Crash of a Piper PA-46-310P Malibu in Sion

Date & Time: Nov 4, 1994 at 2030 LT
Operator:
Registration:
HB-PIP
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Sion - Sion
MSN:
46-8508091
YOM:
1985
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2468
Captain / Total hours on type:
1.00
Copilot / Total flying hours:
3097
Copilot / Total hours on type:
167
Aircraft flight hours:
2780
Circumstances:
Owned by the Federal Office of Civil Aviation (FOCA), the aircraft was dispatched at Sion Airport to perform several local training flight. At the end of the day, a pilot under training and an FOCA inspector decided to complete a local training flight out of Sion Airport. The single engine aircraft took off at 1935LT and the crew completed several touch-and-go maneuvers. Less than an hour later, after takeoff from runway 26, while in initial climb, the engine failed. The crew attempted to make an emergency landing in an open field when the aircraft collided with a car on a street and crashed on the ground. Both pilots escaped with minor injuries while one people in the car was seriously injured. The aircraft and the car were destroyed.
Probable cause:
Engine failure during initial climb due to fuel exhaustion. Investigations revealed that during the flight preparation, the flight inspector was the victim either of a mistake or of a lack of attention when he checked the quantities in the fuel tanks, an operation carried out at night using a flashlight which was uneasy. The aircraft already flew for three hours prior to the accident and no fuel was added prior to the present flight.
Final Report:

Crash of a Pilatus PC-6/B1-H2 Turbo Porter in Raeford

Date & Time: Jul 9, 1994 at 1015 LT
Operator:
Registration:
N111FX
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Raeford - Raeford
MSN:
701
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3000
Captain / Total hours on type:
108.00
Aircraft flight hours:
9960
Circumstances:
The pilot was performing the initial takeoff, when he observed a loss of power, associated with a torque indication of zero. He force landed the aircraft in a wooded area when he could not make an open field. A post accident inspection of the engine revealed that the fuel control unit arm was loose, and the lock wire was not in place. The arm was positioned so that a maximum power demand from the throttle would correspond to an idle power demand at the fuel control. The engine underwent a 100 hour inspection, by company maintenance personnel, 8 days prior to the accident. The inspection checklist called for examining the fuel control linkage for security.
Probable cause:
The improper inspection of the aircraft by company maintenance personnel, which resulted in an unsafetied and disconnected fuel control arm.
Final Report:

Crash of a Boeing B-52H Stratofortress at Fairchild AFB: 4 killed

Date & Time: Jun 24, 1994 at 1416 LT
Type of aircraft:
Operator:
Registration:
61-0026
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Fairchild AFB - Fairchild AFB
MSN:
464453
YOM:
1960
Flight number:
Czar 52
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
In preparation for the 1994 Fairchild Airshow, the Pilot Lt Col Arthur A. "Bud" Holland was again selected as the command pilot for the B-52 demonstration flight. On 15 June 1994, Holland briefed the new wing commander, Colonel William Brooks, on the proposed flight plan. Holland's demonstration profile violated numerous regulations, including steep bank angles, low-altitude passes, and steep pitch attitudes. Brooks ordered Holland not to exceed 45° bank angle or 25° pitch attitude during the demonstration. During the first practice session, on 17 June, Holland repeatedly violated these orders. Brooks witnessed this, but took no action. Pellerin flew with Holland on that flight and reported to Brooks that, "the profile looks good to him; looks very safe, well within parameters." The next practice flight on 24 June ended with the fatal crash. The demonstration profile designed by Holland included a 360° turn around Fairchild's control tower, a maneuver which he had not attempted in previous air show demonstrations. During the final flight, Holland performed a series of 60° bank turns and a 68° pitch climb in violation of Brooks' orders. There is no evidence to suggest that either McGeehan or Wolff attempted to intervene as Holland carried out these dangerous maneuvers. Pellerin was originally scheduled to fly in this mission, as he had done on the 17 June flight, but he was unavailable for the 24 June flight and Wolff was selected as the replacement aircrew member. Due to the short notice of his assignment to the mission, Wolff did not participate in the pre-flight briefing and boarded the aircraft after the engines were started. He was therefore unaware of the planned mission profile and had no opportunity to raise any objections before take-off. All of the four aircrew involved in the crash had only limited flying time in the months before the crash. It would appear that none of them had noticed that the aircraft had stalled until shortly before impact, as indicated by a failure to apply standard recovery techniques to the aircraft once it entered the stall. The investigation reported that even if the proper stall recovery techniques had been applied, it was unlikely that the accident could have been prevented as the aircraft was already flying too low to be recovered.
Crew:
Lt Col Arthur A. "Bud" Holland, pilot,
Lt Col Mark C. McGeehan, copilot,
Col Robert E. Wolff, observer,
Lt Col Kenneth "Ken" Huston, operations officer.
Probable cause:
The accident investigation concluded that the crash was primarily attributable to Holland's personality and behavior, USAF leaders' inadequate reactions to the previous incidents involving Holland, and the sequence of events and aircrew response during the final flight of the aircraft. Holland's disregard for procedures governing the safe operation of the B-52 aircraft that he commanded and the absence of firm and consistent corrective action by his superior officers allowed Holland to believe that he could conduct his flight in an unsafe manner, culminating with the slow, steeply banked, 360° turn around the control tower. The other environmental factors involved, including the addition of a new maneuver (the 360° turn around the tower), inadequate pre-flight involvement of Wolff, and the distractions from the base shooting four days prior, combined with Holland's unsafe and risk-taking piloting behavior to produce conditions favorable for the crash to occur. The final factor, according to the USAF investigation report, was the 10-knot (19 km/h) wind and its effect on the maneuvers required to achieve the intended flightpath in relation to the ground.

