Crash of a Let L-410UVP-E off Djibouti City: 4 killed

Date & Time: Mar 17, 2002 at 1802 LT
Type of aircraft:
Operator:
Registration:
J2-KBC
Flight Type:
Survivors:
No
Schedule:
Mogadishu – Djibouti City
MSN:
91 25 37
YOM:
1991
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Following an uneventful flight from Mogadishu, the crew started the descent to Djibouti City-Ambouli Airport. While the runway 09 was in use, the crew was cleared for an approach to runway 27. While completing a last turn to the left to join the glide, the aircraft went out of control and crashed in the sea. All four occupants were killed.

Crash of a Beechcraft E90 King Air in Reno

Date & Time: Mar 13, 2002 at 1940 LT
Type of aircraft:
Operator:
Registration:
N948CC
Survivors:
Yes
Site:
Schedule:
Durango - Truckee
MSN:
LW-236
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1610
Captain / Total hours on type:
608.00
Aircraft flight hours:
8773
Circumstances:
During an instrument approach, upon descending to the prescribed minimum descent altitude, about 1/2 mile from the missed approach point, the pilot failed to maintain flying airspeed. The airplane stalled, rolled left, and in an uncontrolled descent collided with a commercial building 0.96 nm from the runway's displaced threshold. The accident occurred during the return portion of a round trip flight, while on final approach to the pilot's alternate airport due to a weather-induced diversion. Moderate intensity snow showers and freezing fog existed. During the initial approach, the reported visibility was 1 1/2 miles. About the time the pilot passed the final approach fix, the visibility decreased to 1/2 mile, but the pilot was not informed of the decrease below his 1-mile minimum requirement. The pilot had maintained the recommended 140-knot approach speed in the icing conditions until about 3 1/2 miles from the runway. Thereafter, the airplane's speed gradually decreased until reaching about 75 knots. After the airplane started vibrating, the pilot increased engine power, but his action was not timely enough to avert stalling. Company mechanics maintained the airplane. On previous occasions overheat conditions had occurred wherein the environmental ducting melted and heat was conducted to the adjacent pneumatic tube that provides deice air to the empennage boots. During the accident investigation, the deice tube was found completely melted closed, thus rendering all of the empennage deice boots dysfunctional.
Probable cause:
The pilot's inadequate approach airspeed for the existing adverse meteorological conditions followed by his delayed remedial action to avert stalling and subsequent loss of airplane control. Contributing factors were the pilot's reduced visibility due to the inclement weather and the icing conditions.
Final Report:

Crash of a Cessna 340A in Cairns

Date & Time: Mar 9, 2002 at 1729 LT
Type of aircraft:
Registration:
N79GW
Flight Type:
Survivors:
Yes
Schedule:
Bankstown – Cairns
MSN:
340A-0680
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot of a Cessna 340 departed Bankstown, NSW at 1223 ESuT, for Townsville, Qld via Walgett, St George, Roma, Emerald and Clermont. He reported that he climbed the aircraft to 16,000 ft and adopted a long range power setting of about 49% which equated to a true air speed (TAS) of 168 kts and a fuel burn of 141 lbs per hour. As the pilot approached the ‘OLDER’ waypoint north of Clermont, he reviewed his fuel situation and, because of a strong tailwind decided to continue on to Cairns. He informed an enroute controller of his decision and requested, for fuel planning purposes, a clearance to allow him to track in the opposite direction on a one-way air route. The controller was unable to approve his request but offered the pilot a direct track to Biboohra, a navigation aid 20 NM west of Cairns. The pilot accepted the amended track with the intention of later requesting a more direct route to Cairns. About 15 minutes later, the pilot requested a more direct track, but was told to call the approach controller for a possible clearance. He contacted the approach controller and told the controller that he had minimum fuel. The controller asked the pilot if he was declaring an emergency, to which he replied affirmative. The pilot later commented that he did this in the hope of expediting his arrival. He was instructed to descend to 6,500 ft and track direct to Cairns. The controller asked the pilot if he preferred to join the runway 15 circuit via a left downwind or right downwind, to which the pilot requested to join a left downwind. The pilot later commented that the aircraft fuel flow gauges were indicating a total flow of 140 lbs per hour and the fuel quantity gauges for the selected main tanks, although wandering somewhat, were ‘displaying a healthy amount’ considering that he was about 12 NM from his destination. As the pilot approached 6,500 ft, he requested a clearance for further descent, to which the controller instructed the pilot to descend to 4,000 ft. As the aircraft descended to 4,000 ft, the pilot saw Cairns City, but could not see the runway at Cairns airport. The aircraft's distance measuring equipment (DME) indicated 9 NM to the DME navigation aid at Cairns Airport. The pilot reported that at about this time, he observed one of the fuel flow gauges indicating zero, while at the same time, one or both engines began to surge and run roughly. He immediately informed the controller of the situation. The controller asked the pilot if he was familiar with a local airstrip (Greenhill which is 10 NM to the southeast of Cairns airport), to which the pilot replied that he wasn't. The controller indicated to the pilot that the strip was situated in his two o'clock position at a range of about two miles and to be aware of power lines and the sugar cane. The pilot was unsure of what to look for and was unable to see the strip, but after conducting a number of steep turns, saw a cleared strip in a field. He decided that he had to land. He extended the landing gear, but realised that the aircraft was too high and attempted a 360-degree steep turn onto final to reposition the aircraft. However, the airspeed was rapidly decreasing and there was insufficient height to complete the approach. At 1729 EST, the aircraft impacted the ground short of the strip and slid for about 20 metres. The pilot was seriously injured and the passengers received minor injuries.
Probable cause:
The reason for the initial fuel flow fluctuations was not identified by the pilot. It is likely that the pilot assumed the zero reading indicated impending fuel exhaustion and concentrated on conducting a landing in unfamiliar terrain. During the landing approach the pilot lost control of the aircraft and it descended rapidly to the ground.
Final Report:

