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N429PA

Cancelled 2018
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Deregistered aircraft · 2001 Piper PA-28-181 · Lycoming O&VO-360 series

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Cancelled
September 13, 2018
Status when cancelled
Registration expired, pending cancellation
Serial number
2843487
Year built
2001
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
August 13, 2001
Certificate issued
September 25, 2007
Last registry action
January 9, 2015
Mode S code
A51E54
Owner when cancelled
Bird Acquisition LLC
Location
Wellesley Hills, MA
Owner type
Corporation
Airframe modelPiper PA-28-181TCDS 2A13 · ADs, bulletins and aircraft registered nowEngine modelLycoming O&VO-360 seriesReciprocating

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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N429PA and the event date: up to this one’s cancellation.

Incident 20130504006181ITaxi · Phoenix, AZA student pilot was taxiing to runway 7R. He attempted to taxi around another aircraft on the taxiway and inadvertently made contact with the wingtip of the of aircraft. The contact was the wingtip of the student pilot's aircraft and the wingtip of the other…May 4, 2013 · No damage

Service difficulty reports · 3

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

SDR FQAR20150210014Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND IS USED TO MOUNT THE FLAP HANDLE ASSY. IT CONTAINS 2 NUT PLATES TFeb 9, 2015 · N429PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR F8ZR871YMount · crackedMOUNTING PLATE STRESSED CRACKED. IDENTICAL TO OTHER FAILURES. CRACKS ON BOTH UNITS WERE 2 INCHES LONG. (K)Jun 6, 2005 · N429PA · Piper PA28181 · Engine StarterSDR 2003FA0000789Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON THE PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT CONTROL INPUT. PRJul 9, 2003 · N429PA · Piper PA28181 · Control Column Section