Zurich – Geneva – Athens – Bombay – Beijing

The approach to runway 15L was unstable. At an excessive speed of 150 knots, the four engine airplane landed about 800-900 meters down the runway 15L, on a wet surface. The crew failed to use all available braking systems and unable to stop within the remaining distance, the airplane overran at a speed of 40 knots, went through a perimeter fence and descended a ravine before coming to rest in flames. 20 passengers were injured while 120 other occupants escaped uninjured. Unfortunately, 14 passengers were killed. The aircraft was totally destroyed by a post crash fire.

Flight / Schedule

Zurich – Geneva – Athens – Bombay – Beijing

Aircraft

Douglas DC-8

Registration

HB-IDE

MSN

45919/312

Year of Manufacture

1967

Operator

Swissair

Date

October 7, 1979 at 09:16 PM

Type

CRASH

Flight Type

Scheduled Revenue Flight

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Athens-Ellinikon Attica / <U+0391>tt<U+03B9><U+03BA><U+03AE>

Region

Europe • Greece

Crash Cause

Human factor

Narrative Report

On October 7, 1979 at 09:16 PM, Zurich – Geneva – Athens – Bombay – Beijing experienced a crash involving Douglas DC-8, operated by Swissair, with the event recorded near Athens-Ellinikon Attica / <U+0391>tt<U+03B9><U+03BA><U+03AE>.

The flight was categorized as scheduled revenue flight and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

154 people were known to be on board, 14 fatalities were recorded, 140 survivors were identified or estimated. This corresponds to an estimated fatality rate of 9.1%.

Crew on board: 10, crew fatalities: 0, passengers on board: 144, passenger fatalities: 14, other fatalities: 0.

The listed crash cause is human factor. The approach to runway 15L was unstable. At an excessive speed of 150 knots, the four engine airplane landed about 800-900 meters down the runway 15L, on a wet surface. The crew failed to use all available braking systems and unable to stop within the remaining distance, the airplane overran at a speed of 40 knots, went through a perimeter fence and descended a ravine before coming to rest in flames. 20 passengers were injured while 120 other occupants escaped uninjured. Unfortunately, 14 passengers were killed. The aircraft was totally destroyed by a post crash fire.

Aircraft reference details include registration HB-IDE, MSN 45919/312, year of manufacture 1967.

Fatalities

Total

14

Crew

0

Passengers

14

Other

0

Crash Summary

The approach to runway 15L was unstable. At an excessive speed of 150 knots, the four engine airplane landed about 800-900 meters down the runway 15L, on a wet surface. The crew failed to use all available braking systems and unable to stop within the remaining distance, the airplane overran at a speed of 40 knots, went through a perimeter fence and descended a ravine before coming to rest in flames. 20 passengers were injured while 120 other occupants escaped uninjured. Unfortunately, 14 passengers were killed. The aircraft was totally destroyed by a post crash fire.

Cause: Human factor

Occupants & Outcome

Crew On Board

10

Passengers On Board

144

Estimated Survivors

140

Fatality Rate

9.1%

Known people on board: 154

Operational Details

Schedule / Flight

Zurich – Geneva – Athens – Bombay – Beijing

Operator

Swissair

Flight Type

Scheduled Revenue Flight

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

Europe • Greece

Aircraft Details

Aircraft

Douglas DC-8

Registration

HB-IDE

MSN

45919/312

Year of Manufacture

1967

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