671
1992-MAR-31 · Istres-Le Tubé Air Base, France

Trans-Air Service — Flight 671

While climbing through FL320 in turbulent conditions, the aircraft's number 4 engine detached from the wing due to fatigue failure of the pylon's forward midspar fitting. As it fell, it struck the number 3 engine, causing it to also detach. Despite a severe fire on the right wing and significant aerodynamic damage, the crew performed an emergency landing at Istres-Le Tubé Air Base. All five occupants survived, though the aircraft was destroyed by the post-landing fire.

Aircraft
Boeing 707-321CH
Registration
5N-MAS
Phase
En Route
Cause
Mechanical Failure
Souls on Board
5
Fatalities
0
Origin → Dest
Luxembourg Findel Airport (LUX) → Mallam Aminu Kano International Airport (KAN)
Report
Success

Investigation Summary

The investigation revealed that the separation was initiated by a fatigue crack in the inboard forward midspar fitting of the No. 4 engine pylon. This crack had likely been present for some time but was not detected during maintenance. The Boeing 707's pylon design was intended to be fail-safe, but the investigation found that the design did not sufficiently account for the effects of corrosion and fatigue on multiple load paths simultaneously. When the No. 4 engine broke away, its trajectory caused it to collide with the No. 3 engine, tearing it from the wing as well. This left the aircraft with no power on the right side and a breached fuel tank, leading to a massive fire. The captain's ability to maintain control of a heavily asymmetric, burning aircraft and land it on a runway is considered a remarkable feat of airmanship.

Final Conclusions

The accident was caused by the separation of the No. 4 engine pylon due to a fatigue crack in the forward midspar fitting that went undetected during inspections. The subsequent loss of the No. 3 engine was a direct result of being struck by the departing No. 4 engine. Contributing factors included the inadequacy of the pylon's fail-safe design under certain fatigue conditions and the difficulty of detecting such cracks with existing maintenance procedures.

Video Analysis

Trans-Air Service Flight 671: Double Engine Separation and Emergency Landing — Analysis of the 1992 Boeing 707 incident where fatigue failure caused both right-wing engines to detach in flight. The crew successfully landed the burning aircraft at Istres-Le Tubé Air Base with no fatalities.

Watch on YouTube ↗

If playback is blocked, the owner has disabled embedding — use the link above.

Systems & Failure Modes

i

Engine Pylon Fittings

The structural components connecting the engine to the wing; the forward midspar fitting failed due to fatigue.

i

Fire Warning System

The system correctly identified fires in the engine nacelle areas, though the engines themselves were no longer attached.

i

Fuel Dumping System

The crew attempted to dump fuel to lighten the aircraft for the emergency landing.

Interesting Facts

  • 01The aircraft was a 28-year-old Boeing 707 that had previously been operated by several airlines including Pan Am.
  • 02The separation occurred during a period of severe turbulence which likely provided the final stress to the fatigued pylon fitting.
  • 03The No. 4 engine struck the No. 3 engine as it fell, causing both to be lost within seconds.
  • 04The landing was performed with the right wing actively on fire and the landing gear extended.
  • 05All 5 people on board (3 crew, 2 passengers) survived without injury.

Safety Actions & Advisories

Pylon Inspection Revision

Source ↗

The BEA recommended more stringent and frequent non-destructive testing (NDT) of Boeing 707 pylon midspar fittings to detect fatigue cracks before they reach critical length.

Fail-Safe Design Review

The investigation prompted a review of the 'fail-safe' certification of older aircraft pylons, ensuring that multiple load path failures are considered in maintenance intervals.

Location

Istres-Le Tubé Air Base, France · 43.5213, 4.9335

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