Crash of a Britten-Norman BN-2A-7 Islander off Hong Kong

Date & Time: Dec 15, 1992
Type of aircraft:
Registration:
HKG-7
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Hong Kong - Hong Kong
MSN:
615
YOM:
1970
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight in Hong Kong on behalf of the Royal Hong Kong Auxiliary Air Force. An engine failed en route and the aircraft crashed in the Tolo harbour, north of Hong Kong. Both pilots were rescued and the aircraft was damaged beyond repair.
Probable cause:
Engine failure for unknown reasons.

Crash of a Curtiss C-46F-1-CU Commando in Laos

Date & Time: Mar 13, 1975
Type of aircraft:
Operator:
Registration:
XW-PMF
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Hong Kong – Vientiane
MSN:
22561
YOM:
1945
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances somewhere in Laos while completing a cargo flight from Hong Kong to Vientiane. Both crew members were rescued while the aircraft was damaged beyond repair. The exact circumstances of the mishap remains unclear.

Crash of a Sud-Aviation SE-210 Caravelle III off Penghu Islands: 25 killed

Date & Time: Nov 21, 1971 at 2150 LT
Operator:
Registration:
B-1852
Flight Phase:
Survivors:
No
Schedule:
Taipei - Hong Kong
MSN:
122
YOM:
1962
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
25
Circumstances:
While cruising by night over the Taiwan Strait en route from Taipei to Hong Kong, the airplane disappeared from the radar screen without any distress call on part of the flying crew. Debris were found in the next early morning, floating on water off the Penghu Islands (Pescadores Islands), Taiwan. None of the 25 occupants survived the crash, among them the Ambassador of Brazil in China. Eye witnesses reported that the airplane disintegrated in the air.
Probable cause:
It was determined that the accident was the consequence of an in-flight disintegration of the airplane after a bomb exploded on board. The author and the reason of this act of terrorism remains unknown.

Crash of a Douglas DC-8-43 in Tokyo: 64 killed

Date & Time: Mar 4, 1966 at 2015 LT
Type of aircraft:
Operator:
Registration:
CF-CPK
Survivors:
Yes
Schedule:
Hong Kong – Tokyo – Vancouver
MSN:
45761
YOM:
1965
Flight number:
CP402
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
62
Pax fatalities:
Other fatalities:
Total fatalities:
64
Captain / Total flying hours:
26564
Captain / Total hours on type:
4089.00
Copilot / Total flying hours:
19789
Copilot / Total hours on type:
3071
Aircraft flight hours:
1792
Circumstances:
Flight 402 was a scheduled international flight from Hong Kong to Tokyo and Vancouver. It took off from Hong Kong at 1614 hours Japan Standard Time and was routed via Taipei, Kagoshima and Ohshima. At 1908 hours it flew over "Spencer Victor" at 25 000 ft and started to descend gradually; at 1912 hours it crossed "Rice Victor" at 18 000 it and two minutes later entered the Kisarazu holding pattern at 14 000 ft where it waited for an improvement of the weather conditions at Tokyo International Airport (TIA). At 1942 hours the flight notified Tokyo air traffic control that if the weather conditions failed to improve within 15 minutes, it would divert to Taipei (alternate airport). Ten minutes later, at 1952 hours the flight was advised by Tokyo ATC that the RVR was 2 400 ft and the pilot then asked for a clearance for approach and landing. The approach clearance was given and the aircraft proceeded to descend to 3 000 ft, in the holding pattern. However, the weather conditions at TIA worsened and the aircraft did not proceed with the approach. The pilot requested a clearance to divert to Taipei at 1958 hours and commenced climbing. At 2005 hours, while heading for Tateyama en route to Taipei the flight was advised by Tokyo air traffic control that visibility at TIA had improved to 4 mile with RVR 3 000 ft. Consequently, the pilot requested a clearance to return to Kisarazu and began descending from 11 500 ft. At 2011 hours the aircraft arrived over Kisarazu at 3 000 ft and began another approach under instructions of the GCA. At this time the flight was quite normal. When the aircraft was 8 NM from touchdown at an altitude of 1 500 ft, it was advised that there was a light tailwind 150015 kt and was cleared to land on runway 33R. The rate of descent for final approach was begun about 5.3 NM from touchdown at approximately 2012:58 hours. The aircraft was on course and on the glide path with a ground speed of approximately 174 kt, gradually decreasing to approximately 140 kt at 2 NM and 114 kt after passing 1 NM. When the aircraft reached one mile from touchdown, the GCA final controller noted that the aircraft was slightly below the GCA glide path and advised "20 ft low, level off momentarily". Nevertheless, the aircraft continued its approach 20 ft below and in parallel with the GCA glide path. After the aircraft passed the P.M. (precision minimum), the aircraft requested the intensity of the lights to be reduced. Shortly thereafter, the aircraft made a sharp descent and its main landing gear wheel struck No. 14 approach light 2 800 ft from touch- down point approximately in an attitude of level flight. Following this first contact, the aircraft struck the approach lights one by one until No. 3 damaging or destroying them, and at approximately 2015 hours crashed against the sea wall with the bottom of the fore-fuselage. Then, the aircraft was thrown over near the end of runway 33R, destroyed and caught fire. All 10 crew members and 54 passengers were killed while eight others were injured.
Probable cause:
The pilot misjudged landing approach under unusually difficult weather conditions. The visibility at Tokyo International Airport was reduced at the time of landing to less than half a mile by fog and smoke, RVR was in the order of 3 000 it. The aircraft carried out a GCA approach to runway 33R under very difficult conditions. It was considered that the approach was normal until a point located between 3 900 and 3 600 ft before the touchdown point. It then entered a steep rate of descent between 3 900 and 3 600 it before the touchdown point, it first struck an approach light 2 800 ft from the touchdown point in an attitude of level flight, then broke several approach light piers and crashed against the sea wall of the airport. The wreckage was thrown over the sea wall near the runway threshold and completely destroyed by the ensuing fire. The steep rate of descent was considered to be the result of an intentional manoeuvre of the aircraft by the pilot-in-command with a view to executing a final approach at a lower altitude than normal. Although no certain cause for the excessive descent which led to striking the approach lights could be determined, it was considered that the poor visibility due to illusive fog conditions that night misled the pilot-in-command in his judgement.
Final Report:

Crash of a De Havilland DH.106 Comet 4C on Mt Khao Yai: 26 killed

Date & Time: Jul 19, 1962 at 2244 LT
Type of aircraft:
Operator:
Registration:
SU-AMW
Flight Phase:
Survivors:
No
Site:
Schedule:
Tokyo – Hong Kong – Bangkok – Bombay – Bahrain – Cairo
MSN:
6464
YOM:
1962
Flight number:
MS869
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
26
Circumstances:
Flight UA869 departed from Hong Kong for Bangkok, an intermediate stop, on a scheduled service to Cairo. Takeoff time was 13:30 UTC. The flight climbed to 31000 ft, the selected cruising altitude. At 15:14 UA869 advised Bangkok ATC that the flight had crossed the Bangkok FIR boundary at 15:08 and passed over Ubol NDB at 15:13 and requested to fly direct from Ubol NDB to Bangkok VOR. This request was granted by Bangkok ATC. At this time UA869 advised Bangkok ATC that the ETA for Bangkok VOR would be 15:47. At 15:27 the flight advised Bangkok ATC that it would be over the 100 mile perimeter at 15:30. After reporting that it was 90 miles out the crew requested descent clearance to a lower altitude. Bangkok control cleared the flight to descend to 4000 ft on the Bangkok VOR radial of 073 degrees and to report when commencing descent from 31000 ft. The flight was instructed to contact Bangkok approach control at 15:39. At 15:35 the flight was cleared to 3000 ft and informed that the altimeter setting was 1007.8 mb. At 15:40 the flight transferred to the Bangkok approach control. Immediately after this UA869 reported to approach control that it was descending from 13000 ft and estimating Bangkok VOR at 15:44. Approach control advised the flight to adjust the altimeter setting to 1007.8 mb and then cleared the flight to cross Bangkok VOR for final approach on runway 21R and report immediately on descending from 3000 ft. This was the last contact with the flight. The Comet flew into the side of Khao Yai Mountain, 52 nm NE of Bangkok.
Probable cause:
The principal cause of the accident was the pilot's action in commencing descent at 1530 hours when the aircraft was 137 miles and not 90 miles from the Bangkok VOR as reported to Bangkok Control, and the aircraft, therefore, collided with a mountain at a point 52 miles distant. It is probable that the pilot-in-command did not actually pass over the point he reported to the Flight Control Units, but only estimated he had passed three points which resulted in grave errors of time and distance in his computations. It is also probable that the pilot-in-command had been too self-confident so that his actions were not according to the fundamental principles of air navigation.
Final Report:

Crash of a Douglas C-54D-15-DC Skymaster near Taitung: 14 killed

Date & Time: Mar 6, 1955
Type of aircraft:
Operator:
Registration:
43-17208
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Tokyo – Kadena – Hong Kong
MSN:
22158
YOM:
1945
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
The aircraft was performing a flight from Tokyo-Haneda to Hong Kong with an intermediate stop at Kadena AFB, Okinawa. While cruising at an altitude of 9,000 feet over Taiwan in reduced visibility, the four engine aircraft hit the slope of a mountain located 32 km northwest of Taitung. The airplane was destroyed by impact forces and all 14 occupants have been killed.
Probable cause:
It is believed the accident was the result of a controlled flight into terrain.

Crash of a Martin PBM-5 Mariner in Hong Kong: 4 killed

Date & Time: Dec 31, 1951
Type of aircraft:
Operator:
Registration:
84682
Flight Phase:
Survivors:
Yes
MSN:
84682
YOM:
1945
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Shortly after takeoff from Hong Kong, the seaplane stalled and crashed into the Kowloon Bay. Four crew members were killed while seven others were injured.

Crash of a Douglas R5D-1 in Hong Kong: 24 killed

Date & Time: Mar 11, 1951
Type of aircraft:
Registration:
HS-POS
Flight Phase:
Survivors:
No
Site:
Schedule:
Hong Kong – Bangkok
MSN:
10396
YOM:
1944
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
24
Circumstances:
Few minutes after takeoff from runway 13 at Hong Kong-Kai Tak Airport, while in initial climb, the four engine aircraft christened 'City of Ayudhya' hit the slope of a mountain located between Mt Butler and Mt Parker, on the Hong Kong Island. All 24 occupants were killed. At the time of the accident, weather conditions were marginal and the visibility was poor due to low clouds. For unknown reason, the aircraft was climbing at an insufficient altitude.

Crash of a Short S.25 Sunderland GR5 near Yuli: 14 killed

Date & Time: Jan 28, 1951 at 0840 LT
Type of aircraft:
Operator:
Registration:
PP107
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Iwakuni – Hong Kong
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
The aircraft was performing a flight from Iwakuni AFB to Hong Kong on behalf of the UN Command for the Korean War. While cruising at an altitude of 5,000 feet in poor weather conditions, the Sunderland hit the slope of a mountain located near Yuli, Taiwan. The wreckage was found few days later in an isolated area and all 14 occupants have been killed.
Probable cause:
The exact cause of the accident could not be determined with certainty. However, it is the opinion of the board that the aircraft was off course at the time of the accident, most probably due to a navigational error on part of the flying crew.

Crash of a Douglas C-47B-20-DK Dakota C.4 into the China Sea: 9 killed

Date & Time: Aug 30, 1950
Operator:
Registration:
KN240
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Singapore – Hong Kong – Saigon
MSN:
15664/27109
YOM:
1945
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
En route from Singapore to Hong Kong, the pilot encountered an unexpected situation and lost control of the aircraft that crashed into the China Sea. A crew member was rescued while nine other occupants were killed.