Crash of a Mitsubishi MU-2B-26A Marquise in Martha’s Vineyard: 4 killed

Date & Time: Oct 6, 2000 at 2158 LT
Type of aircraft:
Registration:
N60BT
Flight Type:
Survivors:
No
Schedule:
Trenton – Martha’s Vineyard
MSN:
358
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1946
Captain / Total hours on type:
253.00
Aircraft flight hours:
5400
Circumstances:
The pilot departed on a night cross-country flight without obtaining a weather briefing or flight plan. Arriving in the area of the destination airport, the weather was reported as, 2 statute miles of visibility and mist; overcast cloud layer at 100 feet. The pilot requested an instrument flight rules clearance from the approach controller, and was vectored and cleared for the ILS 24 approach. The clearance included an altitude restriction of 1,500 feet msl, until the airplane was established on the localizer. As the pilot contacted the control tower, the tower controller issued a low altitude alert to the pilot. The pilot replied that he was climbing and the tower controller cleared the pilot to land, which the pilot acknowledged. No further pertinent radio transmissions were received from the airplane. The airplane came to rest in a wooded area about 3/4-mile from the runway threshold, and about 50 feet right of the extended centerline. Review of the approach plate for the ILS 24 approach revealed that the minimum glide slope intercept altitude at the beginning of the final approach segment on the precision approach was 1,500 feet. The glide slope altitude at the final approach fix for the non-precision approach, which was located about 4 miles from the approach end of the runway, was 1,407 feet. The glide slope altitude at the middle marker, which was located about 0.6 miles from the approach end of the runway, was 299 feet. Review of radar data revealed that the airplane was observed at 700 feet, about 4 miles from the airport, and at 300 feet, about 1.5 miles from the airport. The pilot had accumulated about 1,946 hours of total flight experience, with about 252 hours in make and model. The pilot had attended initial and recurrent training for the make and model airplane; however, did not complete the training. The pilot, aged 61, was Charles B. Yates, member of the New Jersey Senate, who was flying to Martha's Vineyard with his wife and two of his three children.
Probable cause:
The pilot's failure to follow instrument flight procedures resulting in a collision with a tree. A factor related to the accident was the low cloud ceiling.
Final Report:

Crash of a Douglas DC-9-31 in Reynosa: 4 killed

Date & Time: Oct 6, 2000 at 1655 LT
Type of aircraft:
Operator:
Registration:
N936ML
Survivors:
Yes
Schedule:
Mexico City - Reynosa
MSN:
47501
YOM:
1970
Flight number:
AM250
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
85
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
10184
Captain / Total hours on type:
701.00
Copilot / Total flying hours:
1764
Copilot / Total hours on type:
40
Aircraft flight hours:
74277
Circumstances:
Following an uneventful flight from Mexico City, the crew started the descent to Reynosa-General Lucio Blanco Airport and encountered poor weather conditions with heavy rain falls issued from the tropical storm 'Keith'. Following a wrong approach configuration, the aircraft was too high on the glide and approaching at an excessive speed. It landed too far down the wet runway 31 and was unable to stop within the remaining distance. It overran, lost its undercarriage, struck several houses, went down an embankment and came to rest in a canal. All 90 occupants were rescued, among them one passenger was slightly injured. On the ground, four people were killed.
Probable cause:
Long landing and contact, after a high approach with excessive speed as a result of a non-precision approach, on a waterlogged runway and in adverse weather conditions (discharge of CB's in the area), with the aircraft departing from the opposite runway threshold (13).
Final Report:

Crash of an Antonov AN-72 in Luzamba

Date & Time: Oct 6, 2000
Type of aircraft:
Operator:
Registration:
TL-ACW
Flight Type:
Survivors:
Yes
MSN:
36572090796
YOM:
1990
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Luzamba Airport, the crew encountered atmospheric turbulences. The captain increased engine power, causing the approach speed to increase as well. The aircraft, too high, landed too far down the runway. Realizing the situation after touchdown, the captain abandoned the landing manoeuvre and initiated a go-around procedure. While climbing, the crew was aware he should follow a downwind circuit at low height because of hostile actions in the area. During the second approach, the crew forgot to lower the landing gear so the aircraft landed on its belly and slid for about 350 metres before coming to rest on the runway. All 10 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The crew failed to follow the approach checklist and forgot to lower the landing gear during the second approach. As the landing gear were not lowered, an alarm sounded in the cockpit but the crew thought this was a mistake and failed to lower the gear or to initiate a second go-around procedure.

