Crash of a Casa 212 Aviocar 400 off Progreso

Date & Time: Nov 15, 2006
Type of aircraft:
Operator:
Registration:
AMP-114
Flight Phase:
Survivors:
Yes
Schedule:
Cancún - Cancún
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew departed Cancún Airport for a routine maritime patrol flight over the Gulf of Mexico. After 5 hours of flight, while returning to his base and approaching the coast, the crew informed ATC that an engine failed. Few seconds later, the second engine stopped as well. The crew reduced his altitude and ditched the aircraft 3,5 km off Progreso, some 40 km north of Mérida. All 7 occupants were rescued while the aircraft was lost.
Probable cause:
Double engine failure for unknown reasons. Fuel exhaustion suspected.

Crash of a Learjet 35A in Nakhon Sawan: 7 killed

Date & Time: Nov 8, 2006 at 0950 LT
Type of aircraft:
Operator:
Registration:
40208
Flight Phase:
Survivors:
No
Schedule:
Nakhon Sawan – Khon Kaen
MSN:
35-635
YOM:
1987
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
Shortly after takeoff from Nakhon Sawan-Takhli AFB, while climbing to a height of about 150 feet, the pilot contacted ATC and declared an emergency following a loss of engine power. He elected to return for an emergency landing when the aircraft went out of control and crashed onto a hangar located near the airport, bursting into flames. All seven occupants were killed, among them two photographers and one mechanic who were taking part to a reconnaissance mission in view to prepare an incoming air race in Thailand.

Crash of a Casa 212 Aviocar 200 off Falsterbo: 4 killed

Date & Time: Oct 26, 2006 at 1326 LT
Type of aircraft:
Operator:
Registration:
SE-IVF/585
Survivors:
No
Schedule:
Ronneby – Malmö
MSN:
346
YOM:
1985
Flight number:
KBV585
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4424
Captain / Total hours on type:
4192.00
Copilot / Total flying hours:
638
Copilot / Total hours on type:
421
Aircraft flight hours:
17048
Aircraft flight cycles:
7389
Circumstances:
Kustbevakningen (The Swedish Coastguard), henceforth called KBV, intended on that particular day to perform two routine maritime surveillance tasks with flights over the southern Baltic Sea and along the south and west coasts of Sweden, including a flight over the Kattegatt. The flights would be carried out by the aircraft registered SE-IVF, with call sign 585. The crew consisted of two pilots and two system operators. The first flight of the day would take off from Ronneby, with Malmö/Sturup as the landing airport. According to the submitted flight plan the flight from Ronneby would depart north-east outwards across the southern tip of Öland, via reporting point KOLJA and onwards to a point south of Gotland. Thereafter the route would be via KOLJA back on a south-west course to a point south of Smygehamn in the southern Baltic Sea and then directly to Malmö/Sturup airport.

The take off from Ronneby
When KBV 585 taxied out for take off, route clearance had been obtained for take off in accordance with the submitted flight plan. The flight would be undertaken in VFR (Visual Flight Rules) weather conditions. The flight plan did not state the desired altitude, so at the initiative of air traffic control KBV 585 was assigned the altitude band “1500 feet or lower” in connection with the flight clearance. Take off was at 11:09 on runway 19. Immediately after take off the crew requested a “360”, i.e. to make a complete turn from their current position. This request was accepted by air traffic control and KBV 585 performed a circuit at about 500 feet in a left turn around the airfield. No comments or explanations were offered by the crew during this manoeuvre. In an interview with SHK the air traffic controller stated that he thought that the aircraft had suffered a technical fault and/or the crew wanted to carry out some form of check. It later transpired that the reason for the extra circuit may have been to show off the aircraft to a practical work experience student who was at the KBV as part of work experience training. After the completed left hand circuit the pilots returned to their original flight plan and continued, with an initial climb to the south, to then turn left and follow the planned flight route.

The first phase of the flight
During the continuing climb the pilots received an instruction to change radio frequency from Ronneby air traffic control tower to Ronneby control, i.e. the air traffic control section covering the Ronneby terminal area, that normally includes radar surveillance. As KBV 585 continued to climb, the air traffic controller noted that it continued to climb above the maximum altitude of 1500 feet that the stated flight clearance had included. At about 2000 feet while still climbing the pilots requested permission to climb to and maintain 2500 feet, which was granted. When the aircraft left the Ronneby terminal area the pilots changed radio frequency without reporting this to the air traffic control area controller. The air traffic controller on duty on that particular day at Ronneby stated that this was unusual behaviour by the KBV pilot, both to climb through the cleared altitude and to depart from the radio frequency without reporting it. The flight continued to the north-west in accordance with the flight plan. Apart from the routine tasking order concerning environmental and fishing surveillance, the tasking included instructions to search for traces from a previously sunken barge. The flight was performed without any problems being reported. During the flight the pilots were in radio contact both with air traffic controllers and the KBV coordination centre. As the aircraft was en route south-west after having turned at the southern tip of Gotland, the crew received a message from the coordination centre concerning a request they had received to perform a fly-by over Falsterbo. KBV has a base at the Falsterbo canal, which on that particular day was hosting a study visit by two school classes. Therefore a request came from the base to ask whether the pilots could consider performing a fly-by as they were on their way to Malmö/Sturup, so as to demonstrate the aircraft. The pilots accepted this and revised the final part of their flight plan so that a demonstration of the aircraft over the Falsterbo canal could be performed.

The fly-by over the KBV base
At 13:23 KBV 585 came in over the coast at Falsterbonäset on a north-northwesterly course along the canal. The aircraft then continued out over the sea and after a left turn returned to approach the base. The aircraft then performed another fly-by at low speed over the base and along the canal in the opposite direction, i.e. south-south-east, at low altitude. The route of the flight was partly over the canal, partly over the strip of beach and the buildings along the north-eastern shore. Beyond the far end of the canal the aircraft performed a 180 degrees left turn, first climbing and then descending. On its last approach to the base the aircraft came over the beach at the northeastern side of the canal, on a north-westerly course, which was later altered to north-north-westerly as it once again came over the canal.

The accident
As the aircraft neared the base once more it began wing tipping. After two or three wing tippings, by which time the aircraft was approximately above the bridge at the north-west entrance to the canal, a loud bang was heard and the entire left wing separated from the aircraft, to fall into the basin. The aircraft then rolled over onto its back and also fell into the basin, somewhat further out. The impact created a huge cascade of water. The remains of the aircraft and wing then quickly sank to the bottom. The whole sequence of events took place quickly and afterwards various pieces of wreckage could be seen floating on the surface at the point of impact. All on board were fatally injured. The accident took place at position 55° 25' N 012° 56' E; at sea level.
Probable cause:
The accident was caused by an inadequate maintenance system in respect of inspections for fatigue cracks. Contributory to the crack formation has been an unsuitable design of the attachment of the wings to the aircraft fuselage.
Final Report:

Crash of a PZL-Mielec AN-2TP in Zielona Góra

Date & Time: Sep 2, 2005
Type of aircraft:
Operator:
Registration:
SP-ANA
Flight Phase:
Survivors:
Yes
Schedule:
Zielona Góra - Zielona Góra
MSN:
1G29-21
YOM:
1963
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The single engine aircraft was engaged in a local survey flight (forest fire) in the region of Zielona Góra. Shortly after takeoff, while in initial climb, the engine failed. The aircraft stalled and crashed in a wooded area. All three occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
Engine failure for unknown reasons.

Crash of a Casa 212 Aviocar 100 off Sarmi: 15 killed

Date & Time: Feb 22, 2005 at 0715 LT
Type of aircraft:
Operator:
Registration:
P-2032
Survivors:
Yes
Schedule:
Jayapura - Sarmi
MSN:
220/60N
YOM:
1985
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
15
Circumstances:
On final approach to Sarmi Airport, the crew reported engine problems when the aircraft lost height and crashed in the sea about 400 metres from the runway threshold. The wreckage was found 100 metres offshore. Three passengers were rescued while 15 other occupants were killed.

Crash of a Pilatus PC-6/B2-H2 Turbo Porter in Las Lomitas

Date & Time: Sep 6, 2003
Operator:
Registration:
GN-809
Flight Phase:
Schedule:
Las Lomitas - Las Lomitas
MSN:
807
YOM:
1980
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances in Las Lomitas. Occupant fate unknown.

Crash of a Cessna 404 Titan II in Jandakot: 2 killed

Date & Time: Aug 11, 2003 at 1537 LT
Type of aircraft:
Operator:
Registration:
VH-ANV
Flight Phase:
Survivors:
Yes
Schedule:
Jandakot - Jandakot
MSN:
404-0820
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
16722
Captain / Total hours on type:
12345.00
Aircraft flight hours:
16819
Circumstances:
The aircraft took off from runway 24 right (24R) at Jandakot Airport, WA. One pilot and five passengers were on board the aircraft. The flight was being conducted in the aerial work category, under the instrument flight rules. Shortly after the aircraft became airborne, while still over the runway, the pilot recognized symptoms that he associated with a failure of the right engine and elected to continue the takeoff. The pilot retracted the landing gear, selected the wing flaps to the up position and feathered the propeller of the right engine. The pilot later reported that he was concerned about clearing a residential area and obstructions along the flight path ahead, including high-voltage powerlines crossing the aircraft’s flight path 2,400 m beyond the runway. The aircraft was approximately 450 m beyond the upwind threshold of runway 24R when the pilot initiated a series of left turns. Analysis of radar records indicated that during the turns, the airspeed of the aircraft reduced significantly below the airspeed required for optimum single-engine performance. The pilot transmitted to the aerodrome controller that he was returning for a landing and indicated an intention to land on runway 30. However, the airspeed decayed during the subsequent manoeuvring such that he was unable to safely complete the approach to that runway. The pilot was unable to maintain altitude and the aircraft descended into an area of scrub-type terrain, moderately populated with trees. During the impact sequence at about 1537, the outboard portion of the left wing collided with a tree trunk and was sheared off. A significant quantity of fuel was spilled from the wing’s fuel tank and ignited. An intense postimpact fire broke out in the vicinity of the wreckage and destroyed the aircraft. Four passengers and the pilot vacated the aircraft, but sustained serious burns in the process. One of those passengers died from those injuries 85 days after the accident. A fifth passenger did not survive the post-impact fire.
Probable cause:
Significant factors:
1. The material specification contained in the engineering order for replacing the pump bushing of the engine driven fuel pump (EDFP) fitted to the right engine was not appropriate.
2. High torsional loads between the EDFP’s spindle shaft and the sleeve bearing sheared the pump’s drive shaft during a critical phase of flight.
3. The reduction in fuel pressure was insufficient to sustain operation of the engine at the take-off power setting.
4. The loss of engine power occurred close to the decision speed with the landing gear extended while the aircraft was over the runway.
5. The pilot elected to continue the takeoff.
6. The aircraft was manoeuvred, including turns and banks, at low altitude resulting in a decrease in airspeed below that required to maximise one-engine inoperative performance.
7. The pilot was unable to maintain the aircraft’s altitude over terrain that was unsuitable for an emergency landing.
Final Report:

Crash of a Basler BT-67 in Ocaña

Date & Time: Apr 30, 2003
Type of aircraft:
Operator:
Registration:
PNC-212
Survivors:
Yes
MSN:
13110
YOM:
1944
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Ocaña-Aguas Claras Airstrip, the aircraft was unable to stop within the remaining distance. It overran and came to rest in a ditch. There were no casualties.

Crash of a Rockwell Shrike Commander 500S in Mount Pleasant

Date & Time: Apr 14, 2003 at 1140 LT
Operator:
Registration:
N19WL
Flight Phase:
Survivors:
Yes
Schedule:
Mount Pleasant - Mount Pleasant
MSN:
500-3160
YOM:
1973
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4578
Captain / Total hours on type:
280.00
Aircraft flight hours:
11617
Circumstances:
According to the pilot, he requested the refueler to top off his fuel tanks with "100 low lead fuel". After refueling, the pilot performed a preflight including taking fuel samples from under the wings, draining the rear fuel drain, and checking the fuel cap for security. The engine start, run-up, and taxi were uneventful. The airplane departed runway 17 and was in a positive rate of climb. At approximately 200 feet AGL the airplane began to lose power. Shortly after the pilot ensured that the throttle, propeller, and mixture controls were in the full forward position, the airplane lost power in both engines. The pilot executed an emergency off field landing. Examination of the wreckage revealed that the left wing had broken off and the aft cabin area was crushed. According to the refueler, he stated that he mistakenly used the Jet-A fuel truck instead of the AVGAS 100 low lead truck, and pumped 58 gallons of Jet-A into the airplane. Examination of the fuel samples taken from both engines revealed the left and right engine contained 70 percent of jet A fuel.
Probable cause:
The improper refueling of the airplane by airport personnel with the incorrect fuel grade that resulted in a total loss in engine power on both engines during initial climb. A factor was the inadequate preflight inspection by the pilot in command.
Final Report:

Crash of a Cessna 208B Caravan near El Paujil: 3 killed

Date & Time: Mar 25, 2003 at 1920 LT
Type of aircraft:
Operator:
Registration:
N5512B
Flight Phase:
Survivors:
No
Site:
Schedule:
Larandia - Larandia
MSN:
208B-0299
YOM:
1992
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The single engine aircraft departed Bogotá on a flight to Larandia AFB where it was refueled. On board were one passenger and two pilots who were taking part to an anti-narcotic program on behalf of the US and Colombian Governments. The aircraft departed Larandia AFB at 1906LT on a reconnaissance flight to find three Americans who were taken hostage by FARC rebels after the crash of a first Cessna 208 operated by One Leasing last February 13. About 14 minutes into the flight, while cruising by night at an altitude of 4,500 feet in limited visibility, the aircraft struck a tree and crashed, bursting into flames. The wreckage was found on the slope of Mt La Sonora and all three occupants were killed.