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NYC05LA144 · Piper PA-28-180

20 Sept 2005 · Millville, NJ, United States

Piper PA-28-180 · Accident: partial loss of engine power (mechanical failure) during initial climb

From Millville Municipal Airport (MIV) to Atlantic City International Airport (ACY)

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Event

NTSB case
NYC05LA144
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-28-180

Aircraft type
Piper PA-28
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
N6494J
Operator
Unknown
Onboard fatalities
Unknown
Route
From Millville Municipal Airport (MIV), Millville, NJTo Atlantic City International Airport (ACY), Atlantic City, 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
Initial climb
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
Partial loss of engine power (mechanical failure)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Stall
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

  • Pilot in command(cfi) › Airspeed, not maintained
  • Pilot in command(cfi) › In-flight planning/decision, improper

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

NTSB narrative

After takeoff from runway 28, at an altitude of 600 feet msl, the pilot initiated a right turn. During the turn, the engine began to "run rough," and the engine rpm decreased to between 1,800 - 2,000 rpm. The flight instructor told the pilot to return to the airport, and the pilot set up the airplane for a downwind landing on runway 10. When the airplane was halfway down the runway, the pilots decided to perform a go-around. They applied full power, and initiated a "slight" climbing right turn above trees at the departure end of runway 28, and then a left turn to return for landing on runway 28. During the turn, the aircraft "entered an accelerated stall," and the left main landing gear impacted the ground. The airplane continued across a grass area and struck a group of trees. Examination of the engine revealed the number 3 cylinder contained a crack from the spark plug hole to a point between the cylinder intake and exhaust valve. The most recent annual inspection was performed 2 months prior to the accident, during which no abnormalities were noted with the cylinders. At the time of the accident, the wind was from 250 degrees at 7 knots. The airport consisted of two runways; runway 10/28, which was 6,002 feet long by 150 feet wide, and runway 14/32 which was 5,057 feet long by 150 feet wide.

Probable cause

The flight instructor's improper in-flight decision to perform a emergency landing to a runway, with a tailwind, and his failure to maintain airspeed after aborting that landing, which resulted in an inadvertent stall and subsequent impact with terrain. Factors in the accident were the partial loss of engine power due to a cracked cylinder, and tailwind condition.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record NYC05LA144
Event ID
20051004X01566
Case number
NYC05LA144
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: ee52210e7655cb5db9b5c835bd3ed8fad4ebcbe2ac40c3b3dcc9fe7b9bfccdb7; retrieved 2026-09-21T09:03:09.075Z.