CEN25LA357

NTSB accident investigation · Piper PA-24-250 · Gregory, MI · August 28, 2025

Accident · Serious injuriesClass 3 · LimitedPreliminary report
Date
August 28, 2025, 15:50 local (19:50 UTC)
Place
Gregory, MI
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N7412PPiper PA-24-250
Defining event
Enroute: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Investigation ongoing
Investigation class
Class 3
NTSB office
Central Region
Parties
FAA - East Michigan FSDO
FAA report
20250828018339A
Case key
200924

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Preliminary report

What NTSB knew early in the investigation. It may change in the final report.

On August 28, 2025, at about 1550 eastern daylight time, a Piper PA-24-250 airplane, N7412P, was substantially damaged when it was involved in an accident near Gregory, Michigan. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. The pilot reported that he and the airplane owner flew the airplane from the Toledo Suburban Airport (DUH), Lambertville, Michigan, to the Charlevoix Municipal Airport (CVX), Charlevoix, Michigan, where he dropped off the airplane owner. He then re-boarded the airplane to return to DUH alone. He reported that the flight from DUH to CVX was uneventful, as was the flight from CVX toward DUH, until about 1:20 into the flight. At this time the engine suddenly stopped producing power. The pilot was in communication with air traffic control (ATC) and reported the power loss. The controller provided the pilot with options for nearby airports and the pilot elected to attempt a landing at the Richmond Field Airport (69G), near Gregory, Michigan. The airplane came to rest in a field just south of 69G and a post-impact fire ensued which consumed the cabin portion of the airplane. Postaccident examination of the engine revealed extensive fire damage. Initially the engine could not be rotated; however, after removal of the fire damaged accessories and accessory housing on the back of the engine, the remainder of the engine was free to rotate. Thumb compression was verified on all cylinder and valve continuity was verified. All of the accessory case gears were intact. The engine still had an unknown amount of oil that drained out of the broken crankcase during the examination. Examination of the accessory case components revealed that the vacuum pump drive shaft, the tachometer drive shaft, and the oil pump drive shaft were seized in their bores. Disassembly of the accessory case components did not reveal any anomalies and the seizures were consistent with the fire damage. The rear mounted magnetos were extensively damaged by the postimpact fire and were unable to be tested.

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Aircraft

Registration
N7412P
Reported as
Piper PA-24-250
Category
Airplane
Serial number
24-2600
Built
1961
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Espyess Aviation LLC
Registered owner
Espyess Aviation LLC
Departed
CVX · Charlevoix, MI
Destination
DUH · Lamberville, MI
Airport
69G · Richmond Fld

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 7 knots
Visibility
10 statute miles
Lowest ceiling
3,600 ft broken
Temperature
72 °F, dew point 57 °F
Altimeter
30.01 inHg
Observed at
KOZW, 12 nm away
METAR
METAR KOZW 281955Z AUTO 30007KT 10SM SCT029 BKN036 OVC048 22/14 A3001 RMK AO2=

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.