Country
code

West Sussex

Crash of an Airspeed AS.57 Ambassador 2 in London-Gatwick

Date & Time: Jul 26, 1969
Type of aircraft:
Operator:
Registration:
G-ALZR
Flight Type:
Survivors:
Yes
Schedule:
Paris - London
MSN:
5214
YOM:
1952
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On touchdown at Gatwick Airport, the nose gear collapsed. The airplane slid for dozen yards before coming to rest. All eight occupants were evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Nose gear collapsed on landing.

Crash of a Boeing 727-113C in London: 50 killed

Date & Time: Jan 5, 1969 at 0134 LT
Type of aircraft:
Operator:
Registration:
YA-FAR
Survivors:
No
Schedule:
Kabul - Kandahar - Beirut - Istanbul - Frankfurt - London
MSN:
19690/540
YOM:
1968
Flight number:
FG701
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
54
Pax fatalities:
Other fatalities:
Total fatalities:
50
Captain / Total flying hours:
10400
Captain / Total hours on type:
512.00
Copilot / Total flying hours:
3259
Copilot / Total hours on type:
210
Aircraft flight hours:
1715
Circumstances:
The accident occurred on a scheduled passenger flight from Frankfurt when the aircraft was making an ILS approach for a night landing on Runway 27 at Gatwick Airport. The weather was clear except that freezing fog persisted in places including the Gatwick area. The runway visual range (RVR) at Gatwick was 100 metres. The approach was commenced with the autopilot coupled to the instrument landing system (ILS) but after the glide-slope had been captured the commander who was at the controls, disconnected the autopilot because the "stabiliser out of trim" warning light illuminated. At the outer marker the flap setting was changed from 1° to 30° and shortly afterwards the rate of descent increased and the aircraft descended below the glide-slope. Some 200 feet from the ground the pilot realised that the aircraft was too low and initiated a missed approach procedure. The aircraft began to respond but the descent was not arrested in time to avoid a collision with trees and a house that destroyed both the aircraft and the house and set the wreckage on fire. 48 occupants as well as two people in the house were killed. 14 others were injured. The aircraft was totally destroyed by impact forces and a post crash fire.
Probable cause:
The accident was the result of the commander inadvertently allowing the aircraft to descend below the glide slope during the final stage of an approach to land until it was too low for recovery to be effected. The following findings were reported:
- The deceptive nature of the weather conditions led the commander to an error of judgment in deciding to make an approach to Gatwick,
- The commander's decision to conduct an approach was not in itself a cause of the accident,
- Incorrect flap configuration at glide-slope interception led to a temporary out-of-trim condition during the automatic approach and the illumination of the stabilizer "out-of-trim" warning light,
- The commander interpreted the "out-of-trim" warning light as indicating a possible malfunction and disconnected the auto-pilot,
- Out-of-sequence and late selection of 30° flaps from 15° while the-aircraft was being flown manually resulted in an increase in the rate of descent, causing the aircraft to go rapidly below the glide-slope,
- The commander did not become aware of the deviation from the glide-slope until it was too late to effect a full recovery,
- The pilot's attention was probably directed outside the aircraft at the critical time in an attempt to discover sufficient visual reference to continue the approach rather than to the flight instruments,
- Monitoring by precision approach radar would have warned the pilots of the deviation in time, if corrective action was taken promptly, to avoid the accident.

Crash of a Sud-Aviation SE-210 Caravelle 10R in Haslemere: 37 killed

Date & Time: Nov 4, 1967 at 2202 LT
Operator:
Registration:
EC-BDD
Survivors:
No
Schedule:
Málaga – London
MSN:
202
YOM:
1966
Flight number:
IB062
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
37
Circumstances:
Iberia flight IB062 left Málaga, Spain, at 19:30 UTC on a flight to London-Heathrow Airport, United Kingdom. The weather at the time was slightly misty with intermittent drizzle but there was reasonable visibility. The aircraft was cleared to descend to FL210 after passing latitude 50 °N and was given a routing via Ibsley and Dunsfold. After passing conflicting traffic, the aircraft was recleared to FL110 and directed to turn right on to 060° for Dunsfold. Passing abeam Fawley the aircraft was further cleared to FL60 and, in acknowledging this instruction, the crew reported leaving FL145. Just under 4 minutes later the aircraft was cleared to proceed direct to Epsom on its own navigation. The flight crew acknowledgement this instruction. All the while the aircraft had been in a continuous descent, until it impacted trees on the southern slope of Blackdown Hill, approximately 48 km south-southwest of Heathrow Airport. The aircraft continued for hundreds of yards, passing across a meadow where it killed 65 grazing sheep. It then broke through a large hedge and parts of the aircraft fell off destroying a garage, and damaging parts of the roof of Upper Blackdown House as the aircraft disintegrated. None of the 37 occupants survived the crash.
Probable cause:
Accident investigators failed to find the reason for the continued descent. A possible misreading of the altimeters was examined in detail. The aircraft was fitted with three-pointer altimeters with warnings to indicate when the aircraft was below 10,000ft. The aircraft descended continuously at a steady rate over a period of 13 1/2 minute and the pointers would have been in continuous motion throughout, increasing the likelihood of misreading. The cross hatching in this type of altimeter first appears in a window in the 10,000ft disc at an indicated altitude of 26,666ft and the edge of the cross hatching would have been visible within 2 minutes of the aircraft beginning its descent. At 10,000 feet the cross hatching completely fills the window and it remains filled as long as the aircraft is below 10,000ft. Thus the cross hatching would have been visible to the crew for a period of about 9 1/2 minutes before the aircraft passed through FL60. According to the investigation report, it is not difficult to read an indication of 6,000ft as 16,000ft with this type of altimeter if particular note is not made of the position of the 10,000ft pointer. Evidence against the possibility of a simple misreading of this sort is the message from the aircraft to ATC reporting passing FL145. indicating that at this time the crew knew that they were below 16,000ft. This evidence indicates that down to this level there had been no misreading or misinterpretation but it does not dispose of the possibility that the crew subsequently suffered a mental loss of sequence and transposed themselves in time and space back to some altitude above 16,000ft. This has been known to, happen in the past, the investigators noted. Nevertheless, there is no evidence to show that it happened on this occasion. In conclusion, the accident was due to the aircraft having continued to descend through its assigned flight level down to the ground. No reason could be established for the continued descent.

Crash of a Handley Page H.P.67 Hastings at RAF Thorney Island: 1 killed

Date & Time: Dec 17, 1963
Operator:
Registration:
TG610
Flight Type:
Survivors:
Yes
Schedule:
Thorney Island - Thorney Island
MSN:
88
YOM:
1949
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was completing a local training flight at RAF Thorney Island. After touchdown, the four engine aircraft encountered difficulties to stop within the remaining distance, overran and collided with a building housing the radiotelegraph services of the airbase. None of the crew was injured while one person working in the building was killed.

Crash of a Vickers 651 Valetta C.1 in London-Gatwick

Date & Time: Sep 21, 1963
Type of aircraft:
Operator:
Registration:
G-APKR
Flight Type:
Survivors:
Yes
Schedule:
London - London
MSN:
338
YOM:
1949
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After a flight of some two hours, made for the purpose of testing radio navigation equipment, the aircraft returned to London-Gatwick Airport, U.K.. Before, and during, the flight, undercarriage operation was normal, as was the functioning of the undercarriage light and horn warning system. During the approach, the undercarriage extended normally, and the green lights indicated that it was locked down. Some 50 yards after touch down, the aircraft began to sink on the starboard side and the captain noticed that the starboard green light was no longer showing. There were, however, no reds, and the horn was not sounding. The starboard main undercarriage leg eventually retracted and the aircraft swung off the runway to the right, on to the grass.

Crash of a Handley Page H.P.67 Hastings C.1 at RAF Thorney Island

Date & Time: Mar 7, 1962
Operator:
Registration:
TG508
Flight Type:
Survivors:
Yes
MSN:
12
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to RAF Thorney Island, during the last segment, the airplane was caught by downdraft and struck the ground. On impact, the undercarriage were sheared off. The airplane slid for several yards and came to rest in flames. There were no casualties but the aircraft was destroyed.
Probable cause:
Suffered downdraft on final approach.

Crash of a Vickers 648 Varsity T.1 near RAF Tangmere: 2 killed

Date & Time: Oct 19, 1959
Type of aircraft:
Operator:
Registration:
WF381
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Boscombe Down - Boscombe Down
MSN:
540
YOM:
1952
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was involved in a test flight for an asymmetric safety speed assessment out from RAF Boscombe Down. At an altitude of 10,000 feet, the crew lost control of the airplane after applying full power on one engine in takeoff configuration. The aircraft stalled, dove into the ground and crashed in an open field. Both crew members were killed.

Crash of a Vickers 794D Viscount in London: 14 killed

Date & Time: Feb 17, 1959 at 1647 LT
Type of aircraft:
Operator:
Registration:
TC-SEV
Flight Type:
Survivors:
Yes
Schedule:
Ankara - Rome - London
MSN:
429
YOM:
1958
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
14
Captain / Total flying hours:
7716
Captain / Total hours on type:
216.00
Copilot / Total flying hours:
5504
Copilot / Total hours on type:
103
Aircraft flight hours:
548
Circumstances:
The aircraft was on a special flight from Ankara to London via Rome with Adnan Menderes the Prime Minister of Turkey and a party of Turkish Government officials on board. The aircraft left Rome at 13:02. TC-SEV called London Airways at 15:56 after passing Abbeville and was cleared by ATC to the Epsom Radio Range station, the holding point for London Airport. Because of poor visibility at destination London (Heathrow) Airport, the London Airport Commandant decided to inform the Turkish captain that he should divert to Gatwick. At 16:21 hrs the aircraft reported over the Epsom range and was given diversion instructions. At 16:27 it left Epsom for Mayfield, the holding point for Gatwick, where it was informed by Gatwick Approach Control that it would be positioned by radar for an ILS approach to runway 09. The latest weather report for Gatwick was given as wind calm, visibility 1.1 nm, mist, cloud 3 oktas at 600 feet, QFE 1036 mb. Over the Mayfield NDB at 4,000 feet the flight was instructed to steer a course of 280 and to descend to 2,000 feet. This was acknowledged. A further descent clearance was given to 1500 feet. The aircraft overshot the centre line slightly as it turned on to the ILS approach path. At 5nm from touchdown, the aircraft affirmed that it could continue on the ILS. TC-SEV was then asked to change to tower frequency and this request was acknowledged. This was the last communication with the aircraft. At a position of some 5 km from the runway threshold and 550 feet to the north of the approach path centre line, the aircraft contacted tops of trees 390 feet amsl at the edge of Jordan's Wood. The aircraft began to disintegrate as it descended through the trees at an angle of about 6 degrees from the horizontal until the wheels made contact with the ground. After rising again slightly the main part of the wreckage came to rest about 100 yards further on and then caught fire. The Prime Minister Adnan Menderes survived the accident with nine other people while 14 other occupants were killed, among them five crew members.
Probable cause:
The evidence is insufficient to establish the cause of the accident. There is no indication however that this can be associated either with a technical failure of the aircraft or with a failure of the ground services. Thus it is believed the accident was the result of a controlled flight into terrain.

Crash of a Hurel-Dubois/Miles HDM.105 Aerovan in Shoreham

Date & Time: Jun 28, 1958
Registration:
G-AHDM
Flight Type:
Survivors:
Yes
Schedule:
Shoreham - Shoreham
MSN:
105/1009
YOM:
1957
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The HDM 105 was a "Proof of Concept" aircraft for the proposed M106 family of Light Transport Aircraft. It was created by replacing the wooden wing of a standard M57 Aerovan (G-AJOF) with a high aspect ratio wing designed by Hurel-Dubois. As such, it first flew on 3 March 1957 piloted by George Miles and Ian Forbes, the latter doing most of the flight testing. The aircraft was severely damaged in a landing accident at Shoreham on 28 June 1958 when it stalled on landing and the tail boom cracked at the hinge line for the rear door. The aircraft was taxied to the hangar with the pilot unaware that the empennage was dragging along the ground. Subsequently, the Hurel-Dubois wings were removed and put in storage, and the wooden remains of G-AHDM disposed of at Shoreham in 1958-59.

Crash of a Miles M.60 Marathon at RAF Thorney Island

Date & Time: Nov 30, 1957
Type of aircraft:
Operator:
Registration:
XA273
Flight Type:
Survivors:
Yes
Schedule:
Thorney Island - Thorney Island
MSN:
126
YOM:
1950
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a local training flight at RAF Thorney Island. After touchdown, one of the main landing gear collapsed. The airplane sank on its belly and slid for several yards before coming to rest. Both pilots were uninjured while the aircraft was considered as damaged beyond repair.
Probable cause:
Undercarriage collapsed on landing.