Crash of a Swearingen SA227AC Metro III in Goose Bay

Date & Time: Mar 4, 2002 at 0456 LT
Type of aircraft:
Operator:
Registration:
C-FITW
Flight Type:
Survivors:
Yes
Schedule:
Saint John's - Goose Bay
MSN:
AC-638
YOM:
1986
Flight number:
PB905
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was on a scheduled courier flight from St. John=s, Newfoundland and Labrador, to Goose Bay. The aircraft touched down at 0456 Atlantic standard time and, during the landing roll on the snow-covered runway, the aircraft started to veer to the right. The captain's attempt to regain directional control by the use of full-left rudder and reverse on the engines was unsuccessful. The aircraft continued to track to the right of the centreline, departed the runway, and struck a hard-packed snow bank. There were no injuries to the two crew members. The aircraft was substantially damaged.
Probable cause:
Findings as to Cause and Contributing Factors:
1. Aircraft directional control was lost, likely because of negative castering of the nosewheel when snow piled up in front of the nosewheel assembly.
Findings as to Risk:
1. The crew members were not aware of negative castering; the aircraft flight manual and emergency checklists do not address negative castering.
2. The emergency response to the occurrence was delayed by four minutes because of the lack of communication from the aircraft to the tower.
Final Report:

Crash of a Tupolev TU-134 at Mozdok AFB

Date & Time: Mar 4, 2002
Type of aircraft:
Operator:
Flight Type:
Survivors:
Yes
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Mozdok AFB, the crew encountered bad weather conditions with heavy snow falls when the aircraft struck the ground and crashed 450 metres short of runway. There were no casualties but the aircraft was damaged beyond repair.

Crash of an Antonov AN-26 in Heglig

Date & Time: Feb 27, 2002 at 0915 LT
Type of aircraft:
Operator:
Registration:
ST-MGL
Survivors:
Yes
Schedule:
Khartoum - Heglig
MSN:
97 09
YOM:
1980
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was completing a charter flight from Khartoum to Heglig on behalf of an oil company, carrying 12 passengers and four crew members. On final approach in good weather conditions, the aircraft was too low and struck the ground short of runway 34 threshold. The aircraft bounced then landed hard, causing the undercarriage to be torn off. The aircraft slid on its belly, veered off runway and came to rest in bushes. Al 16 occupants evacuated safely while the aircraft was damaged beyond repair. Wind was gusting to 23 knots at the time of the accident.

Crash of an Ilyushin II-76MD in Mashhad

Date & Time: Feb 24, 2002
Type of aircraft:
Registration:
15-2281
Flight Type:
Survivors:
Yes
Schedule:
Mashhad - Tehran
MSN:
0073475236
YOM:
1987
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
222
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Few minutes after takeoff from Mashhad Airport, while flying at FL230 about 80 km from his departure point, the crew encountered technical problems when the autopilot system disengaged and the engine n°4 caught fire. The crew elected to extinguish the fire but without success and was cleared to return to Mashhad for an emergency landing. The fire spread to the right wing and the engine n°4 detached. Nevertheless, the crew was able to land safely at Mashhad Airport 24 minutes later and stopped the airplane on the runway. All 230 occupants escaped uninjured while the aircraft was partially destroyed after the right wing broke off and fell on the ground.
Probable cause:
Fire on engine n°4 for unknown reasons.

Crash of an Antonov AN-26 at Lakhta AFB: 17 killed

Date & Time: Feb 21, 2002 at 2045 LT
Type of aircraft:
Operator:
Registration:
07 red
Flight Type:
Survivors:
Yes
Schedule:
Safonovo - Lakhta
MSN:
ZR726001
YOM:
1975
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
Following an uneventful flight from Safonovo NAS (Severomorsk), the crew started a night descent to Lakhta AFB. Weather conditions were poor with low clouds at 120 metres, a visibility of 1,500 metres and snow squalls. On final, at a distance of 2,700 metres from the runway threshold, the aircraft was 30 metres below the glide. Once the crew reached the decision altitude, he decided to continue despite he did not establish any visual contact with the ground. At a speed of 220-240 km/h and at a height of 16 metres, the right wing collided with trees. The aircraft descended and crashed in a snow covered field located 1,725 metres short of runway and 52 metres to the left of the extended centerline. Three people, among them a pilot, survived, while 17 other occupants were killed. The aircraft was totally destroyed.
Probable cause:
The crew's decision to continue the approach after the decision height without any visual contact with the ground until the aircraft collided with trees and impacted terrain. The crew failed to follow the published procedures and to initiate a go-around manoeuvre.

Crash of a Rockwell Shrike Commander 500S in Exeter: 1 killed

Date & Time: Feb 17, 2002 at 1752 LT
Registration:
N999N
Survivors:
No
Schedule:
Wilmington - Newport
MSN:
500-3277
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
900
Captain / Total hours on type:
200.00
Aircraft flight hours:
2145
Circumstances:
The airplane was in instrument meteorological conditions and the pilot was cleared for an approach. As the airplane neared the final approach fix, the controller observed the airplane diverge from the approach course and change altitude rapidly. Shortly thereafter, the pilot said he had "all sorts of problems." The pilot requested and received vectors to an alternate airport. At 1748:29, the pilot was cleared for an ILS approach and was told to report when "established" on the approach. When asked if he was established on the ILS course, the pilot replied "I sure hope so." The controller observed the airplane descend below the published glide slope intercept altitude and advised the pilot to climb back to 2,000 feet. The pilot reported "I have problems." When asked the nature of the problem, the pilot reported "...I'm all over the place...I think I'm iced up..." Radar data indicated the airplane's radar track began following a left descending turn from 1,900 feet, about 1 minute before radar contact was lost. At 1751:33, the controller advised the pilot that his altitude was 1,000 feet, and requested that he climb to 3,000 feet. The pilot responded, "hey, I'm trying like hell." Radar contact with the airplane was lost about 1752, at 800 feet. A witness near the accident site stated he observed the airplane come out of the clouds, "wobbling" from side to side, make a "hard" left turn and strike the ground. He stated the engine was "loud" and seemed to be at "full throttle." Examination of the airplane did not reveal any pre impact mechanical malfunctions. The pilot purchased the accident airplane about 2 months prior to the accident. His total flight time in make and model was estimated to be about 200 hours. Airman's Meteorological Information (AIRMET) Zulu, Update 4, for Ice and Freezing Level was valid for the accident site area at the time of the accident. The AIRMET advised of occasional moderate rime/mixed icing in cloud in precipitation below 12,000 feet. The AIRMET reported the freezing level was from the surface to 4,000 feet. According to United States Naval Observatory astronomical data obtained for the accident site area, Sunset occurred at 1723, and the end of civil twilight was at 1751. The airplane was equipped with both wing leading edge and empennage de-icing boots. The switches for the de-icing boots were observed in the "Auto" position. The propeller de-ice and windshield anti-ice switches were observed in the "off" position.
Probable cause:
The pilot's failure to maintain control after encountering icing conditions while on approach for landing. Factors in this accident were the night light conditions and pilot's failure to select the airplane's propeller de-icing switches to the "on" position.
Final Report:

Crash of an Antonov AN-12BP in Monrovia: 1 killed

Date & Time: Feb 15, 2002 at 0608 LT
Type of aircraft:
Operator:
Registration:
ER-ADL
Flight Type:
Survivors:
Yes
Schedule:
N’Djamena – Monrovia
MSN:
4 3 426 10
YOM:
1964
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
While descending to Monrovia-Roberts Airport, the crew informed ATC about technical problems. The captain realized he could not reach the airport and attempted an emergency landing in an open field located about 11 km from the airfield. On impact, the aircraft lost its undercarriage and slid for few dozen metres before coming to rest. A crew member was killed while nine other occupants were rescued.