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N6399W

Cancelled 2015

Deregistered aircraft · 1964 Piper PA-28-140 · Lycoming 0-320 series

Open in FAA registry

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Cancelled: April 27, 2015
Status when cancelled: Registration expired, pending cancellation
Serial number: 28-20467
Year built: 1964
Type: Fixed wing single engine
Engine: Reciprocating
Airworthiness: Standard, normal, utility
Airworthiness date: November 3, 1964
Certificate issued: December 6, 2005
Last registry action: December 16, 2008
Mode S code: A862D3
Owner when cancelled: Viets Clifton W
Location: Bloomer, WI
Owner type: Individual

Airframe modelPiper PA-28-140TCDS 2A13 · ADs, bulletins and aircraft registered now Engine modelLycoming 0-320 seriesTCDS E-274 · 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 · 1

Matched to this aircraft by N6399W and the event date: up to this one’s cancellation.

NTSB SEA05LA048Accident · No injuriesLimited investigationFinal reportSuperior, MTA loss of engine power due to the pilot's inadequate planning/decision and improper fuel management, which resulted in fuel starvation. A contributing factor was the berm.Feb 9, 2005 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N6399W and the event date: up to this one’s cancellation.

Accident 20050209001359AFcd/Prec Ldg From Cruise · Superior, MT(-23) On February 9, 2005, at 1630 MST, a Piper PA-28-140, N6399W, sustained substantial damage during a forced off-field landing, 2 miles east of Superior, Montana. The certified private pilot and his passenger were not injured. Visual meteorological…Feb 9, 2005 · Substantial damage

Service difficulty reports · 2

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

SDR 2006FA0000339Spar · corrodedDURING 100 HR INSPECTION ON REAR SPAR CHANNEL, RIVET HEADS WERE POPPED ON BOTH SIDES. A COMPLETE INSPECTION REVEALED SEVERE CORROSION BETWEEN CHANNEL AND STEEL PLATES. ALSO, SEVERE CORROSION EXISTED BETWEEN REAR IB ATTACH FITTINGS TO SPAR. THE ATTACH FITTINMar 17, 2006 · N6399W · Piper PA28140 · Wing Spar SDR 2006FA0000338Spar · corrodedDURING 100 HR INSPECTION ON REAR SPAR CHANNEL, RIVET HEADS WERE POPPED ON BOTH SIDES. A COMPLETE INSPECTION REVEALED SEVERE CORROSION BETWEEN CHANNEL AND STEEL PLATES. ALSO, SEVERE CORROSION EXISTED BETWEEN REAR IB ATTACH FITTINGS TO SPAR. THE ATTACH FITTINMar 17, 2006 · N6399W · Piper PA28140 · Wing Spar