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EGT/RPM Warning Light or Compressor Stall
- 1. Throttle - Minimum for safe flight
- 2. Controls - NEUTRALIZE
- 3. EGT/RPM - MONITOR
If EGT is greater than 450 oC for more than 6 seconds after throttle IDLE:
4. Execute Airstart
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Fire Warning Light
- GROUND
- 1. Execute Emergency Engine 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
-
GTS Fire Warning Light
- GROUND
- 1. Execute Emergency Shutdown/Egress
- IN-FLIGHT
- 1. ENGINE switch - OFF
-
OIL PRESS Warning Light
- 1. Throttle - Mimimum for safe flight
- 2. Minimize throttle movements
-
OXYGEN warning light
- 1. Emergency oxygen green ring - PULL
- 2. OBOGS FLOW selector - OFF
- 3. Altitude - DESCEND TO LESS THAN 10,000 FEET CABIN ALTITUDE OR MINIMUM SAFE ALTITUDE
-
BRAKE PRESS
1. Suspend Launch
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CANOPY Caution Light
1. CANOPY control lever - CHECK LOCKED
-
TP HOT Caution Light
- GROUND
- 1. Execute Emergency Shutdown/Egress
- IN-FLIGHT
- 1. Throttle - Minimum for safe flight
-
SIM MODE Advisory Procedures
- IN-FLIGHT
- 1. Revert to standby instruments
-
CLEAR ENGINE Procedure
- 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
-
EMERGENCY SHUTDOWN/EGRESS
- 1. Throttle - OFF
- 2. ENGINE switch - OFF
- 3. FUEL SHUTOFF handle - PULL
- 4. Ejection Seats - SAFE
- 5. BATT switches - OFF
-
ABNORMAL START
1. Execute Clear Engine Procedure
-
TAILPIPE FIRE AFTER SHUTDOWN
1. Execute Clear Engine Procedure
-
BRAKE Failure
- If flyaway airspeed available:
- 1. Go around
- If flyaway airspeed not available:
- 2. Throttle - IDLE
- 3. Brakes - RELEASE
- 4. Anit-skid switch - OFF
- 5. Attempt braking
- If brakes still unavailable:
- 6. Hook - DOWN (1,000 feet prior to arresting gear, if required)
- 7. Parking brake handle - PULL, if requried
-
BRAKE FAILURE - AFLOAT
- 1. Throttle - IDLE
- 2. Parking brake handle - PULL
- 3. Hook - DOWN
- 4. Transmit
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ABORT
- 1. Throttle - IDLE
- 2. Speed Brakes - EXTEND
- 3. Brakes - AS REQUIRED
- 4. Hook - DOWN (1,000 feet prior to arresting gear, if required)
- 5. Release brakes prior to crossing the arresting gear
-
AIRCRAFT SETTLING OFF CATAPULT
- 1. Throttle - CHECK FULL FORWARD
- 2. Maintain 24 units AOA
- If settle not stopped:
- 3. Eject
-
ENGINE FAILURE DURING CATAPULT LAUNCH
1. Eject
-
LOSS OF DIRECTIONAL CONTROL
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
-
BLOWN TIRE(S) AT THE CARRIER
1. Gear and flaps - DO NOT REPOSITION
-
ENGINE FAILURE
- If below 1,500 feet AGL and airspeed below 180 KIAS:
- 1. Eject
- If above 1,500 feel AGL or airspeed greater than 180 KIAS:
- 2. Execute airstart
-
UNASSITED AIRSTART (Immediate/Windmill)
- 1. Emergency oxygen green ring -PULL
- 2. Throttle - OFF
- Simultaneously perform steps 3 and 4
- 3. GTS start button - PRESS and HOLD
- 4. Throttle - IDLE
-
ASSISTED AIRSTART
- Below 15,000 feet MSL, 165 - 250 KIAS:
- 1. Throttle - OFF
- 2. GTS - START
- When RPM drops below 20% N2 and GTS advisory light ON:
- 3. ENGINE switch - START
- 4. Throttle - IDLE
-
ELECTRICAL FIRE
1. GEN switch - OFF
-
Elimination of smoke or fumes from cockpit
- 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
-
Hypoxia/OBOGS Contamination
- 1. Emergency oxygen green ring - PULL
- 2. OBOGS FLOW selector - OFF
- 3. Altitude - DESCEND TO LESS THAN 10,000 FEET CABIN ALTITUDE OR MINIMUM SAFE ALTITUDE
-
TOTAL ELECTRICAL FAILURE
1. Emergency oxygen green ring - PULL
-
UNCOMMANDED ROLL/YAW
1. FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING
-
DEPARTURE/SPIN PROCEDURE
- 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 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
-
GINA Failure
1. Revert to standby instruments
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