Emergency Procedures Flashcards

1
Q

APU

FIRE

A

**APU FIRE LIGHT*******
*1. APU FIRE light - PUSH.
*2. FIRE EXTGH READY light - PUSH.
GROUND
*3. Throttles - OFF.
4. Egress.
IN-FLIGHT
3. Land as soon as possible

E63

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2
Q

[L BLEED ] | [R BLEED]

A

**DUAL L/R BLEED WARNING LIGHTS***
GROUND
1. Throttles - OFF.
———————————-
IN FLIGHT
*1. Throttles - MINIMUM PRACTICAL
OBOGS Aircraft:
*2. Emergency oxygen green ring(s) - PULL.
All Aircraft:
*3. BLEED AIR knob - OFF (DO NOT CYCLE).
*4. Initiate rapid descent to below 10,000 feet MSL.

Additional steps on E64

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3
Q

[L BLEED]

A

**SINGLE L BLEED OR R BLEED WARNING LIGHT****
GROUND
1. Throttles - OFF.
———————————-
IN FLIGHT
*1. Throttle affected engine - IDLE.
*2. BLEED AIR knob - L OFF or R OFF (DO NOT CYCLE).
If light goes out, execute single BLD OFF caution procedure (p E77).
If light remains on:
*3. Throttle affected engine - OFF.
If light remains on:
OBOGS Aircraft:
*4. Emergency oxygen green ring(s) - PULL.
All Aircraft:
*5. BLEED AIR knob - OFF (DO NOT CYCLE).
*6. Initiate rapid descent to below 10,000 feet MSL.
7. Land as soon as possible.

Additional steps on E65

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4
Q

[R BLEED]

A

**SINGLE L BLEED OR R BLEED WARNING LIGHT****
GROUND
1. Throttles - OFF.
———————————-
IN FLIGHT
*1. Throttle affected engine - IDLE.
*2. BLEED AIR knob - L OFF or R OFF (DO NOT CYCLE).
If light goes out, execute single BLD OFF caution procedure (p E77).
If light remains on:
*3. Throttle affected engine - OFF.
If light remains on:
OBOGS Aircraft:
*4. Emergency oxygen green ring(s) - PULL.
All Aircraft:
*5. BLEED AIR knob - OFF (DO NOT CYCLE).
*6. Initiate rapid descent to below 10,000 feet MSL.
7. Land as soon as possible.

Additional steps on E65

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5
Q

[FIRE] | [FIRE]

A
*********FIRE LIGHT*********
Ground
*1. Throttles - OFF.
*2. FIRE light affected engine - PUSH.
*3 FIRE EXTGH READY light - PUSH.
4. BATT switch - OFF.
5. Egress.
--------------------------------
IN FLIGHT
Dual FIRE lights:
*1. Throttles - Minimum Practical.
Single FIRE light or Dual when side confirmed:
*2. Throttle affected engine - OFF.
*3. FIRE light affected engine - PUSH.
*4. FIRE EXTGH READY light - PUSH.
*5. HOOK handle - DOWN.
6. Land as soon as possible. (Single Engine Approach and Landing p E32)

Additional steps on E66

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6
Q

[FIRE]

A
*********FIRE LIGHT*********
Ground
*1. Throttles - OFF.
*2. FIRE light affected engine - PUSH.
*3 FIRE EXTGH READY light - PUSH.
4. BATT switch - OFF.
5. Egress.
--------------------------------
IN FLIGHT
Dual FIRE lights:
*1. Throttles - Minimum Practical.
Single FIRE light or Dual when side confirmed:
*2. Throttle affected engine - OFF.
*3. FIRE light affected engine - PUSH.
*4. FIRE EXTGH READY light - PUSH.
*5. HOOK handle - DOWN.
6. Land as soon as possible. (Single Engine Approach and Landing p E32)

Additional steps on E66

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7
Q

L EGT HIGH

A

**EGT HIGH L/R (ENGINE CAUTIONS/ENGINE STALL)***
*1. Throttle affected engine - IDLE
If caution remains at IDLE or engine response is abnormal:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If caution clears:
2. Land as soon as practical.
3. Consider HLF flap approach for landing.

