Date & Time:
Mar 29, 1981 at 0940 LT
Type of aircraft:
Boeing 707
Registration:
OO-SJA
Flight Phase:
Landing (descent or approach)
Flight Type:
Charter/Taxi (Non Scheduled Revenue Flight)
Survivors:
Yes
Schedule:
Brussels - Tenerife
MSN:
17623/78
YOM:
1959
Flight number:
SLR1915
Country:
Belgium
Region:
Europe
Crew on board:
7
Crew fatalities:
0
Pax on board:
110
Pax fatalities:
0
Other fatalities:
0
Total fatalities:
0
Captain / Total hours on type:
3400
Copilot / Total hours on type:
2000
Aircraft flight hours:
64462
Circumstances:
The four engine airplane departed Brussels-Zavantem Airport runway 02 at 0929LT on a charter flight to Tenerife-Sur Reina Sofia with 110 passengers and a crew of seven on board. After takeoff, while climbing to an altitude of 7,000 feet, the engine n°3 exploded and caught fire. The crew declared an emergency and was cleared to return for a landing on runway 25L. longer than runway 02. After the fire was contained and while completing a last turn on final, the airplane was approaching too fast and overshot so the pilot decided to land onto wet runway 25R. After touchdown, reversers on engine n°1 and 4 were activated and the crew initiated an emergency braking procedure. At a speed of about 80 knots, the captain considered the remaining distance as insufficient and decided to steer the aircraft to the left of the runway. The airplane veered off runway, entered a loose soil and came to rest. All 117 occupants were quickly evacuated and there were no casualties. The airplane was damaged beyond repair.
Probable cause:
It was determined that the explosion of the engine n°3 was the consequence of the disintegration of a blade located on the 10th stage of the compressor due to fatigue cracks.
The following contributing factors were identified:
- The approach was completed with one engine inoperative.
- The total weight of the aircraft was above the max allowable weight upon landing.
- The approach speed was too high.
- The crew failed to use the brakes properly.
- Not all available braking options were used.
The following contributing factors were identified:
- The approach was completed with one engine inoperative.
- The total weight of the aircraft was above the max allowable weight upon landing.
- The approach speed was too high.
- The crew failed to use the brakes properly.
- Not all available braking options were used.
Final Report:
OO-SJA.pdf37.38 MB