Crash of a Cessna T303 Crusader off Aldeburgh

Date & Time: Sep 19, 2006 at 1328 LT
Type of aircraft:
Operator:
Registration:
D-IAFC
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Braunschweig – Oxford
MSN:
303-00244
YOM:
1983
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
24000
Captain / Total hours on type:
6000.00
Circumstances:
Whilst on a cargo flight from Braunschweig, Germany, to Oxford, England, when approximately 30 nm from the English coast, the right engine started to run roughly. On checking the fuel gauges, the pilot observed that they were indicating in the ‘red sector’. The right engine subsequently stopped, shortly followed by the left engine. The aircraft then glided from FL100 towards the Suffolk coast and ditched in the sea approximately 9.5 nm southeast of Aldeburgh. The pilot was able to abandon the aircraft, which sank quickly. He was rescued from the sea some 18 minutes later by a Royal Air Force Search and Rescue helicopter and taken to hospital, where he was found to have suffered a fractured a vertebra. The investigation determined that the aircraft had run out of fuel, due to insufficient fuel for the intended journey being on-board the aircraft at the start of the flight.
Probable cause:
The accident occurred as a result of the aircraft running out of fuel approximately 160 nm short of its destination. Although the wreckage of the aircraft was not recovered, all the evidence suggests that this occurred due to insufficient fuel being on-board the aircraft prior to departure, rather than because of a technical problem. The pilot’s lack of awareness of the fuel quantity and the actual weight of the cargo on board D-IAFC prior to takeoff, are considered to have been significant causal factors in the accident. A contributory factor was that the pilot did not monitor the reportedly ‘unreliable’ fuel gauges, thus missing a chance to notice the aircraft’s low fuel state and divert to a suitable airfield before the situation became critical.
Final Report:

Crash of a Dornier DO328-110 in Bremen

Date & Time: Dec 2, 2001 at 1833 LT
Type of aircraft:
Operator:
Registration:
D-CATS
Flight Type:
Survivors:
Yes
Schedule:
Braunschweig - Bremen
MSN:
3009
YOM:
1994
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6000
Captain / Total hours on type:
1500.00
Copilot / Total flying hours:
1900
Copilot / Total hours on type:
1000
Aircraft flight hours:
10340
Aircraft flight cycles:
9837
Circumstances:
Following an uneventful ferry flight from Braunschweig, the crew was cleared to land on runway 27 at Bremen-Neuenland Airport. After touchdown, the crew started the braking procedure and activated the reverse thrust systems on both engines. At a speed of 60 knots, the aircraft deviated to the right so the captain applied left rudder. The aircraft turn 15° to the left so the captain applied right rudder when the aircraft turned 135° to the right. This turn was so abrupt that it caused the left main gear to collapse. The aircraft rolled for about 1,150 metres before coming to rest. All three crew members evacuated uninjured while the aircraft was damaged beyond repair.
Probable cause:
The accident is due to the fact that the speed display in the cockpit became unusable during the tailwind landing in reverse thrust operation. The following contributing factors were identified:
- The crew failed to comply with published procedures as the reverse thrust systems were not deactivated when the speed of 60 knots was reached during the deceleration manoeuvre,
- The aircraft became unstable while its speed was decreasing during reverse thrust operation,
- The aircraft was oversteered,
- No references either in the AFM or in the AOM on an influence on the speed display by the reverse thrust operation in connection with tail wind up to the permissible value were given,
- In Chapter 05 of the AFM no references to a limited controllability in reverse thrust operation with tail wind was given,
- The information given in Chapter 10 of the AOM for using the thrust reverser in chapter 05 of the AFM was not included.
Final Report:

Crash of a Socata TBM-700 in Braunschweig

Date & Time: Dec 8, 1995
Type of aircraft:
Operator:
Registration:
OE-EHG
Flight Type:
Survivors:
Yes
MSN:
28
YOM:
1991
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Braunschweig-Wolfsburg Airport, the pilot failed to realize his altitude was insufficient when the single engine aircraft struck power cables and crashed in the Oker River, about 3,5 short of runway 08 threshold. All six occupants were injured and the aircraft was destroyed.

Crash of a Consolidated B-24J-140-CO Liberator in Braunschweig: 5 killed

Date & Time: May 19, 1944
Operator:
Registration:
42-110151
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
3947
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The four engine aircraft crashed in unknown circumstances near Braunschweig while on a bombing mission. Five crew members were killed while four others were taken POW.

Crash of a Consolidated B-24J-140-CO Liberator in Braunschweig: 10 killed

Date & Time: May 19, 1944
Operator:
Registration:
42-110153
Flight Phase:
Flight Type:
Survivors:
No
MSN:
3949
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
En route, the four engine aircraft was shot down by enemy fire and crashed, killing all ten crew members.
Probable cause:
Shot down by enemy action.

Crash of an Udet U12a Flamingo in Berlin: 1 killed

Date & Time: Sep 19, 1930
Type of aircraft:
Operator:
Registration:
D-1760
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Berlin – Braunschweig
MSN:
437
YOM:
1928
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew departed Berlin on a training flight to Braunschweig. Shortly after takeoff from Tempelhof Airport, while climbing to a height of 100 metres, the aircraft entered an uncontrolled descent and crashed in a field. The pilot Richard Rödel was killed and the pilot Gerhard Kurz was seriously injured.

Crash of a LVG C.VI in Dortmund

Date & Time: Jun 26, 1921 at 1000 LT
Type of aircraft:
Operator:
Registration:
D-18
Flight Phase:
Survivors:
Yes
Schedule:
Dortmund – Braunschweig
MSN:
5097
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed shortly after takeoff from Dortmund Airport. Both occupants were injured and the aircraft was destroyed.