T-45 Eps

Front 1

EGT/RPM WARNING LIGHT OR COMPRESSOR STALL

Back 1

IN-FLIGHT
Simultaneously:
1. Throttle- Minimum for safe flight
2. Controls - Neutralize
3. EGT/RPM - Monitor
If EGT is greater that 450 for more than 6 seconds after throttle IDLE:
4. Execute Airstart

Front 2

FIRE WARNING LIGHT

Back 2

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

Front 3

GTS FIRE WARNING LIGHT

Back 3

GROUND
1. Execute Emergency Shutdown/Egress
IN-FLIGHT
1. Engine Switch - OFF

Front 4

OIL PRESS WARNING LIGHT

Back 4

1. Throttle - Minimum for safe flight
2. Minimize throttle movements

Front 5

OXYGEN WARNING LIGHT

Back 5

1. Emergency oxygen green ring - PULL
2. OBOGS FLOW selector - OFF
3. Altitude - DESCEND TO LESS THAN 10,000 FT CABIN ALTITUDE OR MINIMUM SAFE ALTITUDE

Front 6

BRK PRESS

Back 6

1. Suspend Launch

Front 7

CANOPY CAUTION LIGHT

Back 7

1. CANOPY control lever - CHECK LOCKED

Front 8

TP HOT CAUTION LIGHT

Back 8

GROUND
1. Execute Emergency Shutdown/Egress
IN-FLIGHT
1. Throttle minimum for safe flight

Front 9

SIM MODE ADVISORY PROCEDURES

Back 9

IN-FLIGHT
1. Revert to standby instruments

Front 10

CLEAR ENGINE PROCEDURE

Back 10

1. Throttle - OFF
2. ENGINE switch - 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

Front 11

EMERGENCY SHUTDOWN/EGRESS

Back 11

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

Front 12

ABNORMAL START

Back 12

1. Execute Clear Engine Procedure

Front 13

TAILPIPE FIRE AFTER SHUTDOWN

Back 13

1. Execute Clear Engine Procedure

Front 14

BRAKE FAILURE

Back 14

If flyaway airspeed available:
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 (1,000 ft prior to arresting gear, if required)
7. Parking brake handle - PULL, if required

Front 15

BRAKE FAILURE - AFLOAT

Back 15

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

Front 16

ABORT

Back 16

1. Throttle - IDLE
2. Speed Brakes - EXTEND
3. Brakes - AS REQUIRED
4. Hook - DOWN (1,000 ft prior to arresting gear, if required)
5. Release brakes prior to crossing the arresting gear

Front 17

AIRCRAFT SETTLING OFF CATAPULT

Back 17

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

Front 18

ENGINE FAILURE DURING CATAPULT LAUNCH

Back 18

1. Eject

Front 19

LOSS OF DIRECTIONAL CONTROL

Back 19

1. Rudder - AS REQUIRED TO COUNTER SWERVE
If flyaway airspeed available:
2. Go-around
If fly away 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

Front 20

BLOWN TIRE(S) AT THE CARRIER

Back 20

1. Gear and Flaps - DO NOT REPOSITION

Front 21

ENGINE FAILURE

Back 21

If below 1,500 ft AGL and airspeed below 180 KIAS:
1. Eject
If above 1,500 ft AGL or airspeed greater than 180 KIAS:
2. Execute Airstart

Front 22

UNASSISTED AIRSTART (Immediate/Windmill)

Back 22

1. Emergency oxygen green ring - PULL
2. Throttle - OFF
Simultaneously:
3. GTS start button - PRESS AND HOLD
4. Throttle - IDLE

Front 23

ASSISTED AIRSTART

Back 23

Below 15,000 ft MSL, 165 to 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

Front 24

ELECTRICAL FIRE

Back 24

1. GEN switch - OFF

Front 25

ELIMINATION OF SMOKE OR FUMES IN THE COCKPIT

Back 25

1. Altitude - DESCEND BELOW 18,000 FT (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

Front 26

HYPOXIA/OBOGS CONTAMINATION

Back 26

1. Emergency oxygen green ring - PULL
2. OBOGS FLOW selector - OFF
3. Altitude - DESCEND TO LESS THAN 10,000 FT CABIN ALTITUDE OR MINIMUM SAFE ALTITUDE

Front 27

TOTAL ELECTRICAL FAILURE

Back 27

1. Emergency oxygen green ring - PULL

Front 28

UNCOMMANDED ROLL/YAW

Back 28

1. FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING

Front 29

DEPARTURE/SPIN PROCEDURE

Back 29

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)
5. Rudder pedal - FULL OPOSITE OF TURN NEEDLE
6. Lateral stick - FULL OPPOSITE OF TURN NEEDLE
7. Longitudinal stick - NEUTRALIZE
UPRIGHT (AOA above 28)
8. Rudder pedal - FULL OPOSITE OF 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 ft AGL:
13. Eject

Front 30

GINA FAILURE

Back 30

IN-FLIGHT
1. Revert to standby instruments