Casualties unknown

Airplane Strikes Fence and Inverts After Engine Power Loss During Climb (N381AS)

Phoenix, AZ, US

On September 15, 2000, a Piper PA-28-161 (registration N381AS) operated by Dgv Holdings was involved in an aviation accident near Phoenix, AZ. Investigators recorded the probable cause as: Loss of engine power for undetermined reasons. A factor was the lack of suitable terrain available for a straight ahead landing during the takeoff initial climb. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

An airplane inverted after hitting a perimeter fence during an emergency return to the runway following a loss of engine power. Post-accident inspection found no engine discrepancies.

Incident Overview

The airplane struck the airport perimeter fence and came to rest inverted after initiating a turn back to the runway for an emergency landing due to a loss of engine power. The event occurred during the initial climb out when the engine began to sputter.

Preflight and Takeoff Procedures

No discrepancies were found during the preflight inspection or during the startup, run-up, or pretakeoff procedures. The flight proceeded normally until the engine issue arose.

Engine Power Loss and Response

During the initial climb out, the engine began to sputter. The Certified Flight Instructor (CFI), who was on board, took control of the airplane. The CFI verified that the fuel pump was on, the throttle was full forward, and the mixture was rich. Despite these actions, the engine sputtered again, and the fuel pressure gauge indicated zero.

Emergency Landing Attempt

During the turn back to the runway, the airplane lost altitude. The aircraft subsequently struck the airport perimeter fence and came to rest inverted.

Post-Crash Inspection and Engine Test

A post-crash engine inspection and run-up were conducted. No discrepancies were noted with the visual inspection of the engine. A remote fuel source was attached to the fuel line on the left wing to facilitate an engine run-up. With the electric fuel pump engaged, fuel pressure was observed on the fuel pressure gauge. No visible fuel leaks were observed on the engine.

The engine was started per the manufacturer's checklist, and a warm-up period was initiated. After the warm-up period, the throttle was advanced to full power with no discrepancies noted.

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Frequently asked questions

What happened in the 15 Sept 2000 Piper PA-28-161 accident near Phoenix, AZ?

An airplane inverted after hitting a perimeter fence during an emergency return to the runway following a loss of engine power. Post-accident inspection found no engine discrepancies.

What aircraft was involved and where did it happen?

The accident on 15 Sept 2000 involved a Piper PA-28-161, registration N381AS, operated by Dgv Holdings, at Phoenix, AZ.

What was the probable cause of the accident?

Loss of engine power for undetermined reasons. A factor was the lack of suitable terrain available for a straight ahead landing during the takeoff initial climb.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22012. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.