Crash of an Embraer EMB-110P1 Bandeirante in Cootamundra

Date & Time: Jun 25, 2001 at 1021 LT
Operator:
Registration:
VH-OZG
Survivors:
Yes
Schedule:
Sydney – Griffith
MSN:
110-241
YOM:
1980
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6850
Captain / Total hours on type:
253.00
Circumstances:
The Embraer EMB-110P1 Bandeirante, VH-OZG, departed from Sydney Kingsford Smith international airport at 0855 on 25 June 2001, on a single-pilot instrument flight rules (IFR) charter flight to Griffith. The nine occupants on board the aircraft included the pilot and eight passengers. At about 0945, while maintaining an altitude of 10,000 ft, the master caution light illuminated. At the same time, the multiple alarm panel ‘GENERATOR 2’ (right generator) warning light also illuminated, indicating that the generator was no longer supplying power to the main electrical bus bar. After resetting the generator and monitoring its output, the pilot was satisfied that it was operating normally. A short time later, the master warning light illuminated again. A number of circuit breakers tripped, accompanied by multiple master alarm panel warnings. The red ‘FIRE’ warning light on the right engine fire extinguisher ‘T’ handle also illuminated, accompanied by the aural fire alarm warning. The pilot reported that after silencing the aural fire alarm, he carried out the engine fire emergency checklist actions. However, he was unable to select the fuel cut-off position with the right fuel condition lever, despite overriding the locking mechanism using his left thumb while attempting to operate the lever with his right hand. He also reported that the propeller lever did not remain in the feathered detent, but moved forward, as if spring-loaded, to an intermediate position. After unsuccessfully attempting to select fuel cut-off with the right fuel condition lever, or feather the right propeller with the propeller lever, the pilot pulled the right ‘T’ handle to discharge the fire bottle. The amber discharge light illuminated and a short time later the fire alarm sounded again. Passengers reported seeing lights illuminated on the multiple alarm panel and heard the sound of a continuous fire alarm in the cockpit. At 0956, the pilot notified air traffic services (ATS) that there was a ‘problem’ with the aircraft, but did not specify the nature of that problem. Almost immediately the pilot transmitted a PAN radio call and advised ATS that there was a fire on board the aircraft. The nearest aerodromes for an emergency landing were not available due to fog, and the pilot decided to divert to Young, which was about 35 NM to the south east of the aircraft’s position at that time. The pilot advised ATS that the fire was extinguished, and that he was diverting the aircraft to Young. Two minutes later, the pilot repeated his advice to ATS stating that a fire in the right engine had been extinguished, and requested emergency services for the aircraft’s arrival at Young. The pilot informed one of the passengers that there was an engine fire warning, and that they would be landing at Young. The passengers subsequently reported seeing flames in the right engine nacelle and white smoke streaming from under the wing. Smoke had also started to enter the cabin in the vicinity of the wing root. The pilot subsequently reported that he had selected the master switch on the air conditioning control panel to the ‘vent’ position, and that he had opened the left direct vision window in an attempt to eliminate smoke from the cabin. When that did not appear to have any effect he closed the direct vision window. The pilot of another aircraft reported to ATS that Young was clear, but there were fog patches to the north. On arrival at Young, however, the pilot of the Bandeirante was unable to land the aircraft because of fog, and advised ATS that he was proceeding to Cootamundra, 27 NM to the south southwest of Young. The crew of an overflying airliner informed ATS that Cootamundra was clear of fog. ATS confirmed that advice by telephoning an aircraft operator at Cootamundra aerodrome. At 1017 thick smoke entered the cabin and the pilot transmitted a MAYDAY. He reported that the aircraft was 9 NM from Cootamundra, and ATS informed him that the aerodrome was clear of fog. The pilot advised that he was flying in visual conditions and that there was a serious fire on board. No further radio transmissions were heard from the aircraft. At 1021, approximately 25 minutes after first reporting a fire, the pilot made an approach to land on runway 16 at Cootamundra. He reported that when he selected the landing gear down on late final there was no indication that the gear had extended. The pilot reported that he did not have sufficient time to extend the gear manually using the emergency procedure because he was anxious to get the aircraft on the ground as quickly as possible. Unaware that the right main landing gear had extended the pilot advised the passengers to prepare for a ‘belly’ landing. He lowered full flap, selected the propeller levers to the feathered position and the condition levers to fuel cut-off. The aircraft landed with only the right main landing gear extended. The right main wheel touched down about 260 m beyond the runway threshold, about one metre from the right edge of the runway. During the landing roll the aircraft settled on the nose and the left engine nacelle and skidded for approximately 450 m before veering left off the bitumen. The soft grass surface swung the aircraft sharply left, and it came to a stop on the grass flight strip east of the runway, almost on a reciprocal heading. The pilot and passengers were uninjured, and vacated the aircraft through the cabin door and left overwing emergency exit. Personnel from a maintenance organisation at the aerodrome extinguished the fire in the right engine nacelle using portable fire extinguishers.
Probable cause:
Significant factors:
1. Vibration from the worn armature shaft of the right starter generator resulted in a fractured fuel return line.
2. The armature shaft of the right engine starter generator failed in-flight.
3. Sparks or frictional heat generated by the failed starter generator ignited the combustible fuel/air mixture in the right engine accessory compartment.
4. Items on the engine fire emergency checklist were not completed, and the fire was not suppressed.
5. The operator’s CASA approved emergency checklist did not contain smoke evacuation procedures.
6. The pilot did not attempt to extend the landing gear using the emergency gear extension when he did not to get a positive indication that the gear was down and locked.
7. The aircraft landed on the right main landing gear and slid to a stop on the right main gear, left engine nacelle and nose.
Final Report:

