- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 2843500
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- December 6, 2001
- Certificate issued
- July 7, 2025
- Expires
- July 31, 2032
- Mode S code
- A55E76
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 · 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 N445PAMatched 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 · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20170711024659ILanding: Touchdown · Phoenix, AZThe aircraft was making a normal landing on runway 25 rt. A crosswind cause the student pilot to initiate a go around. A ride along student was video taping the landing sequence. After watching the video the student took in the back of the aircraft of the…Incident 20170709013979ILanding: Touchdown · Phoenix, AZStudent pilot and instructor with an observer departed runway 25L after a bounced landing. Student applied full power after the bounce but the engine did not respond for more than 3 seconds. Aircraft struck a sign and caused damage to the right flap when it…Incident 20160323007479ILanding: Touchdown · Gila Bend, AZNight cross country into E63. Overflew the airport to check windsock, made a teardrop entry to enter the left downwind for runway 22. Once landed, student started to use both left and right right rudder, airplane became unstable, I asked for flight controls,…
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20170118002Tube · damagedPILOTS NOTED THE LEFT MAIN TIRE TO BE FLAT. INSPECTION OF THE FAILED TUBE REVEALED A 1 MM HOLE 90 DEGREES FROM THE VALVE STEM. THERE WAS NO EVIDENCE OF SCUFFING OR FOLDING ON THE INTERIOR OR EXTERIOR OF THE TUBE.SDR FQAR20161202062Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO, TWO INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET.SDR FQAR20150428030Exhaust Valve · damagedTHE PILOTS NOTED DURING THEIR FLIGHT THAT THE ENGINE WOULD RUN ROUGH BELOW 2000 RPM; A RETURN TO THE AIRPORT WAS UNEVENTFUL. A MAINTENANCE TECH GROUND RAN THE ENGINE AND CONFIRMED THE PROBLEM. WHILE PERFORMING A COMPRESSION TEST, THE NR 4 CYLINDER HAD LITTLE SDR FQAR20140129011Tube · failedDURING LANDING, THE LT MAIN TIRE WENT FLAT. THE WHEEL ASSY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSEMBLY ON THE RUNWAY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/22/2013 AND HAD SINCE ACCRUED 133 HOURS TIME IN SERVICE. SDR FQAR20140129013Tube · failedDURING A PREFLIGHT RUNUP, THE RT MAIN TIRE WENT FLAT. THE WHEEL ASSEMBLY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSY WHILE IN THE RUNUP AREA. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/22/2013 AND HAD SINCE ACCRUED 112 HOURSSDR 2003FA0000793Screw · backed outTHE SCREW THAT HOLDS THE CONTROL WHEEL TO THE YOKE WAS FOUND TO