Crash of a Xian Yunsunji Y-7H-100 off Nouadhibou: 8 killed

Date & Time: Apr 5, 1996
Type of aircraft:
Operator:
Registration:
5T-MAF
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Nouadhibou - Nouakchott
MSN:
00 7H 01
YOM:
1996
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
Shortly after takeoff from Nouadhibou Airport, while climbing, the aircraft stalled and crashed in the sea, killing all eight occupants.
Probable cause:
It is believed that the loss of control was the consequence of an engine failure.

Crash of a Beechcraft T-44A Pegasus in the Gulf of Mexico: 3 killed

Date & Time: Mar 25, 1996
Type of aircraft:
Operator:
Registration:
160839
Flight Phase:
Flight Type:
Survivors:
No
MSN:
LL-1
YOM:
1977
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Crashed in unknown circumstances in the Gulf of Mexico while completing a training mission. All three crew members, two pilots and an instructor, were killed.
Crew:
Cpt John Krafft,
1st Lt Ronald Pahl,
Ltjg Robert Roch.

Crash of a Cessna 402B off Punto Fijo: 8 killed

Date & Time: Mar 13, 1996 at 0815 LT
Type of aircraft:
Operator:
Registration:
P4-AVB
Survivors:
No
Schedule:
Oranjestad - Punto Fijo
MSN:
402B-1201
YOM:
1976
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The twin engine aircraft was completing a charter flight from Oranjestad to Punto Fijo with seven passengers and one pilot on board. While descending to Punto Fijo-Josefa Camejo Airport, the pilot informed ATC about the failure of the left engine. Shortly later, the left engine caught fire and detached, causing a part of the left wing to be torn off. Out of control, the aircraft crashed in the sea about 29,5 km north of Punto Fijo Airport. All eight occupants were killed.
Probable cause:
Failure of the left engine as a result of a cracked exhaust manifold.

Crash of a Cessna 421B Golden Eagle II off Vigan: 1 killed

Date & Time: Mar 3, 1996
Registration:
N69905
Flight Type:
Survivors:
No
Schedule:
Manila - Vigan
MSN:
421B-0537
YOM:
1973
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
On March 3,1996, at a time not reported, a Cessna 421B, N69905, registered to Hi Tech Aviation in Scottsdale, Arizona, reportedly crashed into the sea while attempting to land at the airport at Vigan in the Philippine Islands. The weather at the time and the circumstances of the accident were not reported. It was reported that the pilot was the only occupant onboard. According to the Philippine Air Transportation Office, the aircraft arrived in Manila on March 2, 1996. It departed the next day for a flight to Vigan to pick up a passenger with a return to Manila. It was last seen flying over the airport in the traffic pattern for landing. It is presumed to have crashed into the sea. The FAA aircraft records section in Oklahoma City, Oklahoma, indicated that they received a bill of sale from Hi Tech Aviation indicating the aircraft was sold to a company in Manila on 01/19/96.

Crash of a Piper PA-61P Aerostar (Ted Smith 601P) in the Atlantic Ocean: 1 killed

Date & Time: Feb 17, 1996 at 2130 LT
Operator:
Registration:
N956AF
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Swainsboro – Hilton Head
MSN:
61-0515-215
YOM:
1978
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
9850
Aircraft flight hours:
2884
Circumstances:
The pilot had departed Swainsboro, Georgia at 1930 EST on an IFR flight. About 12 minutes later, he informed Jacksonville Center that he was very dizzy and could not see. There were no other recorded transmissions from the pilot. The airplane was tracked on radar until radar contact was lost at 2130. The airplane was at a heading of 110 degrees and an altitude of 9,000 feet the entire time. Attempts to locate the airplane by aerial intercept were uneventful. All shipping vessels along the airplane's expected course, were notified of the airplane's estimated fuel exhaustion point. No contact was reported and the search was suspended. Prior to departing Swainsboro, the pilot had mentioned to his wife that he had a headache. A review of the pilot's medical records revealed that he had twice indicated on his application for a medical certificate that he had a medical history of unconsciousness. In addition, he was being treated for hypertension with Norvasc and chlorthalidone prescription drugs.
Probable cause:
Pilot incapacitation.
Final Report:

Crash of a Boeing 757-225 off Puerto Plata: 189 killed

Date & Time: Feb 6, 1996 at 2347 LT
Type of aircraft:
Operator:
Registration:
TC-GEN
Flight Phase:
Survivors:
No
Schedule:
Puerto Plata - Gander - Berlin - Frankfurt
MSN:
22206
YOM:
1983
Flight number:
KT301
Crew on board:
13
Crew fatalities:
Pax on board:
176
Pax fatalities:
Other fatalities:
Total fatalities:
189
Captain / Total flying hours:
24750
Captain / Total hours on type:
1875.00
Copilot / Total flying hours:
3500
Copilot / Total hours on type:
71
Aircraft flight hours:
29269
Aircraft flight cycles:
13499
Circumstances:
On behalf of Alas Nacionales, the aircraft was completing a charter flight from Puerto Plata to Frankfurt with intermediate stops in Gander and Berlin, carrying 176 Germans and 13 Turkish crew members. During the takeoff roll, at a speed of 80 knots, the captain noted that his air speed indicator (ASI) seemed to be incorrect while the copilot's ASI seemed to be correct. During initial climb, at an altitude of about 4,700 feet, the captain's ASI read 350 knots while the real speed was 220 knots. This resulted in an autopilot/autothrottle reaction to increase the pitch-up attitude and a power reduction in order to lower the airspeed. At that time the crew got 'Rudder ratio' and 'Mach airspeed' advisory warnings. Both pilots got confused when the copilot stated that his ASI read 200 knots decreasing while getting an excessive speed warning, followed by a stick shaker warning. This led the pilots to believe that both ASIs were unreliable. Finally realizing that they were losing speed and altitude they disconnected the autopilot. The autopilot, fed by the captain's faulty ASI, had reduced the speed close to the stall speed. Full thrust was then applied. At 23:47:17 an aural GPWS warning sounded and eight seconds later, the aircraft crashed in the ocean. All 189 occupants were killed.
Probable cause:
The crew's failure to recognize the activation of the stick shaker as a warning of an imminent stall, and the failure of the crew to execute the procedures for recovery from the onset of loss of control. Before the stick shaker warning activated, there was a confusion by the flight crew due to erroneous indications of relative speed increase and an overspeed warning. It is believed that the incorrect ASI readings was the consequence of an obstructed Pitot tube, maybe by mud and/or debris from a small insect that was introduced in the Pitot tube during the time the aircraft was on the ground. The aircraft was not flown for 20 days before the crash and was returned for service without a verification of the Pitot static system as recommended by Boeing.
Final Report:

