Crash of a PZL-Mielec AN-2R in Verkhnyaya Toyma

Date & Time: Dec 5, 1995 at 1235 LT
Type of aircraft:
Operator:
Registration:
RA-17725
Flight Phase:
Survivors:
Yes
Schedule:
Verkhnyaya Toyma – Kotlas
MSN:
1G202-45
YOM:
1983
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During initial climb, the crew encountered difficulties to gain height. The crew elected to make an emergency landing when the aircraft crashed in an open field some three minutes after takeoff. The wreckage was found 500 metres from the runway end. Four occupants escaped uninjured while 11 others were injured. The aircraft was written off.
Probable cause:
It was determined that the aircraft was overloaded.

Crash of a Boeing 737-2K9 in Douala: 71 killed

Date & Time: Dec 3, 1995 at 2244 LT
Type of aircraft:
Operator:
Registration:
TJ-CBE
Survivors:
Yes
Schedule:
Cotonou – Douala
MSN:
23386
YOM:
1985
Flight number:
UY3701
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
71
Pax fatalities:
Other fatalities:
Total fatalities:
71
Captain / Total flying hours:
7990
Captain / Total hours on type:
5923.00
Copilot / Total flying hours:
5850
Copilot / Total hours on type:
4317
Aircraft flight hours:
18746
Aircraft flight cycles:
23233
Circumstances:
While on a night approach to Douala Airport, at a distance of 3,5 NM, the crew was cleared to land on runway 30. At this time, the aircraft initiated a slight climb and about 15 seconds later, the copilot informed ATC about technical problems. Three seconds later, the aircraft rolled to the left, struck trees and crashed in a mangrove located about 1,700 metres south of runway 30, bursting into flames. Three passengers and two crew members (the copilot and a stewardess) were seriously injured while 71 other occupants were killed.
Probable cause:
The accident resulted from a loss of control of the aircraft during an attempted go-around made during the touchdown maneuver on landing, with degraded performance.
The following factors contributed to the accident:
- The detachment by structural fatigue of a blade from the first stage of the compressor on engine n°1 which led to a loss of power, and
- A destabilization of the trajectory during landing and the late or slow execution of the go-around procedure in an unidentified single-engine configuration which resulted in an irreversible loss of speed.
Final Report:

Crash of a Boeing 737-2A8 in New Delhi

Date & Time: Dec 2, 1995 at 1253 LT
Type of aircraft:
Operator:
Registration:
VT-ECS
Survivors:
Yes
Schedule:
Bombay – Jaipur – New Delhi
MSN:
20963
YOM:
1974
Flight number:
IC492
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
102
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6088
Circumstances:
Following a wrong approach configuration, the aircraft landed too far down the runway, about 600 metres from the runway end. Unable to stop within the remaining distance, the aircraft overran, struck a concrete wall (45 cm high) and came to rest 450 metres further. All 108 occupants were evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
The accident was the consequence of the combination of the following factors:
- The injudicious and imprudent decision of the Pilot-in-Command to hastily complete the flight in the inadequate time available before the notified closure of Delhi airport for a VVIP flight,
- The dangerously unstabilised approach made by the Pilot-in-Command, primarily due to his failure to decelerate the aircraft in time,
- The failure of the First Officer to call out significant deviations from the stipulated approach parameters,
- The failure of the Pilot-in-Command to carry out a missed approach in spite of his approach being grossly unstabilised,
- The inadvertent omission of the Pilot-in-Command to arm the speed brake before landing,
- Touch-down of the aircraft at excessive speed and too far down the runway,
- Failure of the First Officer and Pilot-in-Command to monitor the automatic deployment of the speed brake, and failure of the Pilot-in-Command to deploy it manually,
- Impact of the aircraft with an 18-inch high cement-concrete cable duct in the kutcha ground beyond the over-run area,
- The pilot disregard of procedures, regulations and instructions.
Final Report:

Crash of a PZL-Mielec AN-2R in Makovskoye

Date & Time: Nov 28, 1995 at 1637 LT
Type of aircraft:
Registration:
RA-07419
Flight Phase:
Survivors:
Yes
Schedule:
Makovskoye – Yeniseysk
MSN:
1G150-54
YOM:
1973
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The departure from Makovskoye Airfield was initiated in poor weather conditions. After liftoff, the aircraft lost height, causing the skis to struck the ground. The aircraft bounced, climbed to a height of about 15 metres and collided with a tree before crashing on the ground. All nine occupants evacuated safely while the aircraft was destroyed.

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.

Crash of a Cessna 208B Grand Caravan near Piedras Negras: 9 killed

Date & Time: Oct 31, 1995 at 2050 LT
Type of aircraft:
Registration:
XA-SVM
Flight Phase:
Survivors:
Yes
Schedule:
Saltillo - Piedras Negras
MSN:
208B-0214
YOM:
1990
Flight number:
TAC108
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The pilot started the descent to Piedras Negras by night with a limited visibility due to poor weather conditions (drizzle and mist). Too low, the single engine aircraft struck the slope of a hill located 16 km from Piedras Negras Airport. Two passengers were seriously injured while nine other occupants were killed.
Probable cause:
Controlled flight into terrain after the pilot decided to continue the descent in below minima weather conditions.

Crash of a De Havilland DHC-6 Twin Otter 300 in Addis Ababa

Date & Time: Oct 22, 1995 at 0950 LT
Operator:
Registration:
ET-AIO
Survivors:
Yes
Schedule:
Kombolcha-Dessie – Addis Ababa
MSN:
818
YOM:
1985
Flight number:
ET173
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Addis Ababa-Bole Airport, the twin engine aircraft collided with a white backed vulture of 5,4 kg. The windshield was broken and both pilots were seriously injured. Nevertheless, they elected to make an emergency landing when the aircraft crashed 300 metres short of runway. All 20 occupants were rescued, among them nine were injured.
Probable cause:
Loss of control on final approach following bird strike.

Crash of a Dornier DO228-212K in Male

Date & Time: Oct 18, 1995 at 0946 LT
Type of aircraft:
Operator:
Registration:
9M-PEQ
Survivors:
Yes
Schedule:
Kadhdhoo - Male
MSN:
8213
YOM:
1992
Flight number:
AMI3312
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3152
Captain / Total hours on type:
2948.00
Copilot / Total flying hours:
226
Copilot / Total hours on type:
61
Aircraft flight hours:
3857
Circumstances:
Following an uneventful flight from Kadhdhoo Airport, the crew initiated the approach to Male Intl Airport. The copilot was the pilot-in-command. The aircraft landed on runway 36 at the speed of 95 knots some 600 metres past the runway threshold. After touchdown, the aircraft deviated from the centerline to the left and the copilot overcorrected, causing the aircraft to veer to the right. The captain took over control but this was too late. The aircraft overran, struck a concrete wall and crashed in the sea. All eight occupants were injured and the aircraft was destroyed.
Probable cause:
The following factors were reported:
- Failure of the PIC to take control when the aircraft touched at 20° angle to the centreline and continued towards the western edge of the runway after landing,
- The "over correction" applied by the handling pilot to the prevalent crosswind, leading the aircraft to land at 20° to the centreline,
- The over application of right rudder to get the aircraft onto centreline and subsequently failing to get the power levers to ground idle,
- The lack of a CRM programme in the company had meant that the pilots albeit friendly, did not have an harmonious attitude towards one another; particularly the captain to the copilot,
- The less than effective means of imparting company policy with respect to giving copilots (based on experience, flight conditions) to carry out landings/take-offs.

Crash of a Casa 212-A4 Aviocar 100 near Gunung Antara: 1 killed

Date & Time: Oct 3, 1995 at 0800 LT
Type of aircraft:
Operator:
Registration:
PK-ZAG
Flight Phase:
Survivors:
Yes
Schedule:
Medan - Meulobah
MSN:
158/28N
YOM:
1981
Flight number:
SMC1994
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Thirty minutes into the flight from Medan to Meulaboh, the hydraulic pressure dropped and the crew decided to shut down the left engine and to feather its propeller. Unable to maintain the prescribed altitude and because the aircraft became unstable, the crew also shut down the right engine and attempted an emergency landing when the aircraft struck trees and crashed in a swampy area. A pilot was killed while 13 other occupants were injured.
Probable cause:
Loss of oil pressure for undermined reasons.