Crash of a Fokker F27 Friendship 500RF in Baroda

Date & Time: Jul 1, 1995 at 0840 LT
Type of aircraft:
Operator:
Registration:
VT-EWE
Flight Type:
Survivors:
Yes
Schedule:
Baroda - Baroda
MSN:
10605
YOM:
1980
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9360
Circumstances:
The aircraft was engaged in a training flight at Baroda airport. It was under the command of an examiner pilot with the trainee pilot on right hand seat. The first touch and go exercise was uneventful. During the second exercise, immediately on touchdown the left main landing gear failed at its shock strut outer cylinder and the inner cylinder with the main wheel assembly attached to it got liberated. The aircraft continued moving forward with the remaining portion of left shock strut contacting the runway followed by the left engine propellers and fuselage bottom and finally came to rest on the runway left side strip. There was no fire and no injury to persons on board the aircraft.
Probable cause:
The accident occurred during aircraft touchdown due to liberation of the sliding piston along with the wheels of the left main landing gear as a result of failure of the locking arrangement on the piston top end. Non-compliance by the operator of the Service Bulletin issued by the Manufacturer and Mandatory Modifications issued by the DGCA regarding piston-adapter and dowel pin lock fitment, is the Contributory Factor in the accident.
Final Report:

Crash of a Grumman G-21E Turbo Goose in DuPage: 2 killed

Date & Time: Jun 13, 1995 at 1955 LT
Type of aircraft:
Registration:
N121H
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
DuPage - DuPage
MSN:
1211
YOM:
1942
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4200
Captain / Total hours on type:
400.00
Circumstances:
This was the first flight of the Grumman G-21 in two years. Also, the pilot had not flown the G-21 for two years. Before taking off, the pilot reported that three takeoffs and landings would be needed for purposes of becoming current. After takeoff, he flew the airplane approximately one hour and made two full stop landings. During the third takeoff, the airplane was described as lifting off in a short distance and going into a nose high attitude below an altitude of 100 feet. The airplane then rolled left, struck the ground in a steep descent, and burned. Witnesses reported that the engines were providing power until impact; the engines and propellers had evidence of rotational damage. The flap actuators were found extended to a position that equated with 30° of flaps (half flaps). Four G-21 pilots were interviewed. According to them, flaps were not normally used for takeoff in this airplane. They reported that the turboprop engines had substantial power for the weight of the airplane, especially when the plane was not loaded, and that the G-21 would tend to become airborne quickly with flaps extended. No pre impact mechanical problem was noted during the investigation.
Probable cause:
The pilot allowed excessive nose-up rotation of the airplane during lift-off, and failed to obtain and/or maintain adequate airspeed, which resulted in an inadvertent stall and collision with the terrain. Factors relating to the accident were: the pilot's lack of recent experience in the make and model of airplane, and the use of flaps during a light weight takeoff.
Final Report:

Crash of a Let L-410UVP in Riga: 2 killed

Date & Time: Jun 7, 1995 at 1300 LT
Type of aircraft:
Operator:
Registration:
146
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Riga - Riga
MSN:
83 11 35
YOM:
1983
Country:
Region:
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 flight at Riga-Lielvārdes AFB. While passing over runway 36 at a height of 150-200 metres, the pilot-in-command elected to make a barrel when control was lost. The aircraft crashed on runway and was destroyed, killing both occupants.
Probable cause:
Loss of control after the crew attempted hazardous manoeuvres.

Crash of a Convair CV-580F in Vitoria

Date & Time: May 19, 1995 at 1839 LT
Type of aircraft:
Operator:
Registration:
EC-899
Flight Type:
Survivors:
Yes
Schedule:
Vitoria - Vitoria
MSN:
354
YOM:
1956
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training mission at Vitoria Airport. In good weather conditions, the crew was approaching the airport in a flapless configuration when an alarm sounded in the cockpit. The crew turned off the circuit breaker so the alarm stopped. The aircraft landed on its belly and slid for few dozen metres before coming to rest. All four occupants escaped uninjured and the aircraft was damaged beyond repair.
Probable cause:
The aircraft belly landed after the crew failed to follow the approach checklist and turned off the circuit breaker.

Crash of a BAe Nimrod MR.2 off RAF Lossiemouth

Date & Time: May 16, 1995
Type of aircraft:
Operator:
Registration:
XW666
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Kinloss - Kinloss
MSN:
8041
YOM:
1970
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was one of three Nimrod reconnaissance variants and had just undergone a major servicing at the Nimrod Major Servicing Unit (NMSU), RAF Kinloss by RAF maintenance personnel. Nimrod XW666 departed on a routine post-servicing airtest. After approximately 35 minutes of flight, following a test of the aircraft's anti-icing system, the No 4 engine fire warning illuminated. Whilst the crew were carrying out the fire drill, the No 3 engine fire warning also illuminated. A rear crew member confirmed that the aircraft was on fire and advised the captain that panels were falling away from the starboard wing. After two explosions, the captain feared for the structural integrity of the aircraft and decided to ditch before he lost control authority. Without the aid of flaps, which failed to operate because of a fire/associated hydraulic failure, he completed a controlled ditching into the Moray Firth. The aircraft bounced twice onto the sea before settling. The fuselage broke into two and the aircraft subsequently sank. Parts were salvaged and the cockpit section is now on display at AeroVenture South Yorkshire Aircraft Museum in Doncaster.
Probable cause:
With the assistance of the Department of Transport's Air Accident Investigation Branch, the Inquiry established that despite the correct application of maintenance procedures, the DC electrical loom attached to No 4 engine had sustained mechanical damage, although it could not be positively determined how or when. Arcing occurred when the engine anti-icing system was switched on and this led to initiation of the air starter system. With the No 4 engine already running at idle as part of the overall airtest there was no load on the starter turbine, which quickly ran up to high speed. The nut holding the turbine disk in place failed, allowing the disk to move back on its shaft and out of its protective housing. It then struck the engine bypass casing and the No 2 fuel tank, puncturing both. The resultant fuel leak was ignited either by electrical arcing within the faulty DC loom or by the heat of the engine. The fire spread rapidly to the wing area and forward to the engine intake area. The Inquiry concluded that a sequence of technical difficulties led to the uncontained fire.

Crash of a De Havilland C-115 Buffalo at Ponta Pelada AFB

Date & Time: May 15, 1995
Type of aircraft:
Operator:
Registration:
2361
Flight Type:
Survivors:
Yes
Schedule:
Ponta Pelada AFB - Ponta Pelada AFB
MSN:
31
YOM:
1969
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Ponta Pelada AFB, Manaus. Upon landing, the aircraft went out of control, veered off runway and came to rest few dozen metres further. There were no casualties while the aircraft was damaged beyond repair.

Crash of a Cessna 501 Citation I/SP in San Salvador

Date & Time: Apr 24, 1995 at 1630 LT
Type of aircraft:
Operator:
Registration:
N120ES
Flight Type:
Survivors:
Yes
Schedule:
San Salvador - San Salvador
MSN:
501-0041
YOM:
1977
Country:
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 at San Salvador-Comalapa Airport. On approach to runway 25, the copilot informed the captain about a discrepancy between both altimeters. The crew elected to identify the problem and thus failed to focus his attention on the approach procedure. This caused the aircraft to lose altitude when it collided with trees located 2,500 feet short of runway and crashed on a road 1,200 feet short of runway. Both pilots escaped uninjured and the aircraft was damaged beyond repair.

Crash of a Canadair CC-144A Challenger 601 in Shearwater

Date & Time: Apr 24, 1995
Type of aircraft:
Operator:
Registration:
144613
Flight Type:
Survivors:
Yes
Schedule:
Shearwater - Shearwater
MSN:
3035
YOM:
1984
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew (one instructor and three pilots under training) departed Shearwater Airport on a local training mission. The crew decided to perform a flapless landing but the aircraft arrived too high and to correct the situation, the pilot-in-command nosed down when the aircraft landed very hard and bounced. The crew initiated a go-around procedure and decided to follow a holding pattern after being informed by ATC based in the tower that the right main gear seems to be damaged. About 40 minutes later, the right main gear fell away. The right engine then lost power and a fire erupted in the right wheel well. The crew declared an emergency and was cleared to return to Shearwater Airport. Upon landing, the aircraft sank on its right side then rolled for few dozen metres before coming to rest, bursting into flames. All four occupants escaped uninjured before an explosion occurred in the central fuel tank.
Probable cause:
It was determined that during the first hard landing, the right main gear was seriously damaged upon impact as well as hydraulic and fuel line.

Crash of a Cessna 208A Caravan I in Luziânia

Date & Time: Apr 11, 1995 at 1630 LT
Type of aircraft:
Operator:
Registration:
PT-OGO
Flight Type:
Survivors:
Yes
Schedule:
Luziânia - Luziânia
MSN:
208-0027
YOM:
1985
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine aircraft was dispatched at Luziânia Airport for local training purposes, carrying a crew of five consisting of one instructor and four pilot under training. Following several approaches, the aircraft was descending to the runway when the instructor reduced the engine power to simulate a failure. From a height of about 300 feet, the aircraft nosed down, lost height and crashed short of runway threshold. All five occupants were uninjured and the aircraft was written off.
Probable cause:
The following contributing factors were reported:
- The traffic and the high number of landings caused a natural fatigue by the instructor and reduced his appreciations,
- There were too much pilots under training for one single instructor,
- The copilot's experience was insufficient with only one hour on Cessna 208,
- Poor crew coordination,
- Poor crew action on engine power to expect recovery after stall.

Crash of a Harbin Yunsunji Y-12-II in Iquitos: 3 killed

Date & Time: Apr 4, 1995 at 0730 LT
Type of aircraft:
Operator:
Registration:
OB-1498
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Iquitos - Iquitos
MSN:
0049
YOM:
1992
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was engaged in a local training flight on behalf of the Peruvian Air Force. Shortly after takeoff from Moronacocha Airport, while in initial climb, the aircraft stalled and crashed, bursting into flames. All three crew members were killed.