I have always been interested in the "What", "When", "When" and "Why" aircraft accidents happen. Even more so now that I work in aviation safety, and am involved in investigations. Thought I would I would start a thread, and I will try and update it daily with an event that happened on that particular day.
Here is the first entry...
June 18, 1972
Operator: British European Airways
Flight: 548
Aircraft Type: Hawker Siddeley HS-121 Trident 1C
SN: G-ARPI
Location: Staines, England
Crew: 9
Passengers: 109
Fatalities: 118
Accident Overview: This was a regularly scheduled passenger flight from London to Brussels. The aircraft took off at 16:08, and per BEA standard practice, the take off was conducted with 20 degrees flap, leading edge slats extended, and the engine thrust set to below full power. After take off the pilot should increase speed to VNA which was 177 knots IAS. Shortly thereafter at approximately 90 seconds after take off, flaps should be brought fully up, and the thrust reduced to noise abatement standards. Once the aircraft reached 3000 ft, the power was to be set, and the leading edge slats retracted, and climb established at 225 knots IAS.
The takeoff started normal, but while passing through 1,750 ft, approximately 114 seconds after take off), and at an airspeed of 162 knots IAS, the co-pilot not on the controls mistakenly retracted the leading edge slats, which put the aircraft near stall speed. Two seconds later the stick shaker stall warning/recovery operated. This caused the auto-pilot to automatically disengage, and the nose to pitch down, increasing airspeed. The elevator trim however stayed at the same setting as they were with the auto-pilot engaged, which was with the leading edge slats extended. This caused the aircraft nose to pitch up rapidly 128 seconds into the flight, and entering a true aerodynamic stall, and then a deep stall. Recovery was not possible at that altitude. The aircraft impacted a field, killing all souls on board.
Probable Cause/Cause:
1. Failure of the PIC to achieve proper altitude and speed during noise abatement procedures.
2. Leading edge slat retraction 60 knots below minimum speed.
3. Failure to monitor speed error, and leading edge slat lever movement.
BE548 before the accident.
Picture Source: UNK
Source: Talk:British European Airways Flight 548 - Wikipedia
Source: Row over pilot medical centre closure
Source: Crash of a BAe Trident in London, UK: 118 killed | Bureau of Aircraft Accidents Archives
Source: Crash of a BAe Trident in London, UK: 118 killed | Bureau of Aircraft Accidents Archives
Source: Crash of a BAe Trident in London, UK: 118 killed | Bureau of Aircraft Accidents Archives
Here is the first entry...
June 18, 1972
Operator: British European Airways
Flight: 548
Aircraft Type: Hawker Siddeley HS-121 Trident 1C
SN: G-ARPI
Location: Staines, England
Crew: 9
Passengers: 109
Fatalities: 118
Accident Overview: This was a regularly scheduled passenger flight from London to Brussels. The aircraft took off at 16:08, and per BEA standard practice, the take off was conducted with 20 degrees flap, leading edge slats extended, and the engine thrust set to below full power. After take off the pilot should increase speed to VNA which was 177 knots IAS. Shortly thereafter at approximately 90 seconds after take off, flaps should be brought fully up, and the thrust reduced to noise abatement standards. Once the aircraft reached 3000 ft, the power was to be set, and the leading edge slats retracted, and climb established at 225 knots IAS.
The takeoff started normal, but while passing through 1,750 ft, approximately 114 seconds after take off), and at an airspeed of 162 knots IAS, the co-pilot not on the controls mistakenly retracted the leading edge slats, which put the aircraft near stall speed. Two seconds later the stick shaker stall warning/recovery operated. This caused the auto-pilot to automatically disengage, and the nose to pitch down, increasing airspeed. The elevator trim however stayed at the same setting as they were with the auto-pilot engaged, which was with the leading edge slats extended. This caused the aircraft nose to pitch up rapidly 128 seconds into the flight, and entering a true aerodynamic stall, and then a deep stall. Recovery was not possible at that altitude. The aircraft impacted a field, killing all souls on board.
Probable Cause/Cause:
1. Failure of the PIC to achieve proper altitude and speed during noise abatement procedures.
2. Leading edge slat retraction 60 knots below minimum speed.
3. Failure to monitor speed error, and leading edge slat lever movement.
BE548 before the accident.
Picture Source: UNK
Source: Talk:British European Airways Flight 548 - Wikipedia
Source: Row over pilot medical centre closure
Source: Crash of a BAe Trident in London, UK: 118 killed | Bureau of Aircraft Accidents Archives
Source: Crash of a BAe Trident in London, UK: 118 killed | Bureau of Aircraft Accidents Archives
Source: Crash of a BAe Trident in London, UK: 118 killed | Bureau of Aircraft Accidents Archives