Crash of a Learjet 24D in Rønne

Date & Time: Sep 15, 2012 at 1340 LT
Type of aircraft:
Operator:
Registration:
D-CMMM
Flight Type:
Survivors:
Yes
Schedule:
Strausberg - Rønne
MSN:
24-328
YOM:
1976
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The accident occurred during a private IFR flight from Strausberg Airport (EDAY), Germany, to Bornholm Airport (EKRN), Denmark. Before the flight, an ATS flight plan was filed. Before takeoff at EDAY, the aircraft was refueled with 200 liters of jet fuel. According to the ATS flight plan, the pilot stated the total endurance to be 01:30 hrs and the Estimated Elapsed Time (EET) to be 00:30 hrs. The pilot informed the AIB DK that the estimated total endurance before takeoff at EDAY was approximately 01:00 hrs. The aircraft departed EDAY at 10:58. Enroute, the pilot observed a low fuel quantity warning light. Otherwise, the flight was uneventful until the approach to EKRN. At 11:32:00 hrs and at a distance of approximately18 nm southwest of EKRN, the pilot cancelled the IFR flight plan and continued VFR for a visual approach to runway 29. While descending inbound EKRN, the airspeed was decreasing. At 11:37:08 hrs, the pilot reported to Roenne Tower that the aircraft was turning final for runway 29. The aircraft was cleared to land. The wind conditions were reported to be 280° 19 knots maximum 29 knots. The aircraft was configured for landing (the landing gear was down and the flaps extended to 40°). On a left base to runway 29, both engines suffered from fuel starvation. At 11:39:18 hrs, the pilot three times declared an emergency. The aircraft entered a stall and impacted terrain in a field of sweet corn. A search and rescue mission was immediately initiated.
Probable cause:
CONCLUSION:
Inadequate en route fuel management resulted in fuel starvation of both engines, while the aircraft was flying at low altitude and the airspeed was decreasing. The dual engine flame out and the subsequent aircraft speed control led to an unrecoverable stall and consequently caused the accident.
FINDINGS:
On board the aircraft in the pilot’s personal belongings, the AIB DK found 2 Airline Transport Pilot Licenses (ATPL) issued by the US Federal Aviation Administration (FAA). The 2 US ATPL licenses had the same FAA license number but the names of the license holders were different. The names of the license holders were inconsistent with the pilot’s Iranian identity.
The BFU informed the AIB DK that the pilot was neither in possession of a valid German pilot license nor a German validation of an US license, which was required to operate a German registered aircraft.
The NTSB informed the AIB DK that the pilot was not in possession of a valid US pilot license.
It has not been possible for the AIB DK to determine whether or not the pilot was in possession of valid pilot license issued by another state.
The BFU informed the AIB DK that the certificate of aircraft registration was cancelled in 2009. Later on in the investigation, the BFU corrected this information. On February 2nd , 2012 and due to a missing airworthiness certificate, the Luftfahrt-Bundesamt (CAA - Germany) revoked the certificate of aircraft registration.
The latest valid airworthiness certificate was issued on the 8th of March 2004 and expired on the 31st of March 2005.
At the time of the accident, the aircraft was not recorded to be maintained by a JAR 145 maintenance organization, a maintenance program or a Continuing Airworthiness Management Organization (CAMO).
Final Report:

Crash of a Cessna 402C in Rønne: 1 killed

Date & Time: Jan 17, 1991
Type of aircraft:
Operator:
Registration:
OY-SUM
Flight Type:
Survivors:
No
MSN:
402C-0505
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Crashed on approach to Rønne Airport for unknown reasons. The pilot, sole on board, was killed.

Crash of a Partenavia P.68B in Rønne

Date & Time: Apr 20, 1987
Type of aircraft:
Operator:
Registration:
SE-GFN
Survivors:
Yes
MSN:
56
YOM:
1975
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Rønne Airport, both engines failed simultaneously. The aircraft stalled and crashed in an open field located few km short of runway. All four occupants escaped with minor injuries while the aircraft was damaged beyond repair.
Probable cause:
Double engine failure on approach caused by a fuel exhaustion.

Crash of a Fokker F27 Friendship 500 in Rønne

Date & Time: Dec 27, 1969 at 1555 LT
Type of aircraft:
Operator:
Registration:
OY-APB
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Rønne - Rønne
MSN:
10426
YOM:
1969
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
47
Aircraft flight cycles:
35
Circumstances:
As part of the transition training of the company pilots, Maersk Air had scheduled training flights on the Fokker F27. An instructor captain of Fokker Aircraft was on board, along with three trainee pilots. The aircraft took off from Copenhagen Airport at 15:00 hours and climbed to FL70, heading for Rønne Airport on the island of Bornholm. Two normal touch and go landings on runway 29 using the ILS were made after arrival at Rønne. The third approach and landing was to take place with a simulated engine failure on the right engine. After the second touch and go the aircraft was cleared to 2000 ft. The instructor briefed the trainee on the single engine approach that was about to be carried out while the aircraft was inbound, including the fact that after landing it was intended to take-off again immediately using both engines, but that an engine failure would be simulated again when the speed had built up to between V1 and V2. At a time when the aircraft was just about to pass over, or had just passed over the NDB, the instructor reduced the power of the right engine to a torque pressure of about 50 psi - equal to zero thrust. The trainee flew an approach and the aircraft made a normal landing. After touch down the instructor selected l6,5° flaps, re-trimmed the aircraft and asked for take-off to be made at 85 kt. The trainee applied power to both engines, released the throttles at V1 , pulled the aircraft into the air and ordered "gear up". The gear came up as the instructor cut the left engine. The trainee established a climb of 9° on the flight director but as the speed reached 97 kt., and he wished to hold V2 until 400 ft was reached, he pulled backwards slightly on the control column. The speed began to drop and at one point the instructor called out "watch your speed". However, according to the pilots, the speed dropped to 88-89 kt. and the aircraft began to roll to the left. At this time the height was about 100 ft. The trainee counteracted the left roll with the ailerons but the aircraft continued past the horizontal into a roll to the right. According to the trainee's statement this happened a couple of times during which he counteracted the rolls with large movements of the ailerons. He thinks that the speed was about 90 kt. and he stated that he was unable to control the aircraft. Neither of the pilots noticed the vertical speed indicator but at a time which the pupil estimated was when the aircraft began to lose height as he was able to see the trees or the ground at the end of the runway, the instructor took over the piloting of the aircraft by taking hold of the control column and applied full power to the left engine. However, the aircraft continued to sink in spite of the fact that the speed was still 90 kt. A shock was felt in the aircraft when it hit some bushes and the ground about 270 metres west of the end of the runway on the slope down to the sea. The instructor realized that it would not be possible to regain control of the aircraft even before the left engine had managed to develop full power. He therefore pulled both throttles back and the aircraft then crashed onto the stony beach at the edge of the water at the bottom of the slope. The aircraft broke into several sections before coming to rest in about 1,5 - 2 metres of water about 90 metres from the first point of contact.
Probable cause:
During take-off followed by a simulated engine failure the aircraft was brought into a situation which permitted only a limited climb ability, if any. In order to reduce the speed, the pupil attempted such a rate of climb that the airspeed fell below that desired, causing the aircraft to stall or at least to be in a condition approaching the stall. The reason why the stall developed into an accident was that the instructor did not identify the situation as dangerous quickly enough and initiate the action necessary.

Crash of an Airspeed AS.10 Oxford I near Rønne: 2 killed

Date & Time: Mar 19, 1953
Type of aircraft:
Operator:
Registration:
21-237
Flight Type:
Survivors:
No
Site:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While descending to Rønne Airport, the twin engine aircraft went through a patch of fog when it struck tree tops and crashed in a wooded area located about nine km northeast of the airfield. Both crew members were killed.
Crew:
Cpt N. B. Larsen,
Lt Bent Helge Stier Andersen.