Blown Tire on Takeoff
Abort or Takeoff?
Airspeed? Distance down runway?
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
Modified abort…
ABORT:
Throttle - IDLE
Speed brakes - EXTEND
BLOWN TIRE SUSPECTED therefore ANTI-SKID Switch - OFF
Hook - DOWN (if required)
Release Brakes prior to crossing arresting gear
Runaway Rudder Trim
TRIM FAILURE
- Attempt to trim from both cockpits
- Airspeed - REDUCE (as practical)
- STBY stabilator trim - NOT REQUIRED
RUDDER TRIM HARDOVER
1. Check rudder trim to confirm full trim
2. Trim until uncommanded trim is removed
if trim is not responding or too slow:
3. CONTR AUG switch - RESET AND RELEASE (rudder goes to neutral)
4. Trim as desired
Runaway Stabilator Trim
TRIM FAILURE
- Attempt to trim from both cockpits
- Airspeed - REDUCE (as practical)
- STBY stabilator trim - AS REQUIRED
Rudder trim hardover
abrupt, small lateral acceleration which occurs with a C AUG caution light. Possible occurrence after a electrical generator reset.
- Check rudder trim to confirm full trim
- Trim until uncommanded trim is removed
if trim is not responding or too slow: - CONTR AUG switch - RESET AND RELEASE (rudder goes to neutral)
- Trim as desired
CONTR AUG’s four functions
Yaw damping
Turn coordination (WoW <217KIAS)
Speed Brake to Stabilator Interconnect (SBI)
Rudder trim
C AUG caution light
C Aug Bit Test is being continuously performed automatically. Light triggered by failed bit test
T/F: THE F405-RR-401 ENGINE INSTALLED DEVELOPS 5,527 POUNDS OF THRUST AT STANDARD SEA-LEVEL CONDITIONS.
TRUE
ENGINE FAILURE DURING CATAPULT LAUNCH.
*1. EJECT
BREAK / LANDING PATTERN PROCEDURES WHEN BASH MODERATE
- Normal traffic pattern altitudes and airspeeds in effect unless specifically restricted
- High initial should be utilized to the maximum extent possible
- Both break altitudes will be available unless otherwise specifically restricted
- Break airspeed should be at or below 300 KIAS
- Single ship solo students will recover via GCA or VFR straight-in
- Single ship solo students will full stop at the discretion of the WDO or RDO
SMOKE/FUMES IN COCKPIT
- Altitude - DESCEND BELOW 18,000’ MSL (if practical)
- AIR FLOW knob - OFF
If unable to clear smoke or unable to see.
- Airspeed - REDUCE (As practical)
- Warn other cockpit occupant/secure loose items
- Seat - LOWER
- MDC firing handle - PULL
- Land as soon as possible
- MDC firing handle - PULL
Flaps fail to retract
- Airspeed - BELOW 200 KIAS
- EMER FLAP switch - DOWN
OR POSSIBLE UNCOMMANDED ROLL/YAW
*1. Flaps/Slats - Return to previous setting.
WARNING: Aircraft exhibits no natural stall warning during approach to stall. Stall warning rudder pedal shakers come on at 21.5 units AOA, closely followed by the stall at 23 to 25 units.
Flaps fail to extend
- Airspeed - BELOW 200 KIAS
- EMER FLAP switch - DOWN
if unable to extend flaps: - Airspeed - FLY ON-SPEED AOA
(pull PCL)
Recommend straight in approach with touchdown not greater than 600 fpm.
Runaway Aileron Trim/Aileron trim failure
Trim Failure
- Attempt to trim from both cockpits
- Airspeed - REDUCE (as practical)
Possible Uncommanded Roll/Yaw
- Flaps/Slats lever - RETURN TO PREVIOUS SETTING
- Controllability check - PERFORM AS REQUIRED
- Land as soon as practical.
- Flaps/Slats lever - RETURN TO PREVIOUS SETTING
Speed brake fails to retract
Controllability check?
Play with C AUG? SBI off?
Speed brakes start to blow back at an airspeed of 380 KIAS and extend fully if the airspeed decreases to 340 KIAS.
Split Flaps
Uncommanded Roll/Yaw
- FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING
- Controllability check - PERFORM AS REQUIRED
- Land as soon as practical.
- FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING
Pitot Static Malfunctions
- PITOT HEAT switch - CHECK ON
- Compare Instruments - BOTH COCKPITS
- AOA - SUBSITUTE FOR AIRSPEED (E49)
- Radar altimeter - USE BELOW 5,000 AGL
- Notify ATC and remain VMC, if possible.
- Join with wingman, if possible
Main/nose gear unsafe down
FAIL TO RETRACT 1. Airspeed below 200 KIAS 2. Ensure EMER GEAR handle fully stowed if light remains on 3. LDG GEAR handle - DOWN, DO NOT CYCLE if any gear indicates unsafe: 5. Execute Landing Gear Unsafe/Fail to Extend procedures
LANDING GEAR UNSAFE/FAIL TO EXTEND
1. Airspeed below 200 KIAS
2. LT/TONE TEST switch - LIGHT TEST
3. Obtain visual check if available
If landing gear cannot be confirmed down and locked and no obvious damage
5. Landing gear - CYCLE
If gear still unsafe
6. LDG GEAR handle - DOWN
7. EMER GEAR handle - ROTATE CLOCKWISE AND PULL
8. If necessary, perform positive-g, negative-g, and yawing maneuvers to obtain a down and locked indication.
9. EMER GEAR handle - Restow
If landing gear remain unsafe:
11. Refer to Landing Gear Malfunction Landing Guide.
