Estado: | Accident investigation report completed and information captured |
Fecha: | viernes 10 septiembre 1976 |
Hora: | 10:14 |
Tipo: |  Hawker Siddeley HS-121 Trident 3B |
Operador: | British Airways |
Registración: | G-AWZT |
Numéro de série: | 2320 |
Año de Construcción: | 1972 |
Horas Totales de la Célula: | 8627 |
Ciclos: | 6952 |
Motores: | 3 Rolls-Royce Spey 512-5W |
Tripulación: | Fatalidades: 9 / Ocupantes: 9 |
Pasajeros: | Fatalidades: 54 / Ocupantes: 54 |
Total: | Fatalidades: 63 / Ocupantes: 63 |
Víctimas de la colisión: | Fatalidades: 113 |
Daños en la Aeronave: | Destruido |
Consecuencias: | Written off (damaged beyond repair) |
Ubicación: | cerca Vrbovec ( Croacia)
|
Fase: | En ruta (ENR) |
Naturaleza: | Vuelo Internacional Programado |
Aeropuerto de Salida: | London-Heathrow Airport (LHR/EGLL), Reino Unido |
Aeropuerto de Llegada: | Istanbul-Yesilköy Airport (IST/LTBA), Turquía |
Número de Vuelo: | BE476 |
Descripción:Hawker Siddeley HS-121 Trident 3B operated by British Airways as flight BE476 and a McDonnell Douglas DC-9-32, operated by Inex-Adria Aviopromet, were destroyed when both aircraft crashed near Vrobec following a mid-air collision. All 176 on board both aircraft were killed.
The Trident was on a scheduled flight from London-Heathrow Airport in England to Istanbul-Yesilköy Airport in Turkey, carrying 54 passengers and a crew of 9. The aircraft took off at 08:32 GMT and the flight proceeded normally. First contact with the Zagreb Area Control Centre was established on the Upper Sector frequency 134,45 MHz at 10:04 GMT. The flight was requested to report passing the Zagreb VOR at flight level 330.
The aircraft flew along the centreline of airway UB5 with slight side deviation 1-2 km to the right due to wind. At 2 minutes and 50 seconds before the collision, the aircraft changed heading to 115° to head back towards the airway centreline. Airspeed was 295 Kts.
The DC-9 departed Split Airport at 09:48 GMT to fly 108 West German tourists back to Cologne. Flight JP550 was issued instructions to climb to FL180.
At 09:54 the flight, on passing flight level 130, switched to the Zagreb Area Control Centre lower sector east frequency of 124.6 MHz, receiving clearance to climb to FL240 and later to FL260.
At 10:03 the crew switched to the frequency of the middle sector controller, responsible for safety and regulation of traffic between flight levels 250 and 310. This controller cleared to flight to FL350.
The aircraft assumed a heading of 353° and a speed of 273 Kts as it passed a beam and to the west of the KOS NDB, approximately 2-3 km from the airway centreline. While heading towards the Zagreb VOR, the flight crew radioed the Upper Sector controller on frequency 134,45 MHz at 10:14:04 GMT and reported that they were climbing through FL325. The controller then requested, in Serbo-Croatian, flight JP550 to maintain their present altitude and report passing the Zagreb VOR. The controller stated that an aircraft was in front passing from left to right at FL335, while in fact BE476 was at FL330. At 10:14:38 the crew replied, also in Serbo-Croatian, that they where maintaining FL330.
Three seconds later both aircraft collided. The outer five meters of the DC-9's left wing cut through the Trident's cockpit. Due to the sudden decompression, the forward part of the Trident's fuselage disintegrated. The remaining part of the fuselage struck the ground tail-first. With its left wing torn off, the DC-9 tumbled down and hit the ground right-wing first.
Probable Cause:
CAUSES OF THE ACCIDENT: "1) Direct cause of the accident was the struck of the DC-9 wing into the middle side of the TRIDENT THREE fuselage which occurred at the height of 33.000 feet above Zagreb VOR so that both aircraft became uncontrollable and fell on the ground.; 2) Improper ATC operation; 3) Non-compliance with regulations on continuous listening to the appropriate radio frequency of ATC and non-performance of look-out duty from the cockpits of either aircraft."
Accident investigation:
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Investigating agency: | AIB  |
Status: | Investigation completed |
Duration: | 106 days (4 months) | Accident number: | AAR 5/1977 | Download report: | Final report
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Fuentes:
» Air Disasters
» Aviation Week & Space Technology
»
Collision course / by Tony Brkic
Subsiguiente / acciones de seguridad
issued 5 Safety Recommendations
Issued: 25-DEC-1976 | To: | G-AWZT (1) |
The regulations should specify that an individual secondary radar identity code is retained by each aircraft throughout its entire flight within a Control Area where the radar coverage is provided. |
Issued: 25-DEC-1976 | To: | G-AWZT (2) |
To prohibit switching off of the transponder during the transfer of aircraft between the adjacent sectors. |
Issued: 25-DEC-1976 | To: | G-AWZT (3) |
Radar height filtering system should be used in such a way that it includes the layers between the adjacent sectors thus providing the automatic tracking of aircraft during climbing or descending and their observance before they enter the airspace of the specific sector. |
Issued: 25-DEC-1976 | To: | G-AWZT (4) |
For air-ground radio-telephony communications a standard phraseology in the English language to be used by Air Traffic Control Units and aircraft during the flight along the airways and in the zones used for international air services. |
Issued: 25-DEC-1976 | To: | G-AWZT (5) |
The duties of the crews should be defined more precisely in respect of the look-out for the purpose of avoidance of air collision, when the conditions permit. Produced in |
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Fotos

accident date:
10-09-1976type: Hawker Siddeley HS-121 Trident 3B
registration: G-AWZT
Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does
not display the exact flight path.
Distance from London-Heathrow Airport to Istanbul-Yesilköy Airport as the crow flies is 2495 km (1560 miles).
Accident location: Exact; as reported in the official accident report.
This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.