Crash of a Learjet 35A in Great Falls

Date & Time: May 16, 1997 at 1314 LT
Type of aircraft:
Registration:
N1AH
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Great Falls - Dallas
MSN:
35-398
YOM:
1981
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8700
Captain / Total hours on type:
2000.00
Aircraft flight hours:
8019
Circumstances:
The captain reported: 'Shortly after V1...there was a loss of power to the left engine....' (FAR Part 1 defines V1 as takeoff decision speed.) However, the first officer, who was the pilot flying, stated the captain retarded power on the left engine as a training exercise. The first officer stated there was no preflight discussion of emergency procedure practice. The airplane became airborne about 3,500 feet down the runway; the crew subsequently lost control of the aircraft, and it crashed to the left of the runway, and a fire erupted. The crew escaped with minor injuries. A teardown of the left engine was performed under FAA supervision at the engine manufacturer's facilities; the engine manufacturer reported that damage found during the teardown 'was indicative of engine rotation and operation at the time of impact....' Both airspeed indicator bugs were found set 9 to 11 knots below the V1 speed on the takeoff and landing data (TOLD) card. No evidence of an aircraft or engine malfunction, to include inflight fire, was found at the accident site.
Probable cause:
The captain's inadequate preflight planning/preparation, and the subsequent improper response to a simulated loss of engine power, resulting in liftoff at an airspeed below that for which sustained flight was possible.
Final Report:

Crash of a Beechcraft B200C Super King Air in Steynsburg

Date & Time: May 10, 1997 at 1700 LT
Operator:
Registration:
ZS-LNV
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Steynsburg - Pretoria
MSN:
BL-71
YOM:
1983
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the twin engine aircraft struck a dip, causing a propeller to struck the ground and the aircraft to lose power and speed. Unable to take off, the aircraft veered off runway to the left, went through three fences, crossed a dirt road and came to rest in an open field. All seven occupants were rescued, among them one was slightly injured. The aircraft was dispatched in Steynsburg to enable five forensic experts and detectives to conduct an investigation of suspected arson, as the Grand Hotel at the town was destroyed by fire.

Crash of a Fokker F27 Friendship 600 in Brazzaville: 3 killed

Date & Time: Apr 14, 1997
Type of aircraft:
Operator:
Registration:
D2-TFP
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Brazzaville - Luanda
MSN:
10424
YOM:
1969
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Just after liftoff from runway 06, while in initial climb, the aircraft stalled and sank back on the runway. It skidded for few dozen metres, overran and came to rest 300 metres further, bursting into flames. Three crew members were killed while four others were seriously injured.
Probable cause:
It is believed that the cargo was not properly stored in the in the cargo compartment and that the CofG was aft the limit. The assumption that the cargo shifted at rotation was not ruled out.

Crash of an Aviation Traders ATL-98 Carvair in Griffin: 2 killed

Date & Time: Apr 4, 1997 at 0016 LT
Registration:
N83FA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Griffin – Americus – Rockford
MSN:
5/10365
YOM:
1944
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
12000
Captain / Total hours on type:
1000.00
Aircraft flight hours:
50558
Circumstances:
During the airplane's takeoff roll, about 3/4 down the 3,700 foot runway, a witness reported that the color of the #1 exhaust flame changed from blue to yellow, accompanied by an audible change in the engine power level. The nose of the airplane yawed left and the left wing dipped. Directional control was regained and the takeoff continued. Skid marks were found about 650 feet before the departure end of the runway that continued about 1360 feet to an abandoned grocery store impacted by the plane. About 315 feet before the building, the left wing contacted a privacy fence, and a utility pole, resulting in a fire at the disrupted left wing main fuel tank. A pilot/mechanic who helped dispatch the airplane observed that the elevator was free as it taxied. Fire damage to all engines precluded a detailed post crash examination of essential fuel and ignition systems. The toxicological report regarding the second pilot indicated that 1.110 mcg/ml (ug/ml, ug/g) of Diphenhydramine, was detected in the blood. According to NTSB medical personnel, Diphenhydramine is a sedating antihistamine often found in over-the-counter allergy medications. A single oral dose of medication containing Diphenhydramine, at twice the recommended maximum of over-the-counter dosage, resulted in maximal blood levels of between 0.08 and 0.16 mcg/ml. The level of Diphenhydramine found during the toxicology examination of the second pilot approximated ten times the levels found following a dosage at twice the recommended strength. Diphenhydramine was also found in the urine. Additional prescription and nonprescription medications were also found during the toxicological examination of the second pilot.
Probable cause:
The flightcrew's inadequate procedures, during a rejected takeoff following a possible engine malfunction at a critical time in the takeoff, and the second pilot's physical impairment.
Final Report:

Crash of a Convair CV-580 in Tshikapa

Date & Time: Apr 1, 1997
Type of aircraft:
Operator:
Registration:
9Q-CRU
Flight Phase:
Survivors:
Yes
Schedule:
Kinshasa – Tshikapa – Mbuji-Mayi
MSN:
41
YOM:
1967
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the captain heard a noise and suspected a technical problem so he decided to abandon the takeoff procedure. Unable to stop within the remaining distance, the aircraft overran and struck an embankment. All 14 occupants escaped uninjured while the aircraft was damaged beyond repair. It was reported that the crew initiated the takeoff in an up-slope configuration while the takeoffs at Tshikapa Airport are normally completed in a down-slope configuration. The runway is 1,000 metres long.

Crash of a Cessna 207A Skywagon in Nunapitchuk: 1 killed

Date & Time: Mar 25, 1997 at 1123 LT
Operator:
Registration:
N800GA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Scammon Bay - Bethel
MSN:
207-0495
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2437
Captain / Total hours on type:
1136.00
Aircraft flight hours:
10193
Circumstances:
The pilot of Cessna 207A, N800GA, was returning to his company base, passing about 2 miles north of a remote airstrip that was along the route of flight. The airstrip did not have any control tower. [Communications around an uncontrolled airport are conducted on a common traffic advisory frequency (CTAF)]. The pilot of a Short SC7, N451SA, announced his departure from the same airstrip on the CTAF, and took off in a northerly direction. He then began a climbing right turn toward the same destination as the Cessna 207A was proceeding. The two airplanes collided in mid-air, about 1.49 nautical miles east-northeast of the airstrip, which was about 18.3 miles west of their destination. They were observed spiraling downward from about 800 ft above the ground. Both airplanes were found lying flat and upright on a frozen lake, entangled together at the accident site. The Cessna's burned wreckage was lying on top of (and positioned toward the aft third of) the burned wreckage of the Short SC7.
Probable cause:
Inadequate visual look-out by the pilots of both airplanes, which resulted in their failure to see-and-avoid each other's airplanes.
Final Report:

Crash of a Short SC.7 Skyvan 3 Variant 100 in Nunapitchuk: 1 killed

Date & Time: Mar 25, 1997 at 1123 LT
Type of aircraft:
Operator:
Registration:
N451SA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Nunapitchuk - Bethel
MSN:
1972
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3170
Captain / Total hours on type:
130.00
Aircraft flight hours:
7473
Circumstances:
The pilot of Cessna 207A, N800GA, was returning to his company base, passing about 2 miles north of a remote airstrip that was along the route of flight. The airstrip did not have any control tower. [Communications around an uncontrolled airport are conducted on a common traffic advisory frequency (CTAF)]. The pilot of a Short SC7, N451SA, announced his departure from the same airstrip on the CTAF, and took off in a northerly direction. He then began a climbing right turn toward the same destination as the Cessna 207A was proceeding. The two airplanes collided in mid-air, about 1.49 nautical miles east-northeast of the airstrip, which was about 18.3 miles west of their destination. They were observed spiraling downward from about 800 ft above the ground. Both airplanes were found lying flat and upright on a frozen lake, entangled together at the accident site. The Cessna's burned wreckage was lying on top of (and positioned toward the aft third of) the burned wreckage of the Short SC7.
Probable cause:
inadequate visual look-out by the pilots of both airplanes, which resulted in their failure to see-and-avoid each other's airplanes.
Final Report:

Crash of an Airbus A320-212 in Abu Dhabi

Date & Time: Mar 10, 1997 at 1056 LT
Type of aircraft:
Operator:
Registration:
A4O-EM
Flight Phase:
Survivors:
Yes
Schedule:
Muscat – Abu Dhabi – Bahrain – Cairo
MSN:
536
YOM:
1995
Flight number:
GF071
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
107
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on runway 31 at Abu Dhabi Airport, just before V1, the aircraft started to vibrate and longitudinal control was lost. The captain decided to abandon the takeoff procedure and initiate an emergency braking manoeuvre. Unable to stop within the remaining distance, the aircraft overran, lost its nose gear and came to a halt few dozen metres further. On impact, the cockpit and both engines were almost destroyed and the left wing broke in two.
Probable cause:
It was determined that the vibration during the takeoff roll was the consequence of a tyre burst.

Crash of a Convair CV-240-27 near Hampton

Date & Time: Mar 7, 1997 at 1400 LT
Type of aircraft:
Registration:
N357T
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Griffin - Augusta
MSN:
340
YOM:
1953
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18000
Captain / Total hours on type:
35.00
Aircraft flight hours:
16331
Circumstances:
About two minutes into the flight, the pilot noticed a high cylinder head temperature on the right engine. The pilot opened the cowl flap doors and the cylinder head temperature dropped 200 degrees. When the pilot noticed a reduction in right engine power, he elected to shut down the engine. The copilot was instructed to secure the right engine in accordance with the emergency procedures. Unable to maintain altitude, the pilot selected an emergency landing to a large open field, and the landing gear collapsed during the landing. Examination of the airplane at the accident site disclosed that the engine cowl flaps on both engines were in the open position. Examinations of the right engine subsystems failed to disclose a mechanical malfunction or component failure. A review of the normal and emergency procedures for the aircraft disclosed that the cowl flaps normal position for the shutdown engine is closed. A review of the aircraft performance data revealed that the airplane was capable of maintaining flight and a climb attitude with one engine. There was no cargo on the airplane. During the pilot's subsequent type rating reexamination in the Convair 240-27, the pilot failed to demonstrate a satisfactory level of knowledge in emergency procedures during the oral examination. The pilot subsequently surrendered the Convair 240-27 type rating to the FAA.
Probable cause:
A partial loss of power on one engine for undetermined reason(s), and the pilot's failure to follow aircraft emergency procedures. A factor was inadequate transition/upgrade training.
Final Report:

Crash of a Cessna 500 Citation I near La Felisa: 2 killed

Date & Time: Mar 7, 1997 at 0934 LT
Type of aircraft:
Registration:
HK-3885
Flight Phase:
Survivors:
No
Site:
Schedule:
Pereira - Medellín
MSN:
500-0135
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3048
Copilot / Total flying hours:
173
Aircraft flight hours:
6274
Circumstances:
After takeoff from Pereira-Matecaña Airport, while climbing, the copilot declared an emergency and reported problems. Shortly later, the aircraft entered an uncontrolled descent and crashed near La Felisa. The aircraft was destroyed and both pilots were killed.
Probable cause:
In-flight braking and subsequent separation of both wing tips due to positive wing loading imposed by the unqualified crew exceeding the structural limit stipulated by the manufacturer.
Final Report: