Crash of a Convair B-36B-1-CF Peacemaker at Carswell AFB

Date & Time: Feb 8, 1955
Type of aircraft:
Operator:
Registration:
44-92029
Flight Type:
Survivors:
Yes
Schedule:
Biggs - Carswell
MSN:
26
YOM:
1946
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful training flight from Biggs AAF, the pilot-in-command started the approach to Carswell AFB but was too low. On short final, the airplane hit the ground, lost its undercarriage and came to rest. There were no casualties but the aircraft was written off.
Probable cause:
Too low approach on part of the pilot-in-command.

Crash of a Douglas A-20K Havoc in São Paulo: 2 killed

Date & Time: Jan 24, 1955
Operator:
Flight Type:
Survivors:
No
Schedule:
São Paulo - São Paulo
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a local training mission at São Paulo-Guarulhos Airport when the airplane crashed in unknown circumstances in Cumbica, about 3 km from the airfield. Both crew members were killed.

Crash of an Avro 696 Shackleton MR.2 into the Celtic Sea: 9 killed

Date & Time: Jan 11, 1955 at 2100 LT
Type of aircraft:
Operator:
Registration:
WL743
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Saint Eval - Saint Eval
YOM:
1953
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The aircraft left RAF St Eval at 1020LT for a 15 hours training mission, preceded by six minutes from a first RAF Avro 696 Shackleton MR.2 registered WG531 and carrying nine crew members as well. The last radio contact was recorded at 2058LT and two minutes later, both aircraft disappeared simultaneously. SAR operations were conducted but all operations were suspended few days later as no trace of both aircraft nor the 18 crew members was found. More than eleven years later, a fisherman found in is fishnet the engine number four from the Shackleton registered WL743 about 75 miles north of the assumed collision point.
Crew (42nd Squadron):
P/O L. W. Wood, pilot,
Sgt H. Davies, pilot,
F/O N. Horrocks, navigator,
F/O G. Molyneux, navigator,
Sgt D. Male, flight engineer,
Mst I. O. Cathcart, air signaler,
Sgt C. W. Scott, air signaler,
Sgt R. E. Ridgers, air signaler,
Sgt L. W. Cooper, air signaler.
Probable cause:
Without probent elements, it was not possible to determine the exact cause of the accident. Nevertheless, it is believed that the accident was the result of an in-flight collision that occurred in reduced visibility.

Crash of an Avro 696 Shackleton MR.2 into the Celtic Sea: 9 killed

Date & Time: Jan 11, 1955 at 2100 LT
Type of aircraft:
Operator:
Registration:
WG531
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Saint Eval - Saint Eval
YOM:
21
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The aircraft left RAF St Eval at 1014LT for a 15 hours training mission, followed six minutes later by a second RAF Avro 696 Shackleton MR.2 registered WL743 and carrying nine crew members as well. The last radio contact was recorded at 2058LT and two minutes later, both aircraft disappeared simultaneously. SAR operations were conducted but all operations were suspended few days later as no trace of both aircraft nor the 18 crew members was found. More than eleven years later, a fisherman found in is fishnet the engine number four from the Shackleton registered WL743 about 75 miles north of the assumed collision point.
Crew (42nd Squadron):
F/O G. Board, pilot,
F/O K. G. Richards, pilot,
F/O G. Rogers, navigator,
F/O B. H. Webb, navigator,
F/Sgt M. G. Rae, air signaler,
Sgt L. R. Swann, air signaler,
Sgt J. T. Goodwin, air signaler,
Sgt E. J. Morgan, air signaler,
Sgt G. Thompson, air signaler.
Probable cause:
Without probent elements, it was not possible to determine the exact cause of the accident. Nevertheless, it is believed that the accident was the result of an in-flight collision that occurred in reduced visibility.

Crash of an Avro 683 Lancaster MR.3 into the Celtic Sea: 7 killed

Date & Time: Dec 17, 1954
Type of aircraft:
Operator:
Registration:
RF290
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Saint Eval - Saint Eval
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew left RAF Saint Eval to conduct a training mission consisting of a submarine attack. In unknown circumstances, the aircraft crashed into the Celtic Sea off the Cornwall coast. All seven crew members were killed.
Probable cause:
The cause of the accident could not be established.

Crash of a De Havilland DH.104 Dove 2B in Camden: 1 killed

Date & Time: Dec 1, 1954 at 1200 LT
Type of aircraft:
Operator:
Registration:
VH-DHD
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Camden - Camden
MSN:
04400
YOM:
1953
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was engaged in a local training flight to be familiarized on this aircraft that was registered on the Australian registry two days earlier. Shortly after takeoff, while climbing, the airplane crashed in a field and was destroyed. A pilot was killed while two other occupants were injured.
Crew:
Cpt T. H. Dalton, pilot,
Reginald C. Adsett, examiner, †
R. H. Jarvis, assistant to Mr. Adsett.

Crash of a Lockheed PV-2 Harpoon in Vaccarizzo: 5 killed

Date & Time: Nov 6, 1954 at 0930 LT
Type of aircraft:
Operator:
Registration:
MM80061
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sigonella - Sigonella
MSN:
15-1329
YOM:
1944
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The crew (87th Squadron) was completing a local training sortie from Sigonella NAS. In unclear circumstances, the Harpoon collided in flight with a second Italian Air Force Harpoon registered MM80065 and carrying a crew of four. Following the collision, both aircraft went out of control, dove into the ground and crashed in Vaccarizzo, about 15 km south of Catania. The debris were found in a wasteland located less than a km from the beach. Both aircraft were destroyed and all nine crew members were killed.

Crash of a Lockheed PV-2 Harpoon in Vaccarizzo: 4 killed

Date & Time: Nov 6, 1954 at 0930 LT
Type of aircraft:
Operator:
Registration:
MM80065
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sigonella - Sigonella
MSN:
15-1479
YOM:
1944
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew (87th Squadron) was completing a local training sortie from Sigonella NAS. In unclear circumstances, the Harpoon collided in flight with a second Italian Air Force Harpoon registered MM80061 and carrying a crew of five. Following the collision, both aircraft went out of control, dove into the ground and crashed in Vaccarizzo, about 15 km south of Catania. The debris were found in a wasteland located less than a km from the beach. Both aircraft were destroyed and all nine crew members were killed.

Crash of a Nord 1402 Noroit into the Lake of Bizerte: 7 killed

Date & Time: Nov 2, 1954 at 1030 LT
Type of aircraft:
Operator:
Registration:
53.S.8
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bizerte - Bizerte
MSN:
8
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew left Bizerte-Sidi Ahmed AFB for a local training sortie. While cruising at an altitude of 300 feet, the seaplane nosed down, plunged into the lake of Bizerte and sank by a depth of seven meters. A crew member was rescued while seven others were killed. The aircraft was recovered but was destroyed.
Crew (53S Squadron):
2nd Master Michel Chosserie,
2nd Master Pierre Barbanchon, mechanic, †
Lt Guy Sauvage, †
Off Bernard Dorion, †
1st Master Joseph Le Berre, mechanic, †
Master Henri Menagerm, radio operator, †
2nd Master Robert Mignot, †
Second Master L’Aot, radio operator. †

Crash of a Vickers 720 Viscount in Mangalore: 3 killed

Date & Time: Oct 31, 1954 at 1507 LT
Type of aircraft:
Operator:
Registration:
VH-TVA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Mangalore - Mangalore
MSN:
44
YOM:
1954
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
11000
Captain / Total hours on type:
21.00
Copilot / Total flying hours:
12000
Copilot / Total hours on type:
4
Aircraft flight hours:
100
Aircraft flight cycles:
120
Circumstances:
The crew (pilots and engineers) were engaged in a local training flight at Mangalore Airport, Victoria. During the takeoff roll on runway 22, after it reached V1 speed, the instructor shut down the engine number four and feathered its propeller to simulate an engine failure. The pilot-in-command continued the takeoff procedure. Shortly after rotation, the aircraft turned to the right and reached the height of 100 feet when it stalled and crashed in flames in a field located less than one km west of the airfield. Five crew members were injured (three of them seriously) while three pilots were killed. The aircraft was destroyed. The takeoff from which the accident resulted was being attempted in the most critical three-engine configuration, i.e. with number 4 engine (starboard outer) inoperative. In this configuration, with flaps extended 20° and the three engines on full power, a minimum speed of 96 knots is necessary in order to ensure that, using both rudder and aileron, a constant heading can be maintained. When flying under these conditions at speeds below 96 knots it is not possible to keep the aircraft from turning. The takeoff safety speed for the conditions existing at the time of this accident is given in the flight manual for Viscount VH-TVA as 106 knots and it has been the practice of Trans- Australia Airlines to teach its pilots not to lift the aircraft off the ground at speeds below 110 knots in a three-engine takeoff. It has been calculated that with normal acceleration in a three-engine take-off the speed of the aircraft when it left the runway would have been 85 to 90 knots which was too low.
Probable cause:
The cause of the accident was an error of judgment on the part of the pilot-in-command in that he took the aircraft into the air at a speed below the minimum control speed, following loss of directional control during the ground run. Some difficulty in maintaining directional control had been experienced during the take-off run but the final loss probably occurred through nose-wheel steering being relinquished as the pilot-in-command took over the controls. A factor probably contributing to this accident was the limited experience of the pilot-in-command on this type of aircraft. Also, the report included the conclusion that the injuries sustained by the operating crew indicate that they may have survived this accident if they had been wearing the full safety harness provided for their use in the aircraft.
Final Report: