17
Q

OIL PRESS WARNING LIGHT

A
    1. Throttle - Minimum for safe flight

* 2. Minimize throttle movements

18
Q

SIM MODE (MFD DISPLAY)

A

IN-FLIGHT

*1. Revert to standby instruments

19
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
20
Q

ASSISTED AIRSTART

A

Below 15,000’ MSL, 165 to 250 KIAS:

    1. Emergency oxygen green ring(s) - PULL
    1. Throttle - OFF
    1. GTS - START

When rpm drops below 20% N2 and GTS advisory light illuminates:

    1. Engine switch - START
    1. Throttle - IDLE
21
Q

OXYGEN WARNING LIGHT

A
    1. Emergency Oxygen Green Ring(s) - PULL
    1. OBOGS flow selector(s) - OFF
    1. Initiate rapid descent to below 10,000’ MSL or minimum safe altitude
22
Q

ABNORMAL START/TAILPIPE FIRE AFTER SHUTDOWN

A

*1. Execute clear engine procedure

23
Q

BLOWN TIRE(S) AT THE CARRIER

A

*1. Gear and flaps - DO NOT REPOSITION

24
Q

SMOKE OR FUMES FROM COCKPIT

A
    1. Altitude - Descend below 18,000’ (if practical)
    1. Air flow knob - OFF

If unable to clear smoke or unable to see:

    1. Airspeed - REDUCE
    1. Warn other cockpit occupant/secure loose items
    1. Seat - LOWER
    1. MDC firing handle - PULL
25
Q

LOW/NO MASK FLOW

A

IN-FLIGHT:
*1. Throttle - increase RPM above 75% (80% above FL300)
If no mask flow or low mask flow continues 10 seconds after increasing RPM:
*2. Emergency oxygen green ring(s) - PULL
*3. OBOGS flow selector - OFF
*4. Initiate rapid descent to below 10,000’ MSL or minimum safe altitude

26
Q

ELECTRICAL FIRE

A

*1. GEN switch - OFF

27
Q

TP HOT CAUTION LIGHT

A

GROUND
*1. Execute emergency shutdown/egress
IN-FLIGHT
*1. Throttle - Minimum for safe flight

28
Q

LOSS OF DIRECTIONAL CONTROL

A

*1. Rudder - As required to counter swerve

If flyaway airspeed available:
*2. Go-around

If flyaway airspeed not available:
*3. Abort

If blown tire suspected:

    1. Brakes - RELEASE
    1. Anti-skid switch - OFF prior to braking

If airborne:
*6. Gear and flaps - DO NOT REPOSITION

29
Q

TOTAL ELECTRICAL FAILURE

A

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

30
Q

CANOPY CAUTION LIGHT

A

*1. Canopy control lever - Check locked

31
Q

CLEAR ENGINE PROCEDURE

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