- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 4496109
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 17, 2002
- Certificate issued
- July 7, 2025
- Expires
- July 31, 2032
- Mode S code
- A2E58B
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 N286PAMatched 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
No FAA accident or incident reports matched to N286PAMatched 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-44-180 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 FQAR20200526004Trunnion · crackedDURING A SCHEDULED INSPECTION OF THE LANDING GEAR, THE TECH SAW WHAT HE THOUGHT WAS A CRACK ON THE NOSE GEAR DRAG LINK MOUNTING LUG ON THE NOSE GEAR, HE WENT OVER THE SUSPECTED CRACK WITH A PROBE AND A 1/2 INCH LONG SECTION OF THE LUG BROKE FREE. THE SECTION SDR FQAR20171116095Rib · crackedDURING A ROUTINE INSPECTION, A NOSE RIB IN THE RIGHT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS LOCATED AT WING STA 50.05; CRACKING WAS SEEN WHERE RIB ADJOINS THE WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSSDR FQAR20170919085Exhaust Stack · crackedDURING A ROUTINE INSPECTION THE RIGHT ENGINE NR 2 EXHAUST STACK WAS FOUND CRACKED AT FLANGE AT CYLINDER HEAD. CRACK FOLLOWED WELD AND WAS APPROX 180° AROUND CIRCUMFERENCE OF STACK.SDR FQAR20170606032Skin · crackedDURING A ROUTINE INSPECTION, THE LEFT WING SKIN AROUND FUEL TANK VENT PANEL WAS FOUND CRACKED. CRACK WAS APPROX 1.5 INCHES AND EXTENDED FWD OF THE PANEL. THE PANEL AND DOUBLER WERE NOT DAMAGED. THIS AREA HAS A HISTORY OF SEMI-FREQUENT CRACKING ON THIS AIRCRAFSDR FQAR20160215006Doubler · crackedDURING AN INSPECTION, A CRACK WAS FOUND ON A BULKHEAD DOUBLER IN THE EMPENNAGE. THE DOUBLER IS PART OF THE STRUCTURE THAT ACTS AS THE FORWARD ATTACHMENT FOR THE VERTICAL TAIL FIN. THE CRACK IS BARELY VISIBLE WHEN THE FIBERGLASS L/E FAIRING IS REMOVED.
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