Crash of an Antonov AN-12BK in Petrel

Date & Time: Oct 3, 2000
Type of aircraft:
Operator:
Registration:
04 red
Flight Type:
Survivors:
Yes
MSN:
8 34 60 05
YOM:
1968
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing, the four engine aircraft was unable to stop within the remaining distance. It overran, lost its undercarriage and came to rest 200 metres further. There were no casualties but the aircraft was damaged beyond repair.

Crash of a Cessna 340 off Nadi

Date & Time: Sep 29, 2000 at 1600 LT
Type of aircraft:
Registration:
N130DR
Flight Type:
Survivors:
Yes
Schedule:
Nouméa - Nadi
MSN:
340-0041
YOM:
1972
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On September 29, 2000, at 1600 hours local time, a Cessna 340, N130DR, was destroyed when it impacted the water in Nadi Bay, about 1,500 feet short of the runway 09 threshold at Nadi International Airport in the Republic of the Fiji Islands. The commercial pilot, a citizen of the United States and the sole occupant, received minor injuries. Visual meteorological conditions prevailed for the ferry flight, operated by Benchmark Aviation under 14 CFR Part 91, that departed from Magenta Airport, New Caledonia, NWWM at 1200.

Crash of a Convair CV-580 in La Grande-4

Date & Time: Sep 27, 2000 at 1038 LT
Type of aircraft:
Operator:
Registration:
C-GFHH
Survivors:
Yes
Schedule:
Montreal – Rouyn – La Grande-3 (LG-3) – La Grande-4 (LG-4) – Montreal
MSN:
109
YOM:
1953
Flight number:
APZ180
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15500
Captain / Total hours on type:
6000.00
Copilot / Total flying hours:
11000
Copilot / Total hours on type:
4000
Aircraft flight hours:
78438
Circumstances:
The Hydro-Québec Convair 340 (580), registration C-GFHH, serial number 109, with 18 passengers and 4 crew members on board, made an instrument flight rules flight from La Grande 3 to La Grande 4, Quebec. The aircraft touched down on the snow-covered runway at La Grande 4 approximately 800 feet beyond the runway threshold. Shortly after the nose wheel touched down and the pilot set the propellers to reverse pitch, the aircraft drifted to the right. Despite the attempts of the pilot flying (the captain) to correct, the aircraft continued its course and exited the south side of Runway 09 at approximately 50 knots. The aircraft travelled 350 feet over soft, rocky ground and came to rest about 120 feet outside the runway edge, about 2500 feet from the runway threshold. The flight crew followed the procedure to shut down the engines, but the left engine would not stop. On the captain's order, the first officer went into the passenger cabin and ordered an evacuation. All passengers exited the aircraft via the window emergency exits over the right wing. The left engine eventually shut down on its own after about 15 minutes. Five persons sustained minor injuries. The aircraft sustained substantial damage but did not catch fire.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The steering control valve lever was not reassembled in accordance with the specifications and the drawings in the overhaul manual and the maintenance manual: the lever was assembled with two washers instead of one, and the circumference of the bushing was 0.0005 inch greater than the circumference of the hole in the lever. These two deficiencies created additional resistance that
impeded the pivoting of the aircraft steering wheel.
2. The nylon locknuts were reinstalled during the repair of the steering control valve, contrary to the recommendation that they be used only once. The locknuts then came loose in service, creating play in the parts of the valve.
3. Incorrect interpretation of the problem and the influence of previous experience using the nose-gear steering wheel led the crew to make the flight despite their concern about the aircraft's nose-gear steering system.
Findings as to Risk:
1. The maintenance personnel of Precision Aero Components Inc. used the (incomplete) maintenance manual instead of the overhaul manual to overhaul and repair the steering control valve,
contributing to the incorrect reassembly of the valve.
2. The steering control valve lever was not fitted with a grease fitting, and the outside of the bushing was not grooved to allow adequate lubrication, thereby risking corrosion and seizure of the bushing inside the lever.
3. The limited experience and the lack of formal training of the maintenance personnel concerning the repair and the overhaul on the steering control valve might have contributed to the incorrect
reassembly of the steering control valve.
4. The pilot flying cut the electrical power, as required by the hard landing procedure. The left engine could therefore not be shut down, causing a risk of injury when the passengers evacuated.
5. The pilot flying cut the electrical power after the aircraft exited the runway, as required by the hard landing procedure. The electrical power required to operate the public address and alarm systems was thereby lost, and the evacuation could not be ordered promptly.
6. The evacuation slide automatic deployment system was inadvertently deactivated, which could have delayed the evacuation and compromised passenger safety.
7. After separating from the engine, the left propeller blades entered the fuselage and damaged an unoccupied seat.
Other Findings:
1. The numerous changes in ownership of the Convair type certificate and the lack of technical support from the current holder caused maintenance problems for Convair operators and approved
maintenance organizations (AMOs), particularly for recently established AMOs.

