Incident Overview

Date: Saturday 11 May 1985
Aircraft Type: Boeing 737-268 Advanced
Owner/operator: Saudi Arabian Airlines
Location: Doha International Airport (DOH) – ÿ Qatar
Phase of Flight: Take off
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 104
Component Affected: The low-pressure nozzle case, hush package, and fan bypass duct outer case of the second engine.The low-pressure nozzle case, hush package, and fan bypass duct outer case of the second engine.
Category: Accident
A Saudi Arabian Airlines Boeing 737-200 aircraft aborted takeoff from Doha Airport, Qatar, due to a catastrophic failure of the second engine. A fragment penetrated a wing fuel tank, leading to a fire. Passengers and crew evacuated the aircraft, and the airport fire department extinguished the fire. No injuries occurred.A Saudi Arabian Airlines Boeing 737-200 aircraft aborted takeoff from Doha Airport, Qatar, due to a catastrophic failure of the second engine. A fragment penetrated a wing fuel tank, leading to a fire. Passengers and crew evacuated the aircraft, and the airport fire department extinguished the fire. No injuries occurred.

Description

The captain of a Saudi Arabian Airlines Boeing 737-200 airplane aborted a takeoff from Doha Airport, Qatar, following a catastrophic and uncontained failure of the no. 2 engine. A fragment from the engine penetrated a wing fuel tank and the no.2 engine caught fire. The airplane was stopped on the end of the runway, and the 98 passengers and 6 crewmembers evacuated the airplane while the airport fire department extinguished the fire. There were no injuries to the occupants as a result of the engine failure and fire. Investigation of the accident disclosed that the 2nd stage low-pressure turbine (LPT) disk in the Pratt & Whitney JT8D-15 engine ruptured, and that a large segment of the disk exited the engine near the 1:30 o’clock position (aft looking forward). The released segment passed through the engine and caused substantial damage to the low-pressure nozzle case, the hush package and the fan bypass duct outer case. Considerable damage was inflicted on the no.2 engine nacelle by engine fragments and the ensuing fire.

Primary Cause

Rupture of the second stage low-pressure turbine (LPT) disk in the Pratt & Whitney JT8D-15 engine.Rupture of the second stage low-pressure turbine (LPT) disk in the Pratt & Whitney JT8D-15 engine.

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