Accident Piper PA-23-160 Apache N4307P, Friday 23 June 2023
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Date:Friday 23 June 2023
Time:07:34 LT
Type:Silhouette image of generic PA23 model; specific model in this crash may look slightly different    
Piper PA-23-160 Apache
Owner/operator:
Registration: N4307P
MSN: 23-1808
Year of manufacture:1959
Total airframe hrs:5101 hours
Engine model:Lycoming O-320-B3B
Fatalities:Fatalities: 0 / Occupants: 1
Other fatalities:0
Aircraft damage: Substantial
Category:Accident
Location:near Ocean Springs Airport (5R2), Ocean Springs, MS -   United States of America
Phase: En route
Nature:Private
Departure airport:Ocean Springs, MS
Destination airport:Brevard, NC (3NR3)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot was planning on conducting a cross-country flight to have an annual inspection performed on the airplane. Before the departure, the pilot reported there was about 105 gallons of 100 low-lead fuel onboard. Shortly after the takeoff, the pilot reported the left engine sustained a total loss of engine power, without any prior indications. The pilot performed a forced landing and the airplane impacted an unoccupied grass athletic field on the property of a school. The airplane sustained substantial damage to both wings and the fuselage.
During the accident sequence, the left-wing main fuel cell (rubber bladder style) was breached and no fuel was observed in the cell. The left-wing auxiliary fuel cell (rubber bladder style), was cut open during the recovery to facilitate fuel removal and no recoverable fuel was found. Therefore, it is unknown how much fuel was in the left-wing fuel tanks. During the recovery of the airplane from the accident site, about 45 gallons of fuel was recovered from the right-wing fuel tanks. During the postaccident examination of the left engine, no fuel was observed in any of the fuel hoses forward of the firewall, the engine-driven fuel pump, or the carburetor. All visible damage on the left propeller was consistent with impact forces caused by impact into a soft surface, with the propeller rotating at low or no power.
The investigation identified no preimpact mechanical malfunctions or failures with the airframe, the left engine, or the left propeller that would have precluded normal operation.
Based on the available evidence, it is likely the left engine sustained a total loss of engine power due to fuel starvation for undetermined reasons.

Probable Cause: A total loss of engine power during the initial climb due to fuel starvation for undetermined reasons.

Accident investigation:
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Investigating agency: NTSB
Report number: CEN23LA262
Status: Investigation completed
Duration: 1 year and 5 months
Download report: Final report

Sources:

NTSB CEN23LA262

Location

Media:

Revision history:

Date/timeContributorUpdates
23-Jun-2023 17:15 harro Added
23-Jun-2023 17:16 harro Updated
24-Jun-2023 18:49 Dan Gryder Updated
29-Jun-2023 01:36 Captain Adam Updated
24-Nov-2024 15:08 ASN Update Bot Updated [Time, Operator, Other fatalities, Phase, Departure airport, Destination airport, Source, Embed code, Narrative, ]

Corrections or additions? ... Edit this accident description

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