E83

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8
Q

R EGT HIGH

A

**EGT HIGH L/R (ENGINE CAUTIONS/ENGINE STALL)***
*1. Throttle affected engine - IDLE
If caution remains at IDLE or engine response is abnormal:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If caution clears:
2. Land as soon as practical.
3. Consider HLF flap approach for landing.

E83

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9
Q

L FLAMEOUT

A

**FLAMEOUT L/R (ENGINE CAUTIONS/ENGINE STALL)***
SINGLE ENGINE FLAMEOUT
*1. Throttle affected engine - IDLE.
If rpm continues to decrease with increasing EGT (failed auto-restart):
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If engine auto-restarts:
4. Check engine response at a safe altitude.
5. Land as soon as practical.
6. Consider HALF flap approach for landing.

E86

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10
Q

R FLAMEOUT

A

**FLAMEOUT L/R (ENGINE CAUTIONS/ENGINE STALL)***
SINGLE ENGINE FLAMEOUT
*1. Throttle affected engine - IDLE.
If rpm continues to decrease with increasing EGT (failed auto-restart):
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If engine auto-restarts:
4. Check engine response at a safe altitude.
5. Land as soon as practical.
6. Consider HALF flap approach for landing.

E86

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11
Q

L STALL

A

STALL L/R (ENGINE CAUTIONS/ENGINE STALL)**
*1. Throttle affected engine - IDLE.
If stall does not clear:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If stall clears:
2. Check engine response at a safe altitude.
3. Land as soon as practical.

E99

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12
Q

R STALL

A

STALL L/R (ENGINE CAUTIONS/ENGINE STALL)**
*1. Throttle affected engine - IDLE.
If stall does not clear:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If stall clears:
2. Check engine response at a safe altitude.
3. Land as soon as practical.

E99

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13
Q

L IN TEMP

A
  • **IN TEMP L/R (ENGINE CAUTIONS/ENGINE STALL)****
    1. Throttle affected engine - IDLE.
      1. Land as soon as practical.
      2. Consider HALF flap approach for landing.

E91

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14
Q

R IN TEMP

A
  • **IN TEMP L/R (ENGINE CAUTIONS/ENGINE STALL)****
    1. Throttle affected engine - IDLE.
      1. Land as soon as practical.
      2. Consider HALF flap approach for landing.

E91

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15
Q

L OIL PR

A

**OIL PR L/R (ENGINE CAUTIONS/ENGINE STALL)*******
*1. Throttle affected engine - IDLE.
If caution remains after 15 seconds:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If caution clears:
2. Land as soon as practical.
3. Consider HALF flap approach for landing.

E97

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16
Q

R OIL PR

A

**OIL PR L/R (ENGINE CAUTIONS/ENGINE STALL)*******
*1. Throttle affected engine - IDLE.
If caution remains after 15 seconds:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If caution clears:
2. Land as soon as practical.
3. Consider HALF flap approach for landing.

E97

17
Q

L OVRSPD

A

**OVRSPD L/R (ENGINE CAUTIONS/ENGINE STALL)*******
*1. Throttle affected engine - IDLE.
If caution remains at IDLE or engine response is abnormal:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If caution clears:
2. Land as soon as practical.
3. Consider HALF flap approach for landing.

E97

18
Q

R OVRSPD

A

**OVRSPD L/R (ENGINE CAUTIONS/ENGINE STALL)*******
*1. Throttle affected engine - IDLE.
If caution remains at IDLE or engine response is abnormal:
2. Throttle affected engine - OFF.
3. Refer to Single Engine Approach and Landing procedure (p E32).
If caution clears:
2. Land as soon as practical.
3. Consider HALF flap approach for landing.

E97

19
Q

Loss/Fluctuations of Cabin Pressurization

A

**LOSS/FLUCTUATIONS OF CABIN PRESSURIZATION****
If cabin pressure altitude fluctuations exceed a magnitude of 2,000 feet OR loss of cabin pressurization occurs:
OBOGS Aircraft:
*1. Emergency oxygen green ring(s) - PULL
*2. OXY FLOW knob(s) - OFF
Al Aircraft:
*3. Initiate rapid descent to below 10,000 feet MSL.

