ASN Wikibase Occurrence # 201938
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: | Thursday 18 February 1999 |
Time: | 08:30 LT |
Type: | Beechcraft F33 |
Owner/operator: | Airline Training Center, Inc. |
Registration: | N8253C |
MSN: | CE-1546 |
Year of manufacture: | 1990 |
Total airframe hrs: | 9377 hours |
Engine model: | Continental IO-520 |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Prescott, AZ -
United States of America
|
Phase: | En route |
Nature: | Training |
Departure airport: | Goodyear, AZ (KGYR) |
Destination airport: | Palm Springs, CA (PSP |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot was in cruise flight at 8,500 feet mean sea level (msl) when the engine began to run rough. He verified the engine power controls were in their normal positions. Then the engine quit, and he noted the fuel pressure was reading zero. He turned on the auxiliary fuel pump and tried the restart procedure. Fuel pressure was still zero and the engine was wind milling at 1,600 rpm. He switched tanks and kept the auxiliary fuel pump on. The restart procedure was tried again, but fuel pressure remained zero. He attempted a glide to a dirt landing strip but had insufficient altitude and landed several hundred feet short in rough terrain; the nose gear collapsed when it encountered a ditch. Fuel quantity was verified on scene with the left tank full and the right tank at the bottom of the filler neck. The airframe and engine were examined following recovery and a 5-gallon fuel supply was attached to the right wing fuel system. The fuel selector valve was checked and operated normally. The boost pump was operated and the fuel pressure was observed in the normal range. The engine was primed, started, and run through the complete power range. A 50-rpm drop was observed when each magneto was checked at 1,700 rpm. Normal fuel flows were observed and leaning of the mixture was normal. No mechanical problems were encountered during the engine run and the engine shut down normally.
Probable Cause: A total loss of engine power for undetermined reasons.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | LAX99LA094 |
Status: | Investigation completed |
Duration: | 1 year and 9 months |
Download report: | Final report |
|
Sources:
NTSB LAX99LA094
Location
Revision history:
Date/time | Contributor | Updates |
26-Nov-2017 09:59 |
ASN Update Bot |
Added |
08-Apr-2024 09:32 |
ASN Update Bot |
Updated [Time, 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