20260715008599A

Accident · Substantial damage

FAA accident report · Piper PA-28-180 · Patten, ME · July 15, 2026

Date
July 15, 2026 · 14:57 local
Place
Patten, ME
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9758J
NTSB investigation
NTSBERA26LA273
Reported as
Piper PA-28-180
Reported engine
Lycoming O&VO-360 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Airline transport
Pilot’s flight hours
20,000 total3,000 in this make and model30 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

While en route from 6B0 to pqi, the pilot of Piper PA28-180, privacy data omitted, reported experiencing fuel exhaustion and attempted to divert to mlt. At 9,500 feet MSL traveling south toward mlt, the engine lost power and the pilot executed a forced landing on a logging road 6.5 miles northwest of Patten, ME. The RH wing of the aircraft struck trees and the fuselage was spun 180 degrees, coming to rest off the road. The RH wing was completely detached from the aircraft during the accident sequence and found adjacent to the fuselage. The sole occupant pilot suffered minor injuries.

As the FAA filed it

WHILE EN ROUTE FROM 6B0 TO PQI, THE PILOT OF PIPER PA28-180, ^PRIVACY DATA OMITTED^, REPORTED EXPERIENCING FUEL EXHAUSTION AND ATTEMPTED TO DIVERT TO MLT. AT 9,500 FEET MSL TRAVELING SOUTH TOWARD MLT, THE ENGINE LOST POWER AND THE PILOT EXECUTED A FORCED LANDING ON A LOGGING ROAD 6.5 MILES NORTHWEST OF PATTEN, ME. THE RH WING OF THE AIRCRAFT STRUCK TREES AND THE FUSELAGE WAS SPUN 180 DEGREES, COMING TO REST OFF THE ROAD. THE RH WING WAS COMPLETELY DETACHED FROM THE AIRCRAFT DURING THE ACCIDENT SEQUENCE AND FOUND ADJACENT TO THE FUSELAGE. THE SOLE OCCUPANT PILOT SUFFERED MINOR INJURIES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.