Additional steps on E57

20
Q

[CABIN]

A

**CABIN CAUTION LIGHT****
BELOW 47,000 FEET MSL
OBOGS Aircraft:
*1. Emergency oxygen green ring(s) - PULL
*2. OXY FLOW knob(s) - OFF
Al Aircraft:
*3. Initiate rapid descent to below 10,000 feet MSL.

Additional steps on E79

21
Q

OBOGS DEGD

A

**OBOGS DEGD CAUTION LIGHT IN FLIGHT***
IN FLIGHT
*1. Emergency oxygen green ring(s) - PULL
*2. OXY FLOW knob(s) - OFF
Al Aircraft:
*3. Initiate rapid descent to below 10,000 feet MSL.

Additional steps on E96

22
Q

Cabin Over-Pressurization (in flight)

A

**CABIN OVER-PRESSURIZED**
GROUND
()1. ECS MODE switch - OFF/RAM.
(
)2. Cabin Temp Knob - FULL COLD
INFLIGHT
OBOGS Aircraft:
*1. Emergency oxygen green ring(s) - PULL.
*2. OXY FLOW knob(s) - OFF.
All aircraft:
*3. Initiate rapid descent to below 10,000 feet MSL.

Additional steps on E58

23
Q

FLAPS OFF
FCS
[FCES]
[FLAPS]

A

**FLAPS OFF CAUTION*******
LEF procedures are dictated by LEF INBOARD position only (irrespective of outboard position).
*1. Maintain airspeed above 300 KCAS and wings level.
2. Visually check LEF deflections.

Additional steps on E110

24
Q

Double Generator or Double Transformer-Rectifier Failure

A

**DOUBLE GENERATOR OR DOUBLE TRANSFORMER-RECTIFIER FAILURE**
If BATT SW caution light not on:
*1. BATT switch - ORIDE

Additional steps on E42

25
DEL ON FCS [FCES]
* ******DEL ON (FLIGHT CONTROL CAUTIONS)******* * 1. Speedbrake - CHECK IN. * 2. Decelerate slowly to below 400 knots/Mach 0.8. Additional steps on E106
26
MECH ON FCS [FCES]
* ******MECH ON (FLIGHT CONTROL CAUTIONS)******* * 1. Speedbrake - CHECK IN. * 2. Decelerate slowly to below 400 knots/Mach 0.8. Additional steps on E113
27
Hot Start
*****************HOT START**************** If EGT climbs rapidly through 750 °C: *1. Throttle affected engine - OFF Additional steps on E1
28
Emergency Catapult Flyaway
***********EMERGENCY CATAPULT FLYAWAY*********** If flyaway airspeed available: *1. Throttles - MAX *2. Rudder - FULL AGAINST YAW/ROLL *3. EMERG JETT button - PUSH *4. Maintain 10° pitch attitude with W symbol. • Do not exceed half lateral stick. WARNING • Inputs in excess of 1/2 lateral stick deflection may result in adverse yaw departure. • Exceeding 10° pitch attitude may result in rapid loss of lateral-directional control. • Raising flaps will increase aircraft settle. If unable to arrest yaw/roll or stop settle: *5. Eject. WARNING Delay in determining controllability will likely place aircraft outside the ejection envelope E61
29
Abort
* ************ABORT************ * 1. Throttles - IDLE * 2. Speedbrake - AS DESIRED * 3. Brakes - APPLY * 4. Stick - AFT below 100 knots (if required) * 5. HOOK handle - DOWN (if required) E61
30
Loss of directional control during takeoff or landing
**********LOSS OF DIRECTIONAL CONTROL DURING TAKEOFF OR LANDING********** If detected after touchdown and flyaway airspeed available: *1. Go Around. If flyaway airspeed not available: *1. EMERG BRK handle - PULL TO DETENT (if required) (p E35). *2. HOOK handle - DOWN (if required) If NWS failure suspected: *3. Paddle switch - PRESS If takeoff is continued and blown tire suspected: 2. LDG GEAR handle - DO NOT CYCLE Additional steps on E21
31
Loss of thrust in takeoff or landing configuration
*********LOSS OF THRUST IN TAKEOFF OR LANDING CONFIGURATION********* WARNING Exceeding 12° AOA (half flaps) or 10° AOA (full flaps) with the good engine in MAX afterburner may lead to loss of lateral and directional control. *1. Throttles - MAX *2. FLAP switch - HALF *3. Maintain on-speed AOA and balanced flight. *4. LDG GEAR handle - UP (if required) *5. EMERG JETT button - PUSH (if required) 6. Refer to Single Engine Approach and Landing procedure (if required) (p E32). E34
32
Planing link failure
***********PLANING LINK FAILURE*********** If detected after touchdown and flyaway airspeed available: *1. Go Around. If flyaway airspeed not available: *1. EMERG BRK handle - PULL TO DETENT (if required) (p E35). *2. HOOK handle DOWN (if required) Additional steps on E20
33
Hypoxia / Decompression Sickness (DCS)
*******HYPOXIA/DECOMPRESSION SICKNESS (DCS) (HYPOXIA/DCS/LOW/NO MASK FLOW)****** IN F/A-18B/D, BOTH AIRCREW SHALL EXECUTE THIS PROCEDURE: *1. Emergency oxygen green ring(s) - PULL *2. OXY FLOW knob(s) or OXYGEN supply lever(s) - OFF *3. Initiate rapid descent to below 10,000 feet MSL. Additional steps on E54
34
Low/No Mask Flow
*******LOW/NO MASK FLOW (HYPOXIA/DCS/LOW/NO MASK FLOW)****** IN FLIGHT *1. Emergency oxygen green ring(s) - PULL *2. OXY FLOW knob(s) or OXYGEN supply lever(s) - OFF *3. Initiate rapid descent to below 10,000 feet MSL. Additional steps on E55
35
Cockpit Smoke, Fumes, or Fire
**********COCKPIT SMOKE, FUMES, OR FIRE************ OBOGS Aircraft: *1. Emergency oxygen green ring(s) - PULL *2. OXY FLOW knob(s) - OFF All Aircraft: *3. Initiate rapid descent to below 10,000 feet MSL. *4. CABIN PRESS switch - RAM/DUMP *5. CABIN TEMP knob - FULL COLD Additional steps on E58a
36
Out of control flight
************OCF RECOVERY PROCEDURES************* *1. Controls - RELEASE, FEET OFF RUDDER, SPEEDBRAKE IN If still out-of-control: *2. Throttles - IDLE *3. Altitude, AOA, airspeed, and yaw rate - CHECK If command arrow present: *4. Lateral stick - FULL WITH ARROW When command arrow removed: *5. Lateral stick - SMOOTHLY NEUTRAL When recovery indicated by AOA and yaw rate tones removed, side forces subsided, and airspeed accelerating above 180 KCAS: *6. Recover. Passing 6,000 feet AGL, dive recovery not initiated: *7. Eject E12
37
Uncommanded Yaw/Roll Excursions
* ***********UNCOMMANDED YAW/ROLL EXCURSIONS********* * 1. Rudder and stick - AGAINST YAW/ROLL Additional steps on E8
38
Brake failure
**********BRAKE FAILURE/EMERGENCY BRAKES******** If detected after touchdown and flyaway airspeed available: *1. Go Around. If brake failure occurs at slow speed or flyaway airspeed not available: *1. Brakes - RELEASE *2. EMERG BRK handle - PULL TO DETENT *3. Brakes - APPLY gradually E35
39
Cabin-Overpressurization (on deck)
**********CABIN OVER-PRESSURIZED********** GROUND (*)1. Do not takeoff. (*)2. ECS MODE switch - OFF/RAM. 3. CABIN TEMP knob - FULL COLD. 4. Delay opening canopy until cabin pressurization dissipates (at least 2 minutes). Additional steps on E58