Primary Flight Data
IAS (Airspeed): 110 kts
Altitude: 3500 ft
AoA (Alpha): 14.5°
VSI (Vert Speed): -1200 fpm
G-Load: 0.85 G
Force Vectors
Lift Force ($C_L$)
Drag Force ($C_D$)
Thrust Vector
Relative Wind
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Incident Telemetry Black Box Scrubber
Scenario: High AoA Aerodynamic Stall during Steep Climb
00:00.0
Aerodynamic Envelope ($C_L$ vs AoA)
C_L: 1.42 | C_D: 0.28
Stall Alpha ($\alpha_{crit}$): 15.0°
Post-Stall Hysteresis: Active
Manual Pilot Control Yoke
Pitch & Roll Overrides
Virtual Control Yoke (Click/Drag)
Throttle Input:
85%
Elevator Deflection:
0.60
Rudder Yaw Deflection:
0.00