- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 4496121
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 12, 2002
- Certificate issued
- July 7, 2025
- Expires
- July 31, 2032
- Mode S code
- A32806
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 N302PAMatched 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 N302PAMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR202409251214Shaft · shearedMAGNETO REMOVED AFTER 67 HRS IN SERVICE SINCE LAST 500HR INSPECTION, UPON DISSASSEMBLY FOUND THE DRIVE END OF THE ROTATING MAGNET SHAFT SHEARED INSIDE THE MAGNET BODYSDR FQAR202311271214Landing Gear · brokenLEFT MAIN GEAR DOWN LIGHT WOULD NOT COME ON, PILOT SWAPPED BULBS WITH NO CHANGE, PERFORMED EMERGENCEY GEAR EXTENSION WITH NO LIGHT, AIRCRAFT LANDED WITH NO PROBLEM, AIRCRAFT WAS MOVED INTO THE MAINT HANGAR AND PLACED ON JACKS. DURING TROUBLE SHOOTING A BROKEN SDR FQAR20161214064Rib · crackedDURING INSPECTION, CRACKS WERE NOTED IN A RT WING RIB AT RWS 50.05. THESE CRACKS WERE IN A RIB IMMEDIATELY ADJACENT TO THE ELECTRIC FUEL PUMP AND WERE SEEN AROUND THE RIVET HOLES WHERE RIB MEETS SPAR.SDR FQAR20160323013Bulkhead · crackedDURING INSPECTION, A BULKHEAD DOUBLER IN THE EMPENNAGE WAS FOUND CRACKED. THE DEFECT WAS VISIBLE BY REMOVING A FAIRING THAT JOINS THE EMPENNAGE AND VERTICAL FIN AND LOOKING UP AND AFT. THE DOUBLER HAD 4 CRACKS. THEY WERE LOCATED BESIDE THE TOP, OTBD RIVETSSDR FQAR20160214004Oil Cooler · leakingDURING PREFLIGHT INSPECTION, THE PILOTS NOTED THERE WAS OIL STREAKING FROM THE LT ENGINE COWLING BACK TO THE T/E OF THE FLAP. INSPECTION BY A MAINTENANCE TECH REVEALED THE OIL COOLER WAS LEAKING AT THE END OF THE COOLER ADJACENT TO THE INLET FITTING. FORTUNATSDR FQAR20150609078Cylinder Head · crackedBOROSCOPE INSPECTION INDICATED CRACKING IN THE LT ENGINE NR 2 CYLINDER HEAD. AFTER THE CYLINDER WAS REMOVED, CRACKS WERE OBSERVED TO THE SIDE OF THE LOWER SPARK PLUG HOLE.SDR FQAR20150512035Angle · crackedDURING A PROGRESSIVE INSPECTION, AN ANGLE IN THE RT WING WAS FOUND CRACKED BEHIND THE LANDING GEAR SIDE BRACE FITTING. THE CRACK COULD JUST BARELY BE SEEN BEHIND THE BRACE, AND WHEN THE BRACE WAS REMOVED, DYE PENETRANT INSPECTION REVEALED IT EXTENDED FROM THE
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