ASN Wikibase Occurrence # 133939
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 3 November 1995 |
Time: | 12:30 LT |
Type: | Cessna 150F |
Owner/operator: | Scott W. Taylor |
Registration: | N7089F |
MSN: | 15063689 |
Total airframe hrs: | 2558 hours |
Engine model: | Continental O-200-A |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | New Carlisle, OH -
United States of America
|
Phase: | Initial climb |
Nature: | Training |
Departure airport: | (I11) |
Destination airport: | (I11) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The flight instructor (CFI) stated that before flight, he performed the airplane preflight inspection, and he estimated the total fuel on board was 12 gallons. He and the student pilot flew in the local area for approximately 50 minutes, then returned to the airport to practice touch and go landings. During the initial climb after a touch and go landing, the airplane lost engine power. The CFI stated that the airplane was approximately 100 feet AGL when the power loss occurred, and he made a forced landing in a soft, plowed field. The airplane nosed over and came to rest inverted. An FAA Inspector stated that there was no evidence of spilled fuel, and the fuel tanks were not compromised. He drained 3 3/4 gallons of aviation fuel total from both wing tanks. The POH indicated that the airplane fuel system had a capacity of 38 gallons of fuel, of which 3 gallons were unuseable. The airplane manual also stated that '...in certain flight maneuvers, the fuel may move away from the fuel tank supply outlet...fuel flow to the engine may be interrupted....'
Probable Cause: inadequate preflight planning/preparation by the flight instructor (CFI), which resulted in a loss of engine power during initial climb, due to an inadequate supply of fuel and fuel starvation. The soft terrain encountered during the forced landing was a related factor.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | BFO96LA020 |
Status: | Investigation completed |
Duration: | 1 year and 2 months |
Download report: | Final report |
|
Sources:
NTSB BFO96LA020
Location
Revision history:
Date/time | Contributor | Updates |
21-Dec-2016 19:26 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
09-Apr-2024 11:06 |
ASN Update Bot |
Updated [Time, Operator, Other fatalities, Phase, Departure airport, Destination airport, Source, Narrative, Category, Accident report] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation