- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 4496031
- Year built
- 1999
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 17, 1999
- Certificate issued
- July 7, 2025
- Expires
- July 31, 2032
- Mode S code
- AD88A2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
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 | 4 |
| 1980 | 4 |
| 1981 | 3 |
| 1982 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 2 |
| 2000 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 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 · 17
Advisory, not mandatory.
See all 19 bulletins
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20170808076Rib · 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 WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSPECTSDR FQAR20170808075Rib · crackedDURING A ROUTINE INSPECTION, A NOSE RIB IN THE LEFT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS LOCATED AT WING STA 50.05; CRACKING WAS SEEN WHERE RIB ADJOINS WING SPAR, DIRECTLY NEXT TO ELECTRIC FUEL PUMP. CRACKING OCCURRED AT RIVET HOLES. IT IS SUSPECTESDR FQAR20160607024Doubler · crackedDURING A ROUTINE INSPECTION, A DOUBLER INSTALLED ON A BULKHEAD IN THE EMPENNAGE WAS FOUND TO BE CRACKED. THE CRACKED DOUBLER WAS MADE VISIBLE BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN AND AFT FUSELAGE AND LOOKING AFT AND UP WITH A MIRROR AND FLASHLIGHTSDR FQAR20150731084Exhaust Riser · fracturedDURING A PREFLIGHT RUN, WHEN THE RT ENG CARB HEAT WAS SELECTED ON, THE ENG RPM DROPPED OVER 600 RPM & THE ENG RAN ROUGH. INSPECTION REVEALED THE NR 4 CYLINDER EXHAUST RISER HAD FRACTURED ABOUT THE FLANGE & HAD FALLEN OPEN, ALLOWING EXHAUST GASSES TO BE EMITTESDR FQAR20150527062Cylinder 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. THE CYLINDER HEAD CASTING NR 160941.SDR FQAR20150527061Cylinder 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. THE CYLINDER HEAD CASTING NR 160921.SDR FQAR20150527060Cylinder Head · crackedBOROSCOPE INSPECTION INDICATED CRACKING IN THE RT ENGINE NR 1 CYLINDER HEAD. AFTER THE CYLINDER WAS REMOVED, CRACKS WERE OBSERVED TO THE SIDE OF THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR 168831.SDR FQAR20150305020Squat Switch · separatedTHE PILOTS WERE PERFORMING A PREFLIGHT INSPECTION. WHEN THE BATTERY MASTER WAS TURNED ON, THE GEAR UNSAFE LIGHT IMMEDIATELY ILLUMINATED AND THE GEAR WARNING HORN SOUNDED. BEFORE TURNING THE MASTER OFF, THEY NOTED THE GEAR SELECTOR HANDLE WAS IN THE DOWN POSITSDR FQAR20141106045Pump · seizedWHEN THE PILOTS WERE PERFORMING THEIR ENGINE START CHECKLIST PROCEDURES, THEY NOTED RT SIDE FUEL PRESSURE INDICATED 0 DESPITE RT ELECTRIC FUEL PUMP BEING SELECTED ON. PRELIMINARY INSPECTION BY A MAINTENANCE TECH CONFIRMED THE PROBLEM AND FOUND THE PUMP MOTOR SDR 2009FA0001007Downlock Switch · brokenLT MLG WIRING HARNESS WIRES ON DOWNLOCK SWITCH BROKE AT SWITCH CAUSING AN INDICATION OF UNSAFE GEAR.SDR 2009FA0001008Wire Harness · brokenLT MLG WIRING HARNESS WIRES ON DOWNLOCK SWITCH BROKE AT SWITCH CAUSING AN INDICATION OF UNSAFE GEAR.SDR 2009FA0001009Wire Harness · brokenLT MLG WIRING HARNESS WIRES ON DOWN LOCK SWITCH BROKE AT SWITCH CAUSING AN INDICATION OF UNSAFE GEAR.SDR 20000809SH010Gasket · tornGASKET TEARS AND BREAKS APART AFTER A FEW TIMES OPENING THE GAS CAP. (X)
STCs that may be installed · 235
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