Registered owner
Skywest Leasing Inc
Owner type
Corporation
Serial number
2843288
Year built
1999
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
October 26, 1999
Certificate issued
July 7, 2025
Expires
July 31, 2032
Mode S code
ACD203

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.

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Airworthiness directives that may apply · 70

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: 79 ADs
19631
19641
19661
19671
19692
19774
19794
19806
19811
19821
19862
19881
19893
19911
19921
19951
19964
19971
19982
19991
20001
20011
20021
20042
20053
20067
20071
20083
20091
20103
20122
20131
20151
20161
20172
20182
20212
20222
20243
20261
See all 80 ADs

Information bulletins that may apply · 26

Advisory, not mandatory.

See all 35 bulletins

NTSB investigations

No NTSB investigations matched to N925PAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-28-181 aircraft

FAA incident reports

No FAA accident or incident reports matched to N925PAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Piper PA-28-181 aircraft

Service difficulty reports · 5

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

SDR FQAR20180602739Bracket · crackedDURING A SCHEDULED INSPECTION THE FORWARD FLAP BACKET WAS FOUND TO BE CRACKED, BRACKET IS LOCATED IN THE TUNNEL AND IS THE FORWARD MOUNTING POINT FOR THE FLAP HANDLE ASSEMBLY. SUSPECT CRACKING IS CAUSED BY CREWS IN ADVERTANTLY STEPPING ON THE FLAP HANDLE WHEN Jun 26, 2018 · N925PA · Piper PA28181 · Trailing Edge FlapsSDR FQAR20150523059Cylinder 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.May 23, 2015 · N925PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20150324023Bracket · 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 NUT PLATES TO AMar 23, 2015 · N925PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20150205011Axle · crackedDURING A ROUTINE INSPECTION, THE RT MLG APPEARED TO BE CRACKED BELOW THE STRUT BETWEEN THE TORQUE LINK ATTACH EARS. THE CRACK WAS SMALL AND COULD BE EASILY OBSCURED BY GREASE AND WAS NEARLY INVISIBLE ONCE THE TORQUE LINKS HAD BEEN DISCONNECTED AND LOAD REMOVEJan 28, 2015 · N925PA · Piper PA28181 · Main Landing Gear Strut/Axle/TruckSDR FQAR20140129017Tube · failedTHE RT MAIN TIRE WENT FLAT, THE WHEEL ASSEMBLY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSEMBLY ON 10/25/2013 AND HAD SINCE ACCRUED 177 HOURS TIME IN SERVICE. THIS REPAIR STATION HAS EXDec 10, 2013 · N925PA · Piper PA28181 · Tire Tube

STCs that may be installed · 383

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

See all 383 STCs