Engine Fire During Start
Throttles - OFF
BATTERY - OFF
Alert ground control of egress if possible before turning off battery
Excessive Hydraulic Pressure (Caution Light Off) (On Ground)
Cycle flight controls once to get rid of air introduced during servicing. If it doesn’t work:
- Throttle gate - DISENGAGE
- Affected engine - SHUT DOWN
Emergency Ground Egress
- Throttle gate - DISENGAGE
- Throttles - OFF
- Notify crewmember of decision to ground egress - AS REQUIRED
*4. ISS mode selector - SOLO (AS REQUIRED)
*5 SAFE/ARMED lever - SAFE - BATTERY switch - OFF
Disconnect belts and harnesses - Visor - DOWN (AS REQUIRED)
- Canopy - OPEN
Cockpit - EXIT
Over-Pressure of Oxygen System (Ground)
> 120 psi
1. Oxygen supply hose(s) hang over side of aircraft
2. Gangload
Over 450 PSI egress the aircraft
Barrier Engagement
- Shoulder harness - LOCK
- Speed Brake - Confirm CLOSED
Prior to BARRIER ENGAGEMENT - Brakes - DISENGAGE (IMMEDIATELY PRIOR TO BARRIER ENGAGEMENT)
- Barrier - ENGAGE IN A THREE-POINT ATTITUDE
Electrical Fire
- Oxygen - 100%
- CABIN PRESS switch - RAM DUMP (BELOW 25,000 FEET, IF POSSIBLE)
- BATTERY and L GEN/R GEN - OFF
- All electrical equipment - OFF
- Batter, generator(s), electrical equipment - ON (AS NECESSARY FOR FLIGHT AND LANDING)
Smoke, fumes, or odors in cockpit (in flight)
- Oxygen - 100%
- Check for fire.
- CABIN PRESS switch - RAM DUMP (BELOW 25,000 FEET, IF POSSIBLE)
- If smoke becomes severe - JETTISON CANOPY (BELOW 300 KCAS, IF POSSIBLE)
B-E-R-A-S-E
Boldface
Engine Failure/Shutdown during Flight checklist
Restart during flight
Alternate gear extension
Single Engine Landing / Go-around (reference)
Ejection Procedure (reference)
Restart during Flight
- Throttle gate - DISENGAGE
- Throttle (affected engine) - OFF (10 SECONDS, IF CONDITIONS PERMIT)
- Altitude - BELOW 25,000 FEET
- Engine RPM - WITHIN AIRSTART ENVELOPE, 12% MIN (18-20% is heart of airstart envelope at all altitudes)
- BATTER switch - ON
- BOOST PUMP switches - CHECK ON
- Engine start and ignition circuit breakers - IN (LEFT CONSOLE IN THE FCP)
- ENGINE START button (affected engine) - PUSH
- Throttle - ADVANCE TO IDLE.
Give it 30 seconds in idle before aborting start.
If restart fails, try it with CROSSFEED switch - ON
Compressor Stall
- Throttle - IDLE
- ENGINE START button - PRESS
- Increase/decrease airspeed as necessary
- EGT/RPM - MONITOR
If engine will not restart or recover, engine shutdown in flight.
Abrupt and Uncommanded Aircraft Pitch-Up Flaps Extended
- Control stick - FULL FORWARD TO ARREST PITCH RATE
- Throttles - MAX
- FLAPS - 60%
- Landing gear - UP WHEN CONTINUED FLIGHT IS ASSURED
- FLAPS - UP WHEN THE AIRCRAFT ACCELERATES ABOVE NO FLAP FLYING AIRPSEED. (BE PREPARED TO RELAX FORWARD STICK FORCE AS FLAPS ARE RETRACTED)
- Land with flaps retracted.
Trim Malfunction
In case of a runaway or uncontrollable trim -
- Trim button - Hold in opposite direction
- Associated circuit breaker - PULL (Front cockpit pedestal, left column, second from bottom)
Ejection Procedure (Full)
Notify crewmembers and confirm seat is armed and unpinned, at ISS is set correctly (BOTH).
Select IFF EMERGENCY and transmit distress call
Obtain safe ejection conditions:
a. 200-300 KCAS
b. 2,000 - 4,000’ AGL; 2,000 minimum
c. Wings level, slightly climbing
Stow loose equipment, put visor down, fasten oxygen max and helmet chin strap, lock inertial reel lever and tighten leg straps.
Turn aircraft toward uninhabited area, assume the proper body position, and eject. (Sitting erect, spine straight, head agains seat pad firmly, elbows close to body, extend legs forward until weight of thighs is in the seat, but legs not rigid)
Loss of Canopy
- Airspeed - SLOW TO BELOW 300 KCAS (minimum drag occurs at 225 KCAS)
- Reestablish intercockpit comms
- Land as soon as practical.
Alternate Gear Extension
Airspeed 240 or less, flaps as required
Open gear doors
Landing gear lever down
Ldg gear alternate release handle, pull 10 inches, then stow handle.
