- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- 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.
On this page
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.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1977 | 4 |
| 1979 | 4 |
| 1980 | 6 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 2 |
| 1988 | 1 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 7 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2024 | 3 |
| 2026 | 1 |
Airframe · Piper PA-28-181
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation 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 SDR 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.SDR 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 ASDR 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 REMOVESDR 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 EX
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.
Airframe · Piper PA-28-181
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller