Abort Start Procedure
PCL - OFF; or
Starter switch - AUTO/RESET
Emergency Engine Shutdown on the Ground
1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL
3. Emergency ground egress - As required
Emergency Ground Egress
1. ISS MODE SELECTOR - SOLO
2. SEAT SAFETY PIN - INSTALL (BOTH)
3. PARKING BRAKE - AS REQUIRED
4. CANOPY - OPEN
Emergency Ground Egress (IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS)
5. CFS HANDLE SAFETY PIN - REMOVE (BOTH) (USAF ONLY)
6. CFS HANDLE - ROTATE AND PULL (BOTH)
7. SHOULDER STRAPS, LAP STRAPS, AND LEG RESTRAINT GARTERS - RELEASE BOTH
8. BAT, GEN, AND AUX BAT SWITCHES - OFF
9. EVACUATE AIRCRAFT
ABORT
1. PCL - IDLE
2. BRAKES - AS REQUIRED
Engine Failure Immediately After Takeoff (Sufficient runway remaining straight ahead)
1. AIRSPEED - 110 KNOTS (MINIMUM)
2. PCL - AS REQUIRED
3. EMER LDG GR HANDLE - PULL (AS REQUIRED)
4. FLAPS - AS REQUIRED
Engine Failure During Flight
1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)
2. PCL - OFF
3. INTERCEPT ELP
4. AIR START ATTEMPT (IF WARRANTED)
IF CONDITIONS DO NOT WARRANT AN AIR START
5. FIREWALL SHUTOFF HANDLE - PULL
6. EXECUTE FORCE LANDING OR EJECT
IMMEDIATE AIRSTART
1. PCL - OFF
2. STARTER SWITCH - AUTO/RESET
3. PCL - IDLE, ABOVE 13% N1
4. ENGINE INSTRUMENTS - MONITOR ITT, N1, AND OIL PRESSURE
IF AIRSTART IS UNSUCCESSFUL:
5. PCL - OFF
6. FIREWALL SHUTOFF HANDLE - PULL
7. EXECUTE FORCED LANDING OR EJECT
IF AIRSTART SU
UNCOMMANDED POWER CHANGES/LOSS OF POWER/ UNCOMMANDED PROPELLER FEATHER
1. PCL - MID RANGE
2. PMU SWITCH - OFF
3. PROP SYS CIRCUIT BREAKER (LEFT FRONT CONSOLE) - PULL, IF Np STABLE BELOW 40%
4. PCL - AS REQUIRED
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
5. PEL - EXECUTE
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
6. PROP SYS
COMPRESSOR STALLS
1. PCL - SLOWLY RETARD BELOW STALL THRESHOLD
2. DEFOG SWITCH - ON
3. PCL - SLOWLY ADVANCE (AS REQUIRED)
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
4. PEL - EXECUTE
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
5. PCL - OFF
6. FIREWALL SHUTOFF HANDLE - PULL
INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT
1. PCL - IDLE
2. CONTROLS - NEUTRAL
3. ALTITUDE - CHECK
4. RECOVER FROM UNUSUAL ATTITUDE
FIRE IN FLIGHT (FIRE ANNUNCIATOR ILLUMINATED)
IF FIRE IS CONFIRMED:
1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL
IF FIRE IS EXTINGUISHED:
3. FORCED LANDING - EXECUTE
IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL:
4. EJECT (BOTH)
IF FIRE IS NOT CONFIRMED:
5. PEL - EXECUTE
CHIP DETECTOR WARNING
1. PCL - MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
2. PEL - EXECUTE
OIL SYSTEM MALFUNCTION OR LOW OIL PRESSURE
IF ONLY AMBER OIL PX ANNUNCIATOR ILLUMINATES:
1. TERMINATE MANEUVER
2. CHECK OIL PRESSURE; IF OIL PRESSURE IS NORMAL, CONTINUE OPERATIONS
IF RED OIL PX ANNUNCIATOR ILLUMINATES AND/OR AMBER PX ANNUNCIATOR REMAINS ILLUMINATED FOR 5 SECONDS:
3. PCL- MINIMUM
LOW FUEL PRESSURE
1. PEL - EXECUTE
2. BOOST PUMP - ON
OBOGS FAIL ANNUNCIATOR
1. PCL - ADVANCE
OBOGS FAILURE/PHYSIOLOGICAL SYMPTOMS
1. GREEN RING - PULL (AS REQUIRED) (BOTH)
2. DESCENT BELOW 10,000 FEET MSL - INITIATE
3. DISCONNECT MAIN OXYGEN SUPPLY HOSE FROM CRU-60/P
EJECT
1. EJECTION HANDLE - PULL (BOTH)
FORCED LANDING
1. AIRSPEED - 125KIAS PRIOR TO EXTENDING LANDING GEAR
2. EMER LDG GR HANDLE - PULL (AS REQUIRED)
3. AIRSPEED 120 KIAS MINIMUM UNTIL INTERCEPTING FINAL; 110 KIAS MINIMUM ON FINAL
4. FLAPS - AS REQUIRED
PRECAUTIONARY EMERGENCY LANDING (PEL)
1. TURN TO NEAREST SUITABLE FIELD
2. CLIMB OR ACCELERATE TO INTERCEPT ELP
3. GEAR, FLAPS, SPEED BRAKE - UP
SMOKE AND FUME ELIMINATION/ELECTRICAL FIRE
1. OBOGS - CHECK (BOTH)
a. OBOGS Supply Lever - ON
b. OBOGS concentration Lever - MAX
c. OBOGS pressure Lever - EMERGENCY
Abort Start Procedure
PCL - OFF; or
Starter switch - AUTO/RESET
Emergency Engine Shutdown on the Ground
1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL
3. Emergency ground egress - As required
Emergency Ground Egress
1. ISS MODE SELECTOR - SOLO
2. SEAT SAFETY PIN - INSTALL (BOTH)
3. PARKING BRAKE - AS REQUIRED
4. CANOPY - OPEN
Emergency Ground Egress (IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS)
5. CFS HANDLE SAFETY PIN - REMOVE (BOTH) (USAF ONLY)
6. CFS HANDLE - ROTATE AND PULL (BOTH)
7. SHOULDER STRAPS, LAP STRAPS, AND LEG RESTRAINT GARTERS - RELEASE BOTH
8. BAT, GEN, AND AUX BAT SWITCHES - OFF
9. EVACUATE AIRCRAFT
ABORT
1. PCL - IDLE
2. BRAKES - AS REQUIRED
Engine Failure Immediately After Takeoff (Sufficient runway remaining straight ahead)
1. AIRSPEED - 110 KNOTS (MINIMUM)
2. PCL - AS REQUIRED
3. EMER LDG GR HANDLE - PULL (AS REQUIRED)
4. FLAPS - AS REQUIRED
Engine Failure During Flight
1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)
2. PCL - OFF
3. INTERCEPT ELP
4. AIR START ATTEMPT (IF WARRANTED)
IF CONDITIONS DO NOT WARRANT AN AIR START
5. FIREWALL SHUTOFF HANDLE - PULL
6. EXECUTE FORCE LANDING OR EJECT
IMMEDIATE AIRSTART
1. PCL - OFF
2. STARTER SWITCH - AUTO/RESET
3. PCL - IDLE, ABOVE 13% N1
4. ENGINE INSTRUMENTS - MONITOR ITT, N1, AND OIL PRESSURE
IF AIRSTART IS UNSUCCESSFUL:
5. PCL - OFF
6. FIREWALL SHUTOFF HANDLE - PULL
7. EXECUTE FORCED LANDING OR EJECT
IF AIRSTART SU
UNCOMMANDED POWER CHANGES/LOSS OF POWER/ UNCOMMANDED PROPELLER FEATHER
1. PCL - MID RANGE
2. PMU SWITCH - OFF
3. PROP SYS CIRCUIT BREAKER (LEFT FRONT CONSOLE) - PULL, IF Np STABLE BELOW 40%
4. PCL - AS REQUIRED
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
5. PEL - EXECUTE
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
6. PROP SYS
COMPRESSOR STALLS
1. PCL - SLOWLY RETARD BELOW STALL THRESHOLD
2. DEFOG SWITCH - ON
3. PCL - SLOWLY ADVANCE (AS REQUIRED)
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
4. PEL - EXECUTE
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
5. PCL - OFF
6. FIREWALL SHUTOFF HANDLE - PULL
INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT
1. PCL - IDLE
2. CONTROLS - NEUTRAL
3. ALTITUDE - CHECK
4. RECOVER FROM UNUSUAL ATTITUDE
FIRE IN FLIGHT (FIRE ANNUNCIATOR ILLUMINATED)
IF FIRE IS CONFIRMED:
1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL
IF FIRE IS EXTINGUISHED:
3. FORCED LANDING - EXECUTE
IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL:
4. EJECT (BOTH)
IF FIRE IS NOT CONFIRMED:
5. PEL - EXECUTE
CHIP DETECTOR WARNING
1. PCL - MINIMUM NECESSARY TO INTERCEPT ELP; AVOID UNNECESSARY PCL MOVEMENTS
2. PEL - EXECUTE
OIL SYSTEM MALFUNCTION OR LOW OIL PRESSURE
IF ONLY AMBER OIL PX ANNUNCIATOR ILLUMINATES:
1. TERMINATE MANEUVER
2. CHECK OIL PRESSURE; IF OIL PRESSURE IS NORMAL, CONTINUE OPERATIONS
IF RED OIL PX ANNUNCIATOR ILLUMINATES AND/OR AMBER PX ANNUNCIATOR REMAINS ILLUMINATED FOR 5 SECONDS:
3. PCL- MINIMUM
LOW FUEL PRESSURE
1. PEL - EXECUTE
2. BOOST PUMP - ON
OBOGS FAIL ANNUNCIATOR
1. PCL - ADVANCE
OBOGS FAILURE/PHYSIOLOGICAL SYMPTOMS
1. GREEN RING - PULL (AS REQUIRED) (BOTH)
2. DESCENT BELOW 10,000 FEET MSL - INITIATE
3. DISCONNECT MAIN OXYGEN SUPPLY HOSE FROM CRU-60/P
EJECT
1. EJECTION HANDLE - PULL (BOTH)
FORCED LANDING
1. AIRSPEED - 125KIAS PRIOR TO EXTENDING LANDING GEAR
2. EMER LDG GR HANDLE - PULL (AS REQUIRED)
3. AIRSPEED 120 KIAS MINIMUM UNTIL INTERCEPTING FINAL; 110 KIAS MINIMUM ON FINAL
4. FLAPS - AS REQUIRED
PRECAUTIONARY EMERGENCY LANDING (PEL)
1. TURN TO NEAREST SUITABLE FIELD
2. CLIMB OR ACCELERATE TO INTERCEPT ELP
3. GEAR, FLAPS, SPEED BRAKE - UP
SMOKE AND FUME ELIMINATION/ELECTRICAL FIRE
1. OBOGS - CHECK (BOTH)
a. OBOGS Supply Lever - ON
b. OBOGS concentration Lever - MAX
c. OBOGS pressure Lever - EMERGENCY