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Crash of a Cessna 340A in Orléans

Date & Time: Oct 27, 2024 at 1145 LT
Type of aircraft:
Operator:
Registration:
N38CM
Flight Type:
Survivors:
Yes
Schedule:
Biarritz - Orléans
MSN:
340A-0901
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Orléans-Loiret (Saint-Denis-de-l'Hôtel) Airport, the pilot reported problems with the left engine. Shortly later, the airplane lost height, impacted trees and crashed in a wooded area located about 2,8 km short of runway 05. All five occupants were injured.

Crash of a Cessna 340A in Orléans

Date & Time: Aug 10, 2020 at 1355 LT
Type of aircraft:
Operator:
Registration:
N413JF
Flight Type:
Survivors:
Yes
Schedule:
Perpignan – Orléans
MSN:
340A-0746
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2635
Captain / Total hours on type:
41.00
Circumstances:
Then twin engine airplane departed Perpignan-La Llabanère Airport on a private flight to Orléans, carrying one passenger and one pilot. On final approach to Orléans-Loiret Airport (ex Saint-Denis-de-l’Hôtel), the pilot encountered a loss of power on the left engine. He attempted an emergency landing when the airplane impacted trees and crash landed in a wooded area located about 3 km short of runway 23, bursting into flames. Both occupants escaped uninjured while the airplane was totally destroyed by a post crash fire.
Probable cause:
The exact cause of the loss of power on the left engine could not be determined. The pilot, concentrating on monitoring the approach parameters, did not immediately realize the left engine malfunction. He noticed that the aircraft's rate of descent was too high to follow the standard approach slope. The pilot first attempted to go around and reconfigured the aircraft to do so by retracting the landing gear and flaps. In spite of these actions, the pilot noticed that the power delivered by the aircraft's engines did not allow him to recover the plane and understood, by being aware of the action of his right foot on the rudder pedal, that the power delivered by the left engine was abnormally low. Given the low height of the plane at the time of this observation, the pilot decided to land in the country. Contributing to the high rate of descent after the occurrence of the left engine malfunction was the fact that the drags were extended at the time the engine power decreased and the fact that the left propeller probably windmilling until the landing.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Orléans

Date & Time: Mar 22, 2001 at 1835 LT
Operator:
Registration:
PH-ABD
Flight Phase:
Survivors:
Yes
Schedule:
Orléans - Paris
MSN:
31-7305048
YOM:
1973
Flight number:
TLP2B
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1110
Captain / Total hours on type:
688.00
Copilot / Total flying hours:
327
Copilot / Total hours on type:
50
Aircraft flight hours:
9820
Circumstances:
On 22 March 2001 at about 17h35, the PA-31-350 Chieftain registered PH-ABD, call sign Tulip 2B, began its takeoff from runway 23 at Orléans-Saint Denis de l’Hôtel for an IFR departure to Paris-Le Bourget. The flight was passenger charter flight TLP2B. The pilot flying, who was the co-pilot seated in the left seat, was unable to perform the rotation. He aborted the takeoff but braking failed to stop the aircraft before the end of the runway. The runway surface was wet. Marks were left by the tyres from one hundred metres before the end of the runway. The aircraft ran across grass soaked with water. The nose gear broke and the aircraft came to a stop about one hundred and eighty metres after the end of the runway. The crew had forgotten to remove the flight control locking device.
Probable cause:
The accident was caused by the crew’s failure to perform pre-flight actions and checks relating to unblocking and free movement of the flight controls and flight control surfaces. This failure was able to develop to the point of being the cause of the accident as a result of the absence of precise CRM procedures.
Final Report: