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Pedal Turn
- 1) Clean above 18000'
- 2) Slow to 22 units AOA
- 3) MRT, Hold 22 units AOA
- 4) 30 AOB using rudder only
- 5) Reverse direction using rudder to 30 AOB other direction
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High AOA Deep Stall Investigation
- 1) Clean above 20000'
- 2) IDLE, slow to 20 units AOA
- 3) Slowly increase to 24-26 units AOA
- 4) At 28-30 units, a/s approaching 110-120 (Full stall - aileron effectiveness marginal)
- 5) Recover using OCF procedures
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70o Nose High Departure
- 1) 300 KIAS, above 14000'
- 2) Pull to 17 units
- 3) Establish 70 nose up on ADI
- 4) IDLE at 150 KIAS
- 5) Increase back stick to hold 70 nose up
- 6) When full aft, unable to maintain 70 up, recover using OCF procedures
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110o Nose High Departure
- 1) 350 KIAS, above 14000'
- 2) Pull to 17 units
- 3) Establish 110 nose up on ADI
- 4) IDLE at 150 KIAS
- 5) Increase forward stick to hold 110 nose up
- 6) When full forward, unable to maintain 110 up, recover using OCF procedures
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90o Nose High Departure
- 1) 300-350 KIAS, above 14000'
- 2) Pull to 17 units
- 3) Establish 90 nose up on ADI
- 4) IDLE at 150 KIAS
- 5) Maintain 90 nose up
- 6) When a/s decreases below 85 KIAS, recover using OCF procedures
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Lateral Stick Adverse Yaw Departure
- 1) 275 KIAS, 15o nose up
- 2) 80 - 90 AOB
- 3) IDLE
- 4) At 250 KIAS, full aft stick 28-30 units AOA
- 5) Reverse direction with full opposite aileron and maintain full aft stick
- 6) A/C should depart opposite applied aileron
- 7) Recover using OCF procedures
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When to execute:
Overhead Stuck Throttle Approach
Straight-in Stuck Throttle Approach
Overhead: less than 300 KIAS, 88-89%, 1700pph
Straight-in: greater than 300 KIAS, 88-89%, 1700pph
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Stuck Throttle Approach
- 1) Throttle - do not attempt to reset
- 2) Altitude - stabilize at 10K MSL if practical
- 3) Anti-Skid - Off
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Straight-in Stuck Throttle Approach
1) A/S - below 200 KIAS using SB, nose att, and load factor
2) LG, flaps, and SB - as required to maintain a/s below 200 KIAS
3) 3o glideslope (300' / mile)
4) No lower than on-speed, attempt short-field arrestment, if available
5) A/S above 150 KIAS, FSOH pull at calculated altitude
6) A/S below 150 KIAS, FSOH pull at touchdown
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Calculated FSOH shutdown altitude
- 50' AGL - 160 KIAS
- 100' AGL - 170 KIAS
- 150' AGL - 180 KIAS
- 200' AGL - 190 KIAS
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Overhead Stuck Throttle
1) A/S - below 200 KIAS using SB, nose att, and load factor
2) LG, flaps, and SB - as required to maintain a/s below 200 KIAS
3) Execute Overhead PA, attempt short field arrestment
4) When established in landing flare - FSOH pull
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