AIRFRAME INTEGRITY TELEMETRY
TAIL SKID CONTACT DETECTED
Aft bumper sensor tripped at 10.8° pitch during rotation before main gear oleo liftoff extension.
TAKEOFF DYNAMICS & SENSOR DIAGNOSTICS
Critical Strike Pitch Angle:
10.8°
Minimum Runway Tail Clearance:
-4.2 cm
Impact Liftoff Speed:
156 kts
Tail Skid Sensor (Trip):
TRIPPED
Tyre-Pressure Sensor Warning:
WARNING (GEAR ABN)
Cabin Pressurization Delta:
NOMINAL (8.6 PSI)
EMERGENCY RETURN ENVELOPE (MUNICH SCRIPT)
Max Landing Weight (MLW):
207,000 kg
Fuel Burn/Jettison Required:
58,000 kg
Est. Holding Time to MLW:
48 min
Overweight Landing Margin:
+58,000 kg (Overweight)
Recommended Flight Deck Action: Climb to safe holding altitude (FL100-FL140), evaluate structural telemetry, hold/dump fuel to MLW (207,000 kg), perform overweight/normal flap inspection return landing.