EPs

Question 1

COMPRESSOR STALL

Answer 1

In-Flight
1. Throttle - IDLE
2. EGT/RPM - CHECK
If EGT is greater than 450*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.

Question 2

EGT/RPM WARNING LIGHT

Answer 2

In-Flight
1. Throttle - IDLE
2. EGT/RPM - CHECK
If EGT is greater than 450*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.

Question 3

FIRE WARNING LIGHT

Answer 3

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.

Question 4

GTS FIRE WARNING LIGHT

Answer 4

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

Question 5

OIL PRESS WARNING LIGHT

Answer 5

1. Throttle - MINIMUM FOR SAFE FLIGHT.

2. Minimize throttle movements.

Question 6

OXYGEN WARNING LIGHT

Answer 6

AFTER TAKEOFF:
1. Throttle – Increase N2 RPM above 75%
(80% above FL300)

Question 7

BRK PRESS CAUTION LIGHT CATAPULT

Answer 7

1. Suspend launch

Question 8

CANOPY CAUTION LIGHT

Answer 8

1. CANOPY control lever - CHECK LOCKED.

Question 9

SKID CAUTION LIGHT

Answer 9

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

Question 10

TP HOT CAUTION LIGHT

Answer 10

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

Question 11

CLEAR ENGINE PROCEDURE

Answer 11

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

Question 12

ABNORMAL START

Answer 12

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

Question 13

TP FIRE ON SHUTDOWN

Answer 13

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

Question 14

EMERGENCY SHUTDOWN/EGRESS

Answer 14

1. Throttle - OFF
2. ENGINE switch - OFF
3. FUEL SHUTOFF handle - PULL
4. Ejection seats - SAFE
5. BATT switches - OFF

Question 15

BRAKE FAILURE - ASHORE

Answer 15

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. Attept braking.
If brakes still unavailable:
6. Hook - DOWN (if required)
7. Parking brake handle - PULL (if required)

Question 16

BRAKE FAILURE - AFLOAT

Answer 16

1. Throttle - IDLE
2. Parking brake handle - PULL
3. Hook - DOWN
4. Transmit

Question 17

LOSS OF DIRECTIONAL CONTROL

Answer 17

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.

Question 18

ABORT

Answer 18

1. Throttle - IDLE
2. Speed brakes - EXTEND
3. Brakes - APPLY
4. Hook - DOWN (if required)
5. Release brakes prior to crossing the arresting gear.

Question 19

EMERGENCY CATAPULT FLYAWAY

Answer 19

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

Question 20

BLOWN TIRE(S) AT THE CARRIER

Answer 20

1. Gear and flaps - DO NOT REPOSITION.

Question 21

ENGINE FAILURE

Answer 21

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.

Question 22

AIRSTART

Answer 22

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.

Question 23

ELECTRICAL FIRE

Answer 23

GEN switch - OFF

Question 24

SMOKE OR FUMES IN THE COCKPIT

Answer 24

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:
2. Airspeed - REDUCE (as practical)
3. Warn other cockpit occupant/secure loose items.
4. Seat - LOWER
5. MDC firing handle - PULL.

Question 25

LOW/NO MASK FLOW (IN FLIGHT)

Answer 25

FLIGHT: 1. Throttle – Increase N2 RPM above 75% (80% above FL 300) If no mask flow or low mask flow continues 10 seconds after increasing RPM and cabin altitude above 10,000 ft: 2. Emergency oxygen green ring(s) – PULL 3. OBOGS FLOW selector(s) – OFF

Question 26

TOTAL ELECTRICAL FAILURE

Answer 26

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

Question 27

UNCOMMANDED ROLL/YAW

Answer 27

1. FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING.

Question 28

DEPARTURE/SPIN PROCEDURE

Answer 28

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 160KAIS: 11. Lateral stick - NEUTRALIZE. When recovery indicated: 12. Rudder pedals - SMOOTHLY CENTER. If out of control passing through 10,000 feet AGL: 13. EJECT

Question 29

PCL Only ENGINE FAILURE DURING CATAPULT LAUNCH

Answer 29

1. EJECT.

Question 30

CABIN ALT WARNING LIGHT

Answer 30

IN-FLIGHT: | 1. Mask – ON/TIGHT

Question 30

RAPID DECOMPRESSION

Answer 30

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

Question 31

ADVERSE PHYSIOLOGICAL SYMPTOMS

Answer 31

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