Crash of a Boeing 707-323C in Baku: 2 killed

Date & Time: Nov 30, 1995 at 1910 LT
Type of aircraft:
Operator:
Registration:
4K-401
Flight Type:
Survivors:
Yes
Schedule:
Ürümqi - Baku
MSN:
19584
YOM:
1967
Location:
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
After takeoff from Ürümqi Airport, while on a cargo flight to Baku, the crew encountered technical problems with the left main gear that remained down. The crew decided to continue to Baku in such configuration. On approach to Baku-Bina Airport by night, the captain contacted ATC and was cleared to proceed to a low pass to check the undercarriage. Following the low pass, the crew initiated a turn to the left and followed a circuit for a second approach. While flying at a relative low altitude, all four engines suffered a loss of power. The aircraft lost height, collided with light poles on a bridge and crashed in a field located 9 km from the airport. Four crew members were seriously injured and two others were killed.
Probable cause:
It was determined that all four engines lost power due to low fuel. The following contributing factors were reported:
- A malfunction of the landing gear retraction system, which led to fly with a landing gear extended and caused an excessive fuel consumption. The subsequent failure to lock the left landing gear in the extended position made it necessary to do a second approach with a limited amount of fuel.
- The fuel gauge indicator readings were inaccurate and prevented the crew from having correct info about the amount of fuel available and applying the flight manual's recommendations for low-fuel flights.
- The lack of an airline bulletin on the features of the fuel system prevented the crew in the emergency situation from selecting the optimum mode for flying with a limited amount of fuel.
- Inadequate operational and maintenance organization on the part of the companies Baku Air and ALG Inc.

Crash of a Beechcraft D18S in Fort Collins

Date & Time: Nov 30, 1995 at 1330 LT
Type of aircraft:
Operator:
Registration:
N8603A
Flight Type:
Survivors:
Yes
Schedule:
Fort Collins - Fort Collins
MSN:
A-557
YOM:
1951
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7000
Captain / Total hours on type:
800.00
Circumstances:
The pilot-owner/operator, who was seated in the right seat, said the left seat pilot made the approach to runway 15. The wind was reported as being from the southwest at 20 knots with no reference to gusts. He said the pilot aligned the airplane 40 feet left of runway centerline and failed to flare. The airplane contacted the runway, bounced back into the air with the right wing high, and began drifting to the left. The right seat pilot took control, first trying to lower the wing then attempting to abort the landing. The airplane struck the ground and cartwheeled. The left seat pilot said he was 'receiving training' from the pilot-owner and was 'not at the controls' at the time of the accident.
Probable cause:
The second pilot's failure to compensate for wind conditions and his improper recovery from a bounced landing, and the pilot-in-command's inadequate supervision of the flight. Factors were the second pilot's lack of landing experience in the airplane make/model, and the gusty crosswind conditions.
Final Report:

Crash of a Rockwell Grand Commander 690A in Warsaw

Date & Time: Nov 29, 1995 at 0220 LT
Registration:
EC-FFE
Survivors:
Yes
Site:
MSN:
690-11344
YOM:
1976
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Warsaw-Okecie Airport runway 33 by night, the pilot reported engine problems when the aircraft lost height and crashed in the district of Mysiadło, about six km short of runway threshold. All four occupants were injured and there were no victims on the ground. The aircraft was destroyed. It was reported that both engines lost power on approach, maybe after being taken over by frost. At the time of the accident, icing conditions were present in Warsaw.

Crash of a Fairchild-Hiller FH-227B in Santarém: 3 killed

Date & Time: Nov 28, 1995 at 0200 LT
Type of aircraft:
Operator:
Registration:
PP-BUJ
Flight Type:
Survivors:
Yes
Schedule:
Belém - Santarém
MSN:
569
YOM:
1967
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While on a night approach to Santarém Airport, the crew decided to initiate a go-around procedure. During the second attempt to land, the crew descended below the MDA when the aircraft struck the ground and crashed 1,600 metres short of runway. A passenger was seriously injured while three other occupants were killed. It was reported that a passenger was occupying the copilot seat at the time of the accident. Also, the crew descended below MDA for unknown reasons.