Crash of a Partenavia AP.68TP-300S Spartacus off El Segundo: 1 killed

Date & Time: Jan 9, 1996 at 0914 LT
Type of aircraft:
Operator:
Registration:
N3116C
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oxnard - San Diego
MSN:
8007
YOM:
1987
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8963
Captain / Total hours on type:
1000.00
Aircraft flight hours:
4540
Circumstances:
The aircraft was destroyed after an uncontrolled descent into the Pacific ocean about 14 miles west-southwest of El Segundo, California. The pilot was presumed to have been fatally injured. According to a company search pilot, visual meteorological conditions prevailed at the accident area about 1.5 hours after the time of the accident. No flight plan was filed for the positioning flight which originated at Oxnard, California, on the morning of the accident for a flight to San Diego, California. The aircraft departed Oxnard on a special VFR clearance. The tops of the clouds were reported to be about 1,200 feet msl. The aircraft transitioned southbound through the NAWS Point Mugu airspace. The Point Mugu radar approach control monitored the aircraft on radar for about 25 miles. The pilot was subsequently given a frequency change to SOCAL Tracon. There was no contact made with that facility. A search was initiated when the aircraft failed to arrive at the intended destination. A review of the recorded radar data revealed the aircraft was level at 1,800 feet msl and then climbed to about 2,000 feet msl, at which time it disappeared from radar.
Probable cause:
Loss of control for undetermined reasons.
Final Report:

Crash of a Britten-Norman BN-2A-27 off Bridgetown: 1 killed

Date & Time: Jan 8, 1996
Type of aircraft:
Operator:
Registration:
J8-VAK
Flight Phase:
Survivors:
Yes
Schedule:
Union Island - Bridgetown
MSN:
436
YOM:
1975
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
En route from Union Island to Bridgetown-Grantley Adams Airport, while cruising at an altitude of 7,000 feet, the right engine failed. The pilot informed ATC about his situation on position and reduced his altitude to ditch the aircraft about 30 km southeast of Bridgetown. A passenger was killed while nine other occupants were rescued. The aircraft sank and was lost.
Probable cause:
Failure of the right engine in flight for unknown reasons.

Crash of a Socata TBM-700 in Braunschweig

Date & Time: Dec 8, 1995
Type of aircraft:
Operator:
Registration:
OE-EHG
Flight Type:
Survivors:
Yes
MSN:
28
YOM:
1991
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Braunschweig-Wolfsburg Airport, the pilot failed to realize his altitude was insufficient when the single engine aircraft struck power cables and crashed in the Oker River, about 3,5 short of runway 08 threshold. All six occupants were injured and the aircraft was destroyed.

Crash of a Piper PA-31-325 Navajo in Wollaston Lake

Date & Time: Nov 25, 1995 at 2325 LT
Type of aircraft:
Registration:
C-GOLM
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Wollaston Lake – La Ronge
MSN:
31-7712050
YOM:
1977
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4920
Captain / Total hours on type:
450.00
Aircraft flight hours:
7056
Circumstances:
The Eagle Air Services Piper PA-31-325 Navajo, C-GOLM, departed runway 34 at Wollaston Lake, Saskatchewan, at 2325 central standard time (CST), on a medical evacuation (MEDEVAC) flight to La Ronge. The flight was arranged by the Wollaston nursing station to transport a patient to a hospital in La Ronge. The patient was accompanied on the flight by her mother and a nurse from the nursing station. The aircraft was observed to climb at an unusually shallow angle after take-off, and, when efforts by company personnel to reach the pilot by radio were unsuccessful, a ground search was commenced. The aircraft was found about five minutes after the accident, located on the ice- and snow-covered surface of Wollaston Lake, about 0.75 nautical miles (nm) from the departure end of the runway, and about 1.3 nm from the point of commencement of the take-off roll. The pilot and the patient suffered serious injuries. The other two occupants sustained minor injuries. The accident occurred during the hours of darkness at latitude 58°6.98'N, longitude 103°10.79'W, at an elevation of 1,300 feet above sea level (asl). The temperature was about -25°/C.
Probable cause:
After take-off, the left propeller was likely on its start locks, which, as the airspeed increased, allowed the propeller to overspeed. The pilot was unable to resolve the situation in time to prevent the aircraft from striking the surface of Wollaston Lake. Contributing to the severity of the patient's injuries were the inadequate restraint provided by the stretcher and its restraining strap, the lack of standards regarding stretchers used in aircraft, and the lack of standards as to the operation of MEDEVAC flights.
Final Report: