Animals
Cities
Disasters
Entertainment
Food
Government
Health
Industry
Insects
Military
Nature
People
Sports
Technology
Universe
Vehicles
Explore over 500,000 Images in my personal collection
|
|
- Code Number:
- TAFV41P01_13
- Title:
- Partnair, LN-PAA, Convair CV-580
- CN: 56
Engines: 2x Allison 501-D13
Built: 1953
Total airframe hours: 36943
Cycles: 15116
wo 08/09/1989 North Sea (Skageraki) enroute FBU
Accident report:
Status: Final
Date: Friday 08/09/1989
Time: 16:38
Crew: Fatalities: 5 / Occupants: 5
Passengers: Fatalities: 50 / Occupants: 50
Total: Fatalities: 55 / Occupants: 55
Airplane damage: Destroyed
Airplane fate: Written off (damaged beyond repair)
Location: 18 kilometers (11.3 miles) North of Hirtshals [Skagerrak] Denmark
Phase: En route (ENR)
Nature: International Non Scheduled Passenger Flight
Departure airport: Oslo-Fornebu Airport (FBU/ENFB), Norway
Destination airport: Hamburg-Fuhlsbuttel Airport (HAM/EDDH), Germany
Flight number: 394
Narrative:
Convair CV-580 LN-PAA was performing a charter from Oslo-Fornebu (FBU) Norway to Hamburg (HAM) Germany. The flight was scheduled to depart at 15:00 hours. The departure was delayed by almost a full hour due to the CAA Norway and the catering company having suspended Partnair's credit. Once the financial problem was settled the crew was given permission to fly.
During the time of September 6-8, 1989 this aircraft experienced some technical problems with the left AC power system. The AC generator was replaced, but the malfunction in the system remained. On the flight to Hamburg it was decided to use the APU generator as the electrical power source for the left AC system.
LN-PAA took off at 15:59:50. The flight proceeded normally to the planned cruise level of FL 220. At 16:04 Flight 394 was cleared direct to AAL VOR/DME (Aalborg). When the airplane climbed through FL 180 at time 16:16, the crew was informed by Oslo ACC about strong westerly winds at altitude. The air traffic controller suggested a 101 heading change to the right. At 16:22 Flight 394 was informed that the radar service from Oslo ACC terminated and that the flight would enter Danish-controlled air space within 2 minutes. The flight was then instructed to contact Copenhagen ACC. The airplane reached its cruising level at time 16:23. Half a minute later the crew established contact with Copenhagen ACC and informed them that PAR 394 was maintaining FL 220, whereupon Copenhagen ACC confirmed radar contact. This was the last radio contact with the flight. The flight proceeded normally until about 16:38. Vibrations occurred in the vertical stabilizer. These vibrations developed into violent oscillations or flutter of the horizontal tail surfaces and rudder. Vital parts of the tail section then failed and the crew lost control of the airplane. Both wings failed simultaneously under negative G loads. The Convair fell into the sea.
CAUSES: "The accident was caused by loss of control due to the destruction of primary control surfaces in the tail section, which, in turn, was caused by aeroelastic oscillations initiated by abnormal clearances in the vertical stabiliser attachments to the fuselage structure. The condition of the attachments was a result of excessive wear in pins and sleeves used in this structural joint. The pins and sleeves were of an inferior quality and did not satisfy specified values for hardness and tensile strength. They had also been installed and inspected using sub-standard maintenance procedures. Undamped oscillations in the elevator contributed to the structural failure of the empenage."
Sources:
Aviation Week & Space Technology 29.03.1993 (32-33)
Flight International 31.3-6.4.93(13)
ICAO Adrep Summary 5/89 (#23) - Keywords:
- Caption Disclaimer
