ASN Wikibase Occurrence # 357735
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Friday 23 February 1996 |
Time: | 17:10 LT |
Type: | Beechcraft F35 |
Owner/operator: | Private |
Registration: | N3850B |
MSN: | 4120 |
Total airframe hrs: | 3807 hours |
Engine model: | Continental E-225-8 |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Mt. Sterling, KY -
United States of America
|
Phase: | Initial climb |
Nature: | Executive |
Departure airport: | (KIOB) |
Destination airport: | Dayton, OH (KMGY) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot stated that during the preflight inspection, engine run up, takeoff ground roll, and initial climb out, he noted no evidence of an engine anomaly. As the airplane climbed through about 500 feet agl, the pilot turned the fuel boost pump off and adjusted the power settings to climb power, then he suddenly heard a loud clattering noise and felt a severe vibration. The pilot added power in an attempt to 'limp' back to the departure runway (runway 21,) but when he pushed the throttles forward, the engine noise and vibration got worse, then the engine lost power completely. He stated that he felt his only option was to land in the opposite direction on the runway (runway 3,) so he lowered the landing gear and executed a steep 'S' turn to align with the runway. The pilot stated that the airplane touched down on the last 1000 feet of runway, and he '...stood on the brakes...' but was unable to stop the airplane before the end of the runway. The airplane ran off the departure end of the runway, through a barbed wire fence and down an embankment, coming to a stop against scrub trees. The winds were reported from 220 degrees magnetic at 13 knots gusting to 20 knots. Postaccident examination revealed that the piston in the number one cylinder had failed.
Probable Cause: a loss of engine power due to the failure of the number one piston. Related factors were the unsuitable terrain available for the forced landing, and the strong tailwind encountered during the forced landing.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | IAD96LA047 |
Status: | Investigation completed |
Duration: | 12 months |
Download report: | Final report |
|
Sources:
NTSB IAD96LA047
Location
Revision history:
Date/time | Contributor | Updates |
14-Mar-2024 06:06 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation