Accident Beechcraft E33-C N8112R,
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ASN Wikibase Occurrence # 377637
 
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Date:Friday 1 March 1985
Time:14:15 LT
Type:Silhouette image of generic BE33 model; specific model in this crash may look slightly different    
Beechcraft E33-C
Owner/operator:Walter Morrison
Registration: N8112R
MSN: CJ-23
Total airframe hrs:905 hours
Engine model:CONTINENTAL IO-520-B
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Richfield, UT -   United States of America
Phase: Approach
Nature:Private
Departure airport:
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE PLT STATED THAT HE WAS RETURNING TO THE ARPT AND WAS ON THE BASE LEG OF THE TRAFFIC PATTERN WHEN HE EXPERIENCED A PARTIAL LOSS OF ENG PWR. THE PLT STATED THAT WHEN HE TURNED ON THE BOOST PUMP, PWR WAS RESTORED FOR A SHORT TIME. HE CONTINUED TO STATE THAT HE COULD NOT RESTORE SUFFICIENT PWR TO MAINTAIN FLT. AN EMERGENCY LANDING WAS EXECUTED IN AN OPEN FIELD. POST CRASH EXAM OF THE ENG REVEALED NO EVIDENCE OF A MECHANICAL MALFUNCTION OR FAILURE. THE PLT HAS 2.5 HOURS OF FLT TIME IN THIS MAKE AND MODEL ACFT. THE PLT STATED THAT HE MANAGED TO GET THE ENG STARTED ON BASE LEG AFTER THE INITIAL PWR LOSS BY USING THE FUEL BOOST PUMP. HE STATED THAT AFTER THE ENG STARTED HE FLIPPED THE BOOST PUMP SWITCH OFF AND THE ENG IMMEDIATELY LOST PWR AGAIN. THE PLTS HANDBOOK (FLT MANUAL) STATES THAT THE PUMP SHOULD BE ON FOR AN AIR START & LEFT ON IF THE FUEL PUMP IS SUSPECTED OF FAILURE LOSS OF FUEL PRESSURE WITH BOOST PUMP OFF. THE PLT INDICATED THE START PROCESS WAS REPEATED SEVERAL TIMES WITH SIMILIAR RESULTS.

Probable Cause:

Accident investigation:
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Investigating agency: NTSB
Report number: DEN85LA089
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB DEN85LA089

Location

Revision history:

Date/timeContributorUpdates
30-Mar-2024 14:49 ASN Update Bot Added

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