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N6678M

Cancelled 2017

Deregistered aircraft · 1949 Stinson 108-3 · Franklin 6A4165 series

Open in FAA registry

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Cancelled: February 16, 2017
Status when cancelled: Registration expired, pending cancellation
Serial number: 108-4678
Year built: 1949
Type: Fixed wing single engine
Engine: Reciprocating
Airworthiness: Standard
Airworthiness date: July 25, 1955
Certificate issued: March 14, 1990
Last registry action: August 19, 2008
Mode S code: A8D1B6
Owners when cancelled: Lunger Eric K Damiani David M
Location: Mifflintown, PA
Owner type: Partnership

Airframe modelStinson 108-3TCDS A-767 · ADs, bulletins and aircraft registered now Engine modelFranklin 6A4165 seriesTCDS E-238 · Reciprocating

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 2

Matched to this aircraft by N6678M and the event date: up to this one’s cancellation.

NTSB IAD02LA064Accident · Minor injuriesLimited investigationFinal reportMifflintown, PAOn-ground carburetor icing.Jun 30, 2002 · Substantial damage NTSB NYC77FNC55Accident · No injuriesClosedSaco, MESep 11, 1977 · Substantial damage

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N6678M and the event date: up to this one’s cancellation.

Accident 20020630017249AWindow Rock, AZ(-23) On takeoff on runway 26 @ P34 (mifflintown airport) at approximately 100 feet altitude the engine shut down for no apparent reason. Emergency landing was attempted off the airport. Pilot avoided homes in a residential area, but flew through various…Jun 30, 2002 · No damage Accident 19770911028579AFcd/Prec Ldg From Cruise · Saco, MEOil inlet pressure line to oil cooler split causing loss of oil.Sep 11, 1977 · Substantial damage

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2002FA0000847Engine · shutdownENGINE SHUT DOWN ON CLIMB OUT AT APPROX. 80 FEET, ALTITUDE. VISUAL EXAMINATION REVEALED NO OBVIOUS REASON FOR THE FAILURE. FUEL VENTING AND QUANTITY WERE COMPROMISED BY THE CRASH IMPACT AFTER RECOVERY EFFORTS WERE COMPLETE FUEL WAS PUT IN THE RIGHT WING TANJul 15, 2002 · N6678M · Univar 1083 · Engine (Reciprocating)