EPs (BOLDFACE) Flashcards

1
Q

ECT/RPM Warning Light or Compressor Stall

A
  • IN FLIGHT:*
  • Simultaneously perform steps 1 and 2*

1.) Throttle - Minimum for safe flight.

2.) Controls - Neutralize

3.) 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

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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3
Q

GTS FIRE Warning Light

A

GROUND

1.) Execute Emergency Shutdown/Egress

IN-FLIGHT:

1.) Engine switch - OFF

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4
Q

OIL PRESS Warning Light

A

1.) Throttle - Minimum for safe flight.

2.) Minimize throttle movements.

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5
Q

Oxygen Warning Light

A

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

2.) OBOGS FLOW selectors - OFF.

**3.) Altitude - Descend to less than 10,000 feet cabin altitude of minimimum safe altitude. **

  1. ) OBOGS/ANTI-G switch - OFF
  2. ) Land as soon as practical
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6
Q

BRAKE PRESS CAUTION LIGHT

-or-

BRK PRESS

A

Catapult:

1.) Suspend Launch

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7
Q

CANOPY Caution Light

A

1.) CANOPY Control Lever - Check Locked

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8
Q

TP HOT Caution Light

A

GROUND:

1.) Execute Emergency Shutdown / Egress

IN-FLIGHT:

1.) Throttle - Minimum for safe flight

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9
Q

SIM MODE (MFD Display)

A

1.) Revert to Standby Instruments

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10
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

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11
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

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12
Q

Abnormal Start

A

1.) Exectute Clear Engine Procedure

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13
Q

Tailpipe Fire After Shutdown

A

1.) Execute Clear Engine Procedure

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14
Q

BRAKE FAILURE

A

If flyaway airspeed is availableL

1.) Go Around.

If flyaway airspeed not available:

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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15
Q

Brake Failure - Afloat

A

1.) Throttle - IDLE

2.) Parking brake handle - PULL

3.) Hook - DOWN

4.) Transmit

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16
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

4.) Brakes - RELEASE

5.) ANTI-SKID switch - OFF PRIOR TO BRAKING

If airborne:

6.) Gear and Flaps - DO NOT REPOSITION.

17
Q

ABORT

A

1.) Throttle - IDLE

2.) Speed Brakes - Extend

3.) Brakes - As Required

4.) Hook - DOWN (IF REQUIRED)

**5.) Release brakes prior to crossing the arresting gear. **

18
Q

Aircraft Settling Off Catapult

A

1.) Throttle - Check Full Forward

2.) Maintain 24 Units AoA

If settle not stopped:

3.) Eject

19
Q

Engine Failure During Catapult Launch

A

1.) Eject

20
Q

Blown Tire(s) At The Carrier

A

1.) Gear and Flaps - DO NOT REPOSITION

21
Q

Engine Failure

A

If below 1,500 feet AGL and airspeed below 180 KIAS:

1.) Eject

If above 1,500 or airspeed greater than 180 KIAS:

2.) Execute Airstart.

22
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

23
Q

Assisted Airstart

A

Below 15,000 feet MSL, 165 to 250 KIAS

1.) Throttle - OFF

2.) GTS - Start

When RPM drops below 20% N2 and GTS advisory light illuminates

3.) ENGINE swith - START

4.) Throttle - IDLE

24
Q

Electrical Fire

A

1.) GEN switch - OFF

25
Q

Elimination of Smoke or Fumes from Cockpit

A

1.) Altitude - Descend Below 18,000 feet (if practical)

2.) AIR FLOW knob - OFF

If unable to clear smoke or unable to see:

3.) Airspeed - Reduce

4.) Warn other cockpit occupant / secure loose items.

5.) Seat - LOWER

6.) MDC firing handle - PULL

26
Q

Hypoxia / OBOGS contamination

A

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

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

2.) OBOGS FLOW selector(s) - OFF

**3.) Altitude - Descend to less than 10,000 feet cabin altitude or minimum safe altitude. **

  1. ) OBOGS/ANTI-G switch - OFF
  2. ) Land as soon as practical
27
Q

Total Electrical Failure

A

1.) Emergency oxygen green ring - PULL

28
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 conditon probably exists:

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 recover indicated or airpseed increasing through 160 KIAS:

11.) Lateral Stick - Neutralize.

When recovery indicated:

12.) Rudder Pedals SMOOTHLY CENTER.

If out of control passing through 10,000 AGL:

13.) Eject.

30
Q

GINA Failure

A

IN-FLIGHT:

**1.) Revert to standby instruments. **

31
Q

Generator failure

A
  1. ) confirm engine operation
  2. ) GEN sw - Reset