- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 4496110
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 20, 2002
- Certificate issued
- July 7, 2025
- Expires
- July 31, 2032
- Mode S code
- A2E942
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O-360 model are included below.
On this page
Airworthiness directives that may apply · 65
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 | 2 |
| 1979 | 5 |
| 1980 | 6 |
| 1981 | 4 |
| 1982 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 2 |
| 2000 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-44-180
AD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorAD 2015-26-08Rudder Control SystemInformation bulletins that may apply · 21
Advisory, not mandatory.
See all 30 bulletins
NTSB investigations
No NTSB investigations matched to N287PAMatched 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-44-180 aircraft
FAA incident reports · 1
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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20190618009Snap Ring · brokenDURING A SCHEDULED INSPECTION, A PIECE OF SNAP RING WAS DISCOVERED IN THE OIL DRAIN VALVE, THE OIL SUMP AND REAR CASE WERE REMOVED, THE SNAP RING THAT RETAINS THE TACH DRIVE IN THE CAM GEAR WAS FOUND TO BE MISSING, INSTALLED NEW SNAP RING AND REINSTALLED THE RSDR FQAR20171225100Bracket · crackedDURING ROUTINE INSPECTION A BRACKET IN THE NOSE COMPARTMENT WAS FOUND CRACKED. BRACKET IS LOCATED AGAINST AFT NOSE FIREWALL AT TOP OF COMPARTMENT AND JOINS UPPER NOSE STRINGER TO FIREWALL.SDR FQAR20160229008Bulkhead · crackedDURING ROUTINE MAINTENANCE, A BULKHEAD AND DOUBLER WERE FOUND CRACKED IN THE EMPENNAGE. THE CRACKS WERE VISIBLE ONLY BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN LEADING EDGE AND EMPENNAGE AND SEARCHING WITH A MIRROR AND LIGHT. THE BULKHEAD AND DOUBLER ARESDR FQAR20150603068Cylinder Head · crackedBOROSCOPE INSPECTION INDICATED CRACKING IN THE RT ENGINE NR 3 CYLINDER HEAD. AFTER THE CYLINDER WAS REMOVED, CRACKS WERE OBSERVED TO THE SIDE OF THE LOWER SPARK PLUG HOLE.SDR FQAR20150603067Cylinder 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.SDR FQAR20150218017Squat Switch · separatedAFTER TAKEOFF, THE PILOTS ATTEMPTED TO RAISE THE GEAR. THE GEAR DID NOT COME UP AND THE GEAR UNSAFE LIGHT ILLUMINATED AND THE HORN SOUNDED. THE PILOTS RECYCLED THE GEAR HANDLE WITH THE SAME RESULTS. THEY WERE ABLE TO LAND AND RETURN TO THE RAMP UNEVENTFULLY.
STCs that may be installed · 249
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-44-180
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