Crash of a Partenavia P.68C Victor in Ikorodu: 2 killed

Date & Time: Jun 16, 2001
Type of aircraft:
Registration:
5N-ATE
Flight Phase:
Survivors:
Yes
Schedule:
Lagos – Calabar
MSN:
244
YOM:
1981
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Few minutes after takeoff from Lagos-Murtala Muhammed Airport, en route to Calabar, the pilot informed ATC about engine problems and was cleared to return. He apparently attempted an emergency landing when the aircraft struck a tree and crashed in Igbogbo, in the southern suburb of Ikorodu, about 25 km east of Lagos Airport. A passenger was seriously injured while the pilot and the second passenger were killed.

Crash of a Piper PA-31-310 Navajo in Charlottetown: 3 killed

Date & Time: Jun 5, 2001 at 1621 LT
Type of aircraft:
Operator:
Registration:
C-GMTT
Flight Phase:
Survivors:
Yes
Schedule:
Gander – Charlottetown – Natuashish
MSN:
31-7712004
YOM:
1977
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
2085
Captain / Total hours on type:
185.00
Circumstances:
The flight took off on Runway 22 at Gander, Newfoundland and Labrador, at 1428 Newfoundland daylight time with the pilot and four passengers on board. Their destination was Sango Bay, Newfoundland and Labrador, with an intermediate stop in Charlottetown, Newfoundland and Labrador, to drop off one of the passengers. Radar data show that, on departure from Gander, the aircraft climbed at about 500 feet per minute at 125 knots ground speed to 2500 feet, then descended and proceeded en route to Charlottetown at 1900 feet and 150 knots. The aircraft landed at Charlottetown at 1615. After a brief stop, the flight continued to Sango Bay. The pilot broadcast his intention to take off on Runway 10, taxied the aircraft to the threshold of the runway, and commenced the take-off roll. Part-way down the runway, the pilot aborted the take-off. He then broadcast his intention to take off on Runway 28. Both radio broadcasts were acknowledged by a local pilot who was approaching the airport to land. Upon reaching the threshold of Runway 28, the aircraft turned and accelerated, without stopping, on the take-off roll. The aircraft lifted off shortly before the runway end and remained near treetop height until disappearing from view. After lift-off, the stall warning horn sounded intermittently until impact. The aircraft was unable to climb above the hilly terrain and struck the road 1.5 nautical miles from the departure end of the runway. A passing motorist spotted the downed aircraft and notified firefighters and medical personnel who were then dispatched to the scene. The accident occurred at about 1621 during daylight hours, at 58°45' N, 55°66' W, at 440 feet above sea level.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The aircraft was over the maximum allowable take-off weight throughout its journey, reducing aircraft performance: the pilot apparently did not complete weight and balance calculations for
either of the flights.
2. The pilot did not use the proper short field take-off technique, and the aircraft was forced into the air before reaching sufficient flying speed.
3 The best angle of climb speed was not attained.
4. The unsecured cargo, some of which was found on top of the back of the rear passenger seat, most probably contributed to the severity of the injuries to the passenger in this seat.
Final Report:

Crash of a Yakovlev Yak-40 near Sari: 30 killed

Date & Time: May 17, 2001 at 0745 LT
Type of aircraft:
Operator:
Registration:
EP-TQP
Survivors:
No
Site:
Schedule:
Tehran - Gorgan
MSN:
9 74 08 56
YOM:
1977
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
30
Aircraft flight hours:
11156
Aircraft flight cycles:
6706
Circumstances:
The three engine aircraft departed Tehran-Mehrabad Airport at 0645LT on a charter flight to Gorgan, carrying members of the parliament and government who were flying to Gorgan to inaugurate the new airport. En route, the crew was informed by ATC about the deterioration of the weather conditions at destination and was instructed to divert to Sari Airport. While descending to Sari in marginal weather conditions, the crew failed to realize his altitude was too low when the aircraft struck the slope of a mountain located about 20 km south of the airport. The aircraft disintegrated on impact and all 30 occupants were killed. Among the passengers were Rahman Dadman, Iranian Minister of Transport and two vice-ministers.
Probable cause:
Controlled flight into terrain while descending in stormy weather below the MDA.

Crash of a BAe 125-600B in Lagos

Date & Time: May 15, 2001
Type of aircraft:
Operator:
Registration:
5N-RNO
Survivors:
Yes
Schedule:
Yola – Lagos
MSN:
256054
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Lagos-Murtala Muhammed Airport, both engines failed simultaneously due to fuel exhaustion. The aircraft lost height, collided with approach lights and crashed short of runway threshold. All four occupants escaped with minor injuries while the aircraft was damaged beyond repair. The exact date of the mishap remains unknown, somewhere in May 2001.
Probable cause:
Double engine failure on final approach due to fuel exhaustion. Poor flight preparation.

Crash of a Cessna 208B Grand Caravan near Roque Pérez: 10 killed

Date & Time: Apr 28, 2001 at 0517 LT
Type of aircraft:
Registration:
LV-WSC
Flight Phase:
Survivors:
No
Schedule:
San Fernando – Trelew
MSN:
208B-0580
YOM:
1996
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
4700
Captain / Total hours on type:
605.00
Aircraft flight hours:
1467
Circumstances:
Owned by the Argentinian company Les Grands Jorasses, the single engine airplane was completing a charter flight from San Fernando to Trelew, carrying eight passengers and two pilots, among them the President of the Techint Group and the managing editor of the La Nación newspaper. After departure from San Fernando Airport, the crew was cleared to climb to 6,000 feet then 8,000 feet and later 10,000 feet. Because he encountered icing conditions, the crew asked ATC to climb to 12,000 feet and was cleared to proceed when control was lost. The aircraft entered a dive and crashed in a farmland. The aircraft was totally destroyed by impact forces and all 10 occupants were killed.
Probable cause:
Impact with the ground following a spiral fall due to a stall probably consecutive to an asymmetric accumulation of ice on the fuselage.
Final Report:

Crash of a Cessna 208B Grand Caravan in Tembo

Date & Time: Apr 14, 2001
Type of aircraft:
Operator:
Registration:
ZS-OCZ
Flight Phase:
Survivors:
Yes
MSN:
208B-0617
YOM:
1997
Location:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Tembo Airstrip, while in initial climb, the pilot encountered problems to gain sufficient height as the engine lost power. He attempted an emergency landing when the aircraft crash landed in an open field located about one km from the airfield, bursting into flames. All nine occupants escaped uninjured while the aircraft was destroyed by fire.

Crash of a Rockwell Shrike Commander 500S on Thornton Peak: 4 killed

Date & Time: Apr 10, 2001 at 0725 LT
Operator:
Registration:
VH-UJB
Flight Phase:
Survivors:
No
Site:
Schedule:
Cairns - Hicks Island
MSN:
500-3152
YOM:
1973
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
9680
Captain / Total hours on type:
2402.00
Circumstances:
The aircraft departed Cairns airport at 0707 Eastern Standard Time (EST) on a charter flight to Hicks Island. The aircraft was being operated under the Instrument Flight Rules (IFR) and the expected flight time was 2 hours. Shortly after takeoff the pilot requested an amended altitude of 4,000 ft. He indicated that he was able to continue flight with visual reference to the ground or water. Air Traffic Services (ATS) issued the amended altitude as requested. The IFR Lowest Safe Altitude for the initial route sector to be flown was 6,000 ft Above Mean Sea Level (AMSL). Data recorded by ATS indicated that approximately 13 minutes after departure, the aircraft disappeared from radar at a position 46NM north of Cairns. At the last known radar position the aircraft was cruising at a ground speed of 180 kts and at an altitude of 4,000 ft AMSL. An extensive search located the wreckage the following afternoon at a location consistent with the last known radar position, on the north-western side of Thornton Peak at an altitude of approximately 4,000 ft (1219 metres) AMSL. The aircraft was destroyed by impact forces and post-impact fire. The pilot and three passengers received fatal injuries. Thornton Peak is the third highest mountain in Queensland and is marked on topographic maps as 4,507 ft (1,374 metres) in elevation. Local residents reported that the mountain was covered by cloud and swept by strong winds for most of the year. The aircraft had been observed by witnesses approximately two minutes prior to impact cruising at high speed, on a constant north-westerly heading, in a wings level attitude and with flaps and landing gear retracted. They stated that the engines appeared to sound normal.
Probable cause:
Radar data recorded by Air Traffic Services and witness reports indicated that the aircraft was flying straight and level and maintaining a constant airspeed. Therefore, it is unlikely that the aircraft was experiencing any instrumentation or engine problems. Why the pilot continued flight into marginal weather conditions at an altitude that was insufficient to ensure terrain clearance, could not be established. The aircraft was flown at an altitude that was insufficient to ensure terrain clearance.
Final Report:

Crash of a Beechcraft A100 King Air in Grande Prairie

Date & Time: Apr 7, 2001 at 0512 LT
Type of aircraft:
Operator:
Registration:
C-FWPN
Survivors:
Yes
Schedule:
Fort Saint John – Grande Prairie
MSN:
B-51
YOM:
1970
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Fort Saint John, the crew started a night approach to Grande Prairie Airport. The aircraft landed slightly to the left of the runway centerline. After touchdown on a snow covered runway (about two inches of snow), the left wing struck a windrow of snow. Out of control, the aircraft veered off runway and came to rest in snow. All five occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Beechcraft 200 Super King Air in Las Majaguas

Date & Time: Apr 5, 2001 at 0815 LT
Registration:
YV-O-SATA-6
Flight Phase:
Survivors:
Yes
Schedule:
La Carlota – Barinas
MSN:
BB-5
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While in cruising altitude on a flight from La Carlota to Barinas, the crew declared an emergency following a loss of power on both engines. The crew attempted an emergency landing in a prairie when the aircraft crash landed and came to rest, broken in two. All eight occupants were rescued, among them a pilot was injured.
Probable cause:
Loss of power on both engines for unknown reasons.