Crash of a Piper PA-31-310 Navajo in Kamloops: 1 killed

Date & Time: Nov 22, 1995 at 1902 LT
Type of aircraft:
Operator:
Registration:
C-GKNB
Flight Type:
Survivors:
Yes
Schedule:
Williams Lake – Kamloops – Vancouver
MSN:
31-598
YOM:
1970
Flight number:
FCV705
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The Navair Charter Piper PA-31, flight FCV705, a mail courier with a crew of two, was on a night, instrument flight rules (IFR) flight plan from Williams Lake, British Columbia, to Kamloops. While the crew was conducting an instrument procedure to the Kamloops airport, they flew into an area that was clear of cloud. The captain cancelled his IFR flight plan and descended for a visual flight rules (VFR) approach to the airport. At 1902 PST, the aircraft collided with trees at an elevation of 2,400 feet above sea level (asl), seven nautical miles (nm) east-southeast of the Kamloops airport. The captain was fatally injured on impact, and the first officer was seriously injured; the aircraft was destroyed during the crash and post-crash fire.
Probable cause:
The aircraft collided with trees during a night, VFR descent over mountainous terrain because the crew had inadequate visual cues to accurately determine their height above the ground. Contributing to this accident were the captain's decision to cancel his IFR flight plan and attempt a visual approach from well outside the published VFR circuit area, the inherent risks of VFR flight in mountainous regions, and a requirement by the crew to remain clear of departing IFR traffic from the Kamloops airport.
Final Report:

Crash of an Antonov AN-32B off Palaly: 63 killed

Date & Time: Nov 22, 1995 at 1720 LT
Type of aircraft:
Operator:
Registration:
CR-862
Flight Type:
Survivors:
No
Schedule:
Colombo - Palaly
MSN:
35 03
YOM:
1995
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
57
Pax fatalities:
Other fatalities:
Total fatalities:
63
Circumstances:
While on approach to Papaly Airport, the captain contacted ATC and requested that the approach lights intensity should be increased. Shortly later, the twin engine aircraft went out of control and crashed in the sea few km short of runway. All 63 occupants were killed.
Probable cause:
It is believed that the aircraft was shot down by a shell fired by soldiers from the 'Liberation Tigers of Tamil Eelam'.

Crash of an Antonov AN-12TB in Huambo

Date & Time: Nov 22, 1995
Type of aircraft:
Registration:
RA-11008
Flight Type:
Survivors:
Yes
Schedule:
Luanda - Huambo
MSN:
4 026 12
YOM:
1967
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was completing a humanitarian flight from Luanda to Huambo, carrying three passengers, six crew members and a load of 13,579 kilos of food on behalf of the United Nations Organization. While descending to Huambo-Albano Machado Airport, the crew completed a last turn to join the approach path when he realized that his altitude was insufficient. Instead of initiating a go-around manoeuvre, the pilot-in-command continued the descent but landed too far down the runway which is 2,660 metres long. Unable to stop within the remaining distance, the aircraft overran and came to rest 260 metres further. All nine occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the crew who landed too far down the runway and failed to initiate a go-around. It was reported that the undercarriage and flaps were deployed too late during the approach procedure. A lack of crew coordination and a poor planned approach and landing were considered as contributing factors.

Crash of a Shaanxi Y-8 off Palaly: 5 killed

Date & Time: Nov 18, 1995
Type of aircraft:
Operator:
Registration:
CR-871
Flight Type:
Survivors:
Yes
Schedule:
Colombo - Palaly
MSN:
06 08 01
YOM:
1988
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The aircraft was approaching Palaly AFB in Jaffna following a flight from Colombo, carrying six crew members and supply equipments. On final, the aircraft was shot down by a 20 mm shell and crashed in the sea about 3 km offshore. A crew member was rescued while five other occupants were killed.
Probable cause:
Shot down by a shell fired by soldiers from the 'Liberation Tigers of Tamil Eelam'.

Crash of a Lockheed L-1329 JetStar 731 in Guadalajara

Date & Time: Nov 16, 1995
Type of aircraft:
Operator:
Registration:
XA-MIK
Survivors:
Yes
Schedule:
Mexico City – Guadalajara
MSN:
5066
YOM:
1965
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Guadalajara-Miguel Hidalgo y Costilla Airport, the crew contacted ATC and reported that all hydraulic systems failed. After being able to lower the undercarriage manually, the crew continued the approach but landed on runway 10 in a flapless configuration. Because the brakes and the thrust reversers were unserviceable, the crew was unable to stop the aircraft within the remaining distance. The aircraft overran, struck a drainage ditch and came to rest 300 metres past the runway end. All occupants were rescued, among them five were slightly injured.
Probable cause:
Loss of control upon landing after all hydraulic systems failed on approach.

Crash of a Boeing 737-2F9 in Kaduna: 11 killed

Date & Time: Nov 13, 1995 at 0853 LT
Type of aircraft:
Operator:
Registration:
5N-AUA
Survivors:
Yes
Schedule:
Yola – Jos – Kaduna – Lagos
MSN:
22985
YOM:
1982
Flight number:
WT357
Country:
Region:
Crew on board:
14
Crew fatalities:
Pax on board:
124
Pax fatalities:
Other fatalities:
Total fatalities:
11
Aircraft flight hours:
22375
Aircraft flight cycles:
27567
Circumstances:
Nigeria Airways flight WT357 departed Yola (YOL) at 07:00 en route to Lagos (LOS). Intermediate stops were planned at Jos (JOS) and Kaduna (KAD). The Boeing 737 landed at Jos at 07:40 and departed fifty minutes later. The flight to Kaduna was uneventful. Kaduna ATC gave the aircraft an inbound clearance with no delay for a locator approach to runway 05. Though, the initial landing clearance was for runway 05, the captain requested to land on runway 23. He was reminded by the controller that the wind was from 090 magnetic, but he still insisted on using the 23 approach. At 08:42, the aircraft commenced its initial descent at 48 miles on the ILS/DME to 4,500 ft. At 08:49 UTC, it was cleared to 3,500 ft at 10 miles out and was later descended to 500 ft. The aircraft turned left from the track 310 to align with runway 23 and the aircraft was still in the turn when the threshold was sighted just 1.5 miles to the left of the aircraft. The first officer asked the captain "Can you make it to land from that position?". The observer in the jump seat also suggested going on the downwind, presumably to re-position the aircraft for landing on runway 05. There was no response at all from the captain and the approach was continued for runway 23. The left turn was very steep and it took the aircraft to the left of the runway centreline and a right correction was applied. The observer shouted "Watch the wing" as the wings could have struck the ground on the final approach. By this time, the aircraft crossed the threshold with the flying pilot still struggling to maintain directional control for runway centreline alignment. The aircraft touched down 7820 feet down the runway, leaving just 2020 ft (615.85 m) of runway length. The captain was reported to have used 1.8 and 1.6 EPR on the reversers. When a runway overrun became inevitable, the captain turned the aircraft to the left with the intention to take advantage of the last rapid exit intersection to avoid the runway end lights. At this juncture, the aircraft entered an uncontrollable skid. The right wing hit the ground, thus rupturing the fuel tanks and a huge fire erupted. The aircraft was destroyed by the fire.
Probable cause:
The probable cause of the accident is the continuation of a highly unstabilized approach when the option of a missed approach could have been taken. The contributing factor was the turn off at 76 knots into the high speed intersection when an overrun into the extended runway end should have been maintained.