Registered owner
Bas Part Sales LLC
Location
Greeley, CO
Owner type
LLC
Serial number
2843474
Year built
2001
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
July 20, 2001
Mode S code
A50F78

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 60

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1963In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19631
19641
19661
19671
19692
19774
19793
19804
19821
19862
19893
19911
19921
19951
19964
19971
19982
19991
20001
20011
20042
20052
20065
20071
20083
20091
20103
20122
20131
20151
20161
20172
20182
20212
20221
20243
20261
See all 69 ADs

Information bulletins that may apply · 22

Advisory, not mandatory.

See all 24 bulletins

NTSB investigations · 1

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

FAA incident reports · 4

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 11

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

SDR FQAR20180326026Skin · crackedDURING A SCHEDULED INSPECTION, FOUND THE INBOARD LOWER WING SKIN CRACKED, CRACK WAS LOCATED 4INCHES OUTBOARD OF THE BUTT RIB AND RUNNING PARALELL TO THE SPAR, 2INCHES FORWARD OF THE SPARMar 27, 2018 · N425PA · Piper PA28181 · Wing, Plate/SkinSDR FQAR20171011092Frame · crackedDURING ROUTINE MAINTENANCE, A FUSELAGE FRAME THAT ACTS AS THE FORWARD WING ATTACH STRUCTURE WAS FOUND TO BE CRACKED AT THE UPPER RIGHT END.Oct 11, 2017 · N425PA · Piper PA28181 · Fuselage, Wing Attach FittingsSDR FQAR20170824082Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE INSTALLED AGAINST THE LEFT WING OURBOARD FLAP SUPPORT WAS FOUND CRACKED. CRACKING EXTENDED THROUGH RIVET HOLES TO MATERIAL EDGE.Aug 24, 2017 · N425PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20170626059Stiffener · crackedDURING ROUTINE INSPECTION A STIFFENER ON THE LEFT WING UPPER AFT SKIN NEAR ROOT WAS FOUND CRACKED THROUGH INBOARD MOST RIVET HOLE.Jun 26, 2017 · N425PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20161027044Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO 2" CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. THESE CRACKS CAN ONLY BE SEEN WHEN THE ELT TRAY IS REMOVED.Oct 27, 2016 · N425PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20160908031Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE RIGHT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.Sep 8, 2016 · N425PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20150825092Throttle Cable · separatedDURING ROUTINE INSPECTION, THE THROTTLE CABLE WAS FOUND PULLED APART. THE SEPARATION WAS AT THE SWAGE ON THE CARBURETOR END. HAD THE DEFECT GONE UNCORRECTED, IT WOULD HAVE LED TO A LOSS OF THROTTLE CONTROL. THIS CABLE HAD BEEN IN SERVICE 1 YEAR. MAYBE THE CAug 25, 2015 · N425PA · Piper PA28181 · Power LeverSDR FQAR20150822090Oil Cooler · leakingWHEN A MECHANIC PULLED THE TOP COWLING TO PERFORM ROUTINE MAINTENANCE, HE NOTED OIL WAS ALL OVER THE FIREWALL AND ACCESSORY CASE. INSPECTION REVEALED THE OIL COOLER WAS LEAKING FROM BETWEEN THE PLEATS. THE EXACT QUANTITY OF OIL LOST IS UNKNOWN.Aug 22, 2015 · N425PA · Piper PA28181 · Reciprocating Engine Oil SystemSDR FQAR20150526057Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 3 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-01534.May 26, 2015 · N425PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20150526056Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 1 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-01420.May 26, 2015 · N425PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20140929043Bracket · crackedDURING A PROGRESSIVE INSPECTION, A BRACKET WAS FOUND TO BE 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 TSep 29, 2014 · N425PA · Piper PA28181 · Fuselage Main, Attach Fittings

STCs that may be installed · 369

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 369 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N425PA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.