Crash of a Douglas C-47B in Charlotte

Date & Time: Sep 26, 2000 at 0635 LT
Operator:
Registration:
N12907
Flight Type:
Survivors:
Yes
Schedule:
Anderson - Charlotte
MSN:
15742/27187
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10500
Captain / Total hours on type:
7500.00
Aircraft flight hours:
17425
Circumstances:
After an approach to runway 5, and touched down at 85 knots, the airplane yawed right, exited the runway, the right main landing gear collapsed, and the airplane nosed over. Examination of the airplane revealed that a right main wheel brake had locked up, and the landing gear had collapsed. Inspection of the right main landing gear assembly and all associated components could not provide any determination as to what caused the main wheel brake to lockup. The brake assembly was broken down into its component parts and inspected. No evidence of malfunction could be detected. No contamination of the hydraulic fluid was evident.
Probable cause:
The right main brake locked after touchdown causing the airplane to yaw and depart the runway, resulting in the landing gear collapsing.
Final Report:

Crash of a Cessna 208B Super Cargomaster in Greenville

Date & Time: Sep 23, 2000 at 1950 LT
Type of aircraft:
Operator:
Registration:
N590TA
Flight Type:
Survivors:
Yes
Schedule:
Bangor - Greenville
MSN:
208B-0590
YOM:
1997
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5350
Captain / Total hours on type:
2000.00
Aircraft flight hours:
2671
Circumstances:
According to the pilot, he was conducting a GPS approach during occasional low ceilings, reduced visibility and rain. At the minimum descent altitude, the ground was 'occasionally' visible through fog and rain. Near the missed approach point, the runway lights were visible, so he continued the descent. He lost visual contact with the runway, and began a missed approach, but collided with trees. The accident site was 2 miles prior to the runway, on rising terrain, 200 feet below the runway elevation. The missed approach point was over the approach end of the runway.
Probable cause:
The pilot's improper in-flight decision to continue his descent without visual contact with the runway, and his inattention to his altitude, in relation to the airport elevation.
Final Report:

Crash of a Boeing 707312B in Niamey

Date & Time: Sep 21, 2000 at 2050 LT
Type of aircraft:
Registration:
5V-TAG
Flight Type:
Survivors:
Yes
Schedule:
Paris - Valencia - Niamey
MSN:
19739
YOM:
1968
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The four engine aircraft departed Paris-Le Bourget Airport on a flight to Valencia, Spain, where members of the chorus of the University of Bénin-Togo were dropped off. At the end of the afternoon, the crew departed Valencia on the final leg of the day to Lomé, Togo. While in cruising altitude over the Niger territory, the crew informed ATC about smoke spreading in the cockpit and was cleared for an emergency descent and landing at Niamey-Diori Hamani Airport. On approach, due to the failure of the hydraulic systems, the crew was unable to lower the undercarriage so a belly landing was completed. The aircraft slid for few dozen metres before coming to rest, bursting into flames. All 10 occupants escaped uninjured while the aircraft was destroyed by fire.
Probable cause:
It is believed that the in-flight smoke and fire was the consequence of an electrical short-circuit.

Crash of a Piper PA-31-325 Navajo in Jeffersonville

Date & Time: Sep 20, 2000 at 1930 LT
Type of aircraft:
Registration:
N63706
Survivors:
Yes
Schedule:
Elizabethtown - Jeffersonville
MSN:
31-7712035
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2117
Captain / Total hours on type:
889.00
Aircraft flight hours:
3910
Circumstances:
The pilot said that he 'landed properly' on the runway, touching down at about 700 feet from the approach end. He said that he 'applied brakes, which had no effect, ran out of runway, and turned to the right to avoid trees. [The] Grassy field should have worked out, except for the drainage ditch.' The pilot said that later he was told that there was a tail wind estimated at 45 knots, when he landed. Examination of the airplane revealed no anomalies. Approximately 34 minutes before the accident, the weather observation at Louisville, Kentucky, 11 miles south of the accident site, reported winds of 320 degrees at 16 knots, with gusts to 20 knots.
Probable cause:
The pilot's inadequate normal braking and the pilot's inability to stop the airplane on the runway. Factors relating to this accident were the hydroplaning conditions, wet runway, the tailwind, the trees, and the ravine.
Final Report: