London – Luqa

The Viscount was taxiing along the runway after landing when a hydraulic system pressure loss occurred. Wheel brakes and nosewheel steering were inoperative and the plane left the runway, rolling down an area of downslope. Because of the hydraulic system pressure loss an attempt by the pilot to raise the gear, failed. The aircraft came to rest against the control tower. Investigation revealed a fractured pipe line and faulty operation of a non-return valve intended to conserve pressure if there were a pressure loss in the main hydraulic system. Source: https://aviation-safety.net/database/record.php?id=19600105-0

Flight / Schedule

London – Luqa

Registration

G-AMNY

MSN

6

Year of Manufacture

1953

Date

January 5, 1960 at 12:00 AM

Type

CRASH

Flight Type

Scheduled Revenue Flight

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Luqa All Malta

Region

Europe • Malta

Crash Cause

Technical failure

Narrative Report

On January 5, 1960 at 12:00 AM, London – Luqa experienced a crash involving Vickers Viscount, operated by British European Airways - BEA, with the event recorded near Luqa All Malta.

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.

51 people were known to be on board, 0 fatalities were recorded, 51 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 5, crew fatalities: 0, passengers on board: 46, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is technical failure. The Viscount was taxiing along the runway after landing when a hydraulic system pressure loss occurred. Wheel brakes and nosewheel steering were inoperative and the plane left the runway, rolling down an area of downslope. Because of the hydraulic system pressure loss an attempt by the pilot to raise the gear, failed. The aircraft came to rest against the control tower. Investigation revealed a fractured pipe line and faulty operation of a non-return valve intended to conserve pressure if there were a pressure loss in the main hydraulic system. Source: https://aviation-safety.net/database/record.php?id=19600105-0

Aircraft reference details include registration G-AMNY, MSN 6, year of manufacture 1953.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

The Viscount was taxiing along the runway after landing when a hydraulic system pressure loss occurred. Wheel brakes and nosewheel steering were inoperative and the plane left the runway, rolling down an area of downslope. Because of the hydraulic system pressure loss an attempt by the pilot to raise the gear, failed. The aircraft came to rest against the control tower. Investigation revealed a fractured pipe line and faulty operation of a non-return valve intended to conserve pressure if there were a pressure loss in the main hydraulic system. Source: https://aviation-safety.net/database/record.php?id=19600105-0

Cause: Technical failure

Occupants & Outcome

Crew On Board

5

Passengers On Board

46

Estimated Survivors

51

Fatality Rate

0.0%

Known people on board: 51

Operational Details

Schedule / Flight

London – Luqa

Flight Type

Scheduled Revenue Flight

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

Europe • Malta

Aircraft Details

Registration

G-AMNY

MSN

6

Year of Manufacture

1953

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