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NYC07LA001 · Piper PA-24-250

3 Oct 2006 · Hammonton, NJ, United States

Piper PA-24-250 · Accident: total loss of engine power (mechanical failure) on approach

From Cross Keys Airport (17N) to Hammonton Municipal Airport (N81)

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Event

NTSB case
NYC07LA001
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Piper PA-24-250

Aircraft type
Piper PA-24
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N5097P
Operator
Unknown
Onboard fatalities
Unknown
Route
From Cross Keys Airport (17N), Cross Keys, NJTo Hammonton Municipal Airport (N81), Hammonton, NJ
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Approach · VFR pattern base
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Total loss of engine power (mechanical failure)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Accessory drive assembly, drive gear › Shifted

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The airplane was on a base leg to the airport when the engine lost power, and the pilot performed a forced landing to a swampy area short of the runway. A subsequent examination of the engine revealed that within the accessory section, the idler gear assembly, which normally transferred power from the crankshaft to the left magneto and the camshaft, had been displaced. The mounting shaft had also been displaced, and the shaft hole was elongated. The upper portions of both shaft mounting plate retaining screws were missing. The lower screw appeared to be sheared, while the remnant of the upper screw exhibited mechanical damage. The crankcase surface area around the upper screw hole exhibited fretting, and the idler gear had missing and damaged gear teeth. Remnants of the shaft mounting plate retaining screws and screw lockplate were found in the bottom of the crankcase. The engine operating time was below the recommended time between overhaul (TBO). However, the manufacturer also recommended an overhaul if the TBO was not reached within the previous 12 years, and the accident engine had not been overhauled in over 30 years. The failure sequence could not be determined, and although an excessive amount of time had passed since the previous overhaul, the lack of an overhaul could not be correlated to the displacement of the idler gear assembly.

Probable cause

Displacement of the idler gear assembly, which resulted in a loss of camshaft timing, and a subsequent engine failure. Contributing to the accident was the swampy terrain condition.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record NYC07LA001
Event ID
20061213X01782
Case number
NYC07LA001
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: d3fc171772c8e8444b6ed6bd79d41445c99513717be117e1964eb255f48383fc; retrieved 2026-09-22T04:22:38.384Z.