Air India 787 Crash: Fuel Cutoff Switch Activation After Liftoff

June 12, 2025
Preliminary Report
Wreckage of Air India Flight 171 crash site with emergency personnel walking through debris; large aircraft tail section visible amid rubble and trees. Bold text overlay reads 'AIR INDIA 171 PRELIMINARY REPORT.
Incident Briefing

Air India Flight AI171 Crash – Preliminary Report Summary

Basic Flight and Crash Information

  • Flight: AI171 from Ahmedabad (VAAH) to London Gatwick (EGKK)
  • Date/Time: 12 June 2025, 0809 UTC (13:39 IST)
  • Aircraft: Boeing 787-8, registration VT-ANB, operated by Air India
  • Phase of Flight: Initial Climb
  • Fatalities: All 241 on board (2 flight crew, 10 cabin crew, 229 passengers) and 19 on the ground
  • Wreckage Site: Impacted buildings approx. 0.9 NM from the end of Runway 23, including BJ Medical College hostel

Flight Crew Information

  • Captain: 56-year-old male, ATPL holder, 15,638 hours total time (8,596 on type), fully qualified PIC
  • First Officer: 32-year-old male, CPL holder, 3,403 hours total (1,128 on type), PF for this flight

Aircraft and Maintenance Status

  • Aircraft manufactured in 2013, fully airworthy with all Airworthiness Directives and Service Bulletins complied
  • Active MELs included minor cockpit/cabin systems and one CAT A MEL for nitrogen generation—none deemed contributory
  • Fuel control switch inspections (per FAA SAIB NM-18-33) were not performed, as the directive was advisory only

Accident Sequence Based on EAFR and CVR Data

Normal Takeoff Sequence

  • Pushback at 07:43 UTC; takeoff clearance issued at 08:07:33 UTC
  • Aircraft began takeoff roll at 08:07:37 UTC; rotation speed (Vr) of 155 knots reached at 08:08:35 UTC
  • Aircraft lifted off and transitioned to air mode at 08:08:39 UTC
  • Reached max speed of 180 knots at 08:08:42 UTC

Sudden Engine Shutdown

  • At 08:08:42 UTC, both fuel cutoff switches transitioned from RUN to CUTOFF, one second apart
  • Engine power (N1/N2) began declining due to fuel starvation
  • CVR recorded a pilot asking, “Why did you cut off?” and the other responding, “I did not”
  • RAT (Ram Air Turbine) deployed at 08:08:47 UTC to restore hydraulic power

Attempted Recovery

  • At 08:08:52 UTC: Engine 1 fuel control switch returned to RUN
  • At 08:08:56 UTC: Engine 2 switch also returned to RUN
  • FADEC attempted auto-relight: Engine 1 began recovering; Engine 2 failed to stabilize
  • EGT rise confirmed attempted relight on both engines
  • Mayday call transmitted at 08:09:05 UTC; final data recorded at 08:09:11 UTC
  • Aircraft crashed into residential structures beyond airport perimeter

Investigation Highlights

Wreckage Findings

  • Thrust levers found in idle, but flight data shows they were at takeoff thrust until impact
  • Fuel switches found in RUN, suggesting they were reset prior to crash
  • Gear lever and flaps were in normal takeoff configuration (flaps 5, gear down)

Fuel Switch Design Concern

  • The 787’s fuel switches (Part No. 4TL837-3D) share design with older 737 models
  • Prior advisory (SAIB) warned of locking mechanism issues potentially allowing accidental shutoff
  • Inspections recommended by FAA were not performed by Air India
  • Investigation is exploring inadvertent switch actuation during takeoff due to turbulence or guarding hand contact, however intentional movement of the switches has not been ruled out

Next Steps and Interim Conclusion

  • No safety recommendations yet issued for 787-8 aircraft or GE GEnx-1B engines
  • Investigation ongoing; focus areas include:
    • Engineering review of fuel control switches
    • Detailed aeromedical analysis of crew
    • Analysis of cockpit coordination, workload, and procedure execution
  • Answer the question of “why did the fuel cutoff switches move to the off position?”

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