N297PA

Cancelled 2019

Deregistered aircraft · 2002 Piper PA-28-181 · Lycoming O-360 series

Cancelled
May 4, 2019
Status when cancelled
Sale reported, canceled
Serial number
2843506
Year built
2002
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
March 11, 2002
Last registry action
July 24, 2018
Mode S code
A310C1
Owner when cancelled
Sale Reported
Location
Rantoul, KS
Owner type
Individual

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 N297PA and the event date: up to this one’s cancellation.

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N297PA and the event date: up to this one’s cancellation.

Service difficulty reports · 10

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

SDR FQAR201802282008Fitting · corrodedDURING A CORROSION CONTROL/AGING AIRCRAFT INSPECTION, CORROSION/RUST LVL 1 WAS FOUND TO RIGHT UPPER FWD COCKPIT FITTING. FITTING IS LOCATED AT RIGHT, LOWER END OF WINDSCREEN NEAR INST PANEL. IT IS SUSPECTED THAT CORROSION WAS CAUSED BY LEAKAGE FROM IMPROPERLY Feb 28, 2018 · N297PA · Piper PA28181 · Fuselage Miscellaneous StructureSDR FQAR201802282012Door Frame · crackedDURING A ROUTINE INSPECTION, A COMPONENT THAT FORMS THE LOWER CABIN OUTBOARD DOOR FRAME WAS FOUND TO BE CRACKED. CRACKING WAS FOUND THROUGH RIVET HOLES THAT HAD LOOSE, WORKING RIVETS. IT IS SPECULATED THAT STRESS AND DAMAGE TO THIS STRUCTURE IS FROM OCCASIONALFeb 22, 2018 · N297PA · Piper PA28181 · Fuselage Main, StructureSDR FQAR201802282011Channel · crackedDURING A ROUTINE INSPECTION, A PART THAT FORMS THE FORWARD FRAME OF THE CABIN DOOR SILL WAS FOUND CRACKED. CRACKING WAS THROUGH RIVET HOLES THAT CONTAINED LOOSE, WORKING RIVETS. STRESS TO THIS AREA OF STRUCTURE IS SUSPECTED TO BE CAUSED BY THE CABIN DOOR WHICHFeb 22, 2018 · N297PA · Piper PA28181 · Fuselage Miscellaneous StructureSDR FQAR20180222010Web · crackedDURING A ROUTINE INSPECTION, CRACKS WERE FOUND IN THE CABIN STRUCTURE FORWARD OF THE MAIN DOOR. CRACKING WAS FOUND THROUGH RIVET HOLES, AND RIVETS WERE FOUND WORKING/LOOSE. THIS CRACKING IS SUSPECTED TO BE CAUSED BY FORCES IMPOSED ON CABIN DOOR, WHICH IS MOUNTFeb 22, 2018 · N297PA · Piper PA28181 · Fuselage Miscellaneous StructureSDR FQAR20180228009Pan · crackedDURING A ROUTINE INSPECTION, A COMPONENT THAT FORMS THE LOWER CABIN INBOARD DOOR FRAME WAS FOUND TO BE CRACKED. CRACK WAS FROM LIGHTENING DIRECTLY ABOVE MAIN SPAR CARRY THOUGH AND EXTENDED TO EDGE OF MATERIAL. IT IS SPECULATED THAT THIS CRACKING IS CAUSED BY TFeb 22, 2018 · N297PA · Piper PA28181 · Fuselage Main, StructureSDR FQAR20170705063Cylinder · damagedDURING A ROUTINE INSPECTION, A COMPRESSION TEST WAS PERFORMED. CYLINDER NR 1 DID NOT HOLD PRESSURE AND A LOUD HISSING WAS HEARD FROM THE VICINITY OF CYLINDER HEAD. CYLINDER WAS REMOVED AND A SMALL HOLE WAS OBSERVED IN CYLINDER HEAD BETWEEN FINS, THE HOLE WAS NJul 5, 2017 · N297PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20170425017Support Channel · crackedDURING AN INSPECTION, STRUCTURE THAT HOLDS THE PARKING BRAKE AND HANDLE WAS FOUND CRACKED. STRUCTURE IN QUESTION IS A CHANNEL THAT RUNS BETWEEN THE FIREWALL AFT FACE AND INSTRUMENT PANEL FWD FACE. CRACKING WAS SEEN IN THIS CASE ON THE AFT END OF THE CHANNEL, IApr 25, 2017 · N297PA · Piper PA28181 · Fuselage Miscellaneous StructureSDR FQAR20161220065Mount · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, DISCOVERED TWO, TWO INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET.Dec 20, 2016 · N297PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20150528064Cylinder Head · crackedBOROSCOPE INSPECTION INDICATED CRACKING IN THE RT ENGINE NR 2 CYLINDER HEAD. AFTER THE CYLINDER WAS REMOVED, CRACKS WERE OBSERVED TO THE SIDE OF THE LOWER SPARK PLUG HOLE.May 28, 2015 · N297PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20141215048Control Cable · separatedDURING A ROUTINE ENGINE INSPECTION, A TECH NOTED THE RUBBER BOOT COVERING THE SWAGE ON THE END OF THE MIXTURE CONTROL CABLE WAS BROKEN APART; HE WROTE UP THE CABLE AND BEGAN TO REMOVE IT. AS HE WAS PULLING THE CABLE OUT OF THE FIREWALL, THE SWAGE CAME OPEN ANDec 13, 2014 · N297PA · Piper PA28181 · Mixture Control

Other aircraft with N297PA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N297PA is registered now to the first aircraft listed.