Crash of a Cessna 402B in Malacca

Date & Time: Apr 15, 1994
Type of aircraft:
Operator:
Registration:
M27-07
Flight Type:
Survivors:
Yes
Schedule:
Malacca - Malacca
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew consisting of two trainee pilots and one instructor departed Malacca-Batu Berendam Airport in the morning on a local training flight. Seventeen minutes after takeoff, the crew was returning to his departure point. For unknown reasons, the twin engine aircraft landed hard and came to rest, bursting into flames. All three occupants evacuated safely while the aircraft was written off. It was reported that one of the two pilots under training was attached to the Cambodian Air Force.

Crash of a De Havilland DHC-6 Twin Otter 300 in Tripoli: 1 killed

Date & Time: Mar 19, 1994
Registration:
5A-DJK
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Tripoli - Tripoli
MSN:
775
YOM:
1981
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was completing a local training flight at Tripoli Airport when the aircraft crashed in unknown circumstances near the airfield. The copilot was seriously injured while the captain/instructor was killed.

Crash of a Boeing 737-2R4C in New Delhi: 5 killed

Date & Time: Mar 8, 1994 at 1454 LT
Type of aircraft:
Operator:
Registration:
VT-SIA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
New Delhi - New Delhi
MSN:
21763
YOM:
1979
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
7263
Captain / Total hours on type:
2821.00
Copilot / Total flying hours:
556
Copilot / Total hours on type:
166
Aircraft flight hours:
25947
Aircraft flight cycles:
2861
Circumstances:
The aircraft was engaged in a local training flight at New Delhi-Indira Gandhi Airport, carrying one instructor and three trainee pilots. Five circuits and landings were completed uneventfully and during the sixth touch-and-go exercice, after take off from runway 28, the aircraft took a left turn and crashed on the international apron. The aircraft collided with an Aeroflot Ilyushin II-86 registered RA-86119 that was parked on the apron, bay n°45. Both aircraft were destroyed by fire. All four crew members on board the Boeing 737 were killed as well as four people on board the II-86 and one on the ground.
Probable cause:
Loss of control after rotation due to application of wrong rudder by trainee pilot during engine failure exercice. The instructor did not guard/block the rudder control and give clear commands as instructor so as to obviate the application of wrong rudder control by the trainee pilot.
Final Report:

Crash of a Fokker F27 Friendship 60 in Dar es Salaam

Date & Time: Dec 12, 1993
Type of aircraft:
Operator:
Registration:
5H-MPT
Flight Type:
Survivors:
Yes
Schedule:
Dar es Salaam - Dar es Salaam
MSN:
10566
YOM:
1977
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8700
Circumstances:
The crew was completing a local training flight at Dar es Salaam Airport. The aircraft landed at an excessive speed and in a flapless configuration. Upon touchdown, the undercarriage were torn off and the aircraft came to rest on its belly. Both pilots escaped uninjured but the aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the crew. The following contributing factors were reported:
- Poor flight preparation,
- The crew failed to follow the approach checklist,
- The crew failed to proceed to an approach briefing,
- Excessive approach speed,
- The crew failed to realize the flaps were not selected down.

Crash of an Antonov AN-2 in Yegoryevsk: 2 killed

Date & Time: Aug 16, 1993
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Yegoryevsk - Yegoryevsk
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Two pilots, one German pilot under supervision and one instructor took place on board the aircraft for a local training flight out from Yegoryevsk. After takeoff, while in initial climb, the crew initiated a left turn when the aircraft struck trees and crashed on a military parking lot, bursting into flames. Both occupants were killed.

Crash of a Convair CV-240 in Boise

Date & Time: Jul 27, 1993 at 1317 LT
Type of aircraft:
Registration:
N156PA
Flight Type:
Survivors:
Yes
Schedule:
Boise - Boise
MSN:
324
YOM:
1953
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2128
Captain / Total hours on type:
1400.00
Copilot / Total hours on type:
1
Circumstances:
Left seat pilot was receiving a flight check for ATP and CV-240 type rating; right seat pilot was FAA OPS inspector. Following a simulated single-engine approach the airplane landed wheels up. Left seat pilot had received a total of 1.4 hrs left seat training in CV-240 prior to this flight; log book not endorsed.
Probable cause:
The pilot's failure to extend the landing gear, and the check pilot's inadequate supervision. A factor in the accident was the pilot's inadequate upgrade training by the company.
Final Report:

Crash of a Lockheed C-130E Hercules in Wainwright: 5 killed

Date & Time: Jul 22, 1993
Type of aircraft:
Operator:
Registration:
130321
Flight Type:
Survivors:
Yes
Schedule:
Wainwright - Wainwright
MSN:
4191
YOM:
1967
Flight number:
Trucker 21
Country:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The aircraft was dispatched at Wainwright Airport to practice cargo drop and parachute deployment test. While passing over the runway at low height, the aircraft went out of control, struck the runway surface and crashed, bursting into flames. Five crew members were killed in the accident. The call sign is not confirmed.
Those killed were:
Cpt Michael G. Allen,
Cpt Vincent L. Schurman,
M/WO Joseph Sylvio Castonguay,
Sgt Alain Michaud,
M/Cpl Ronald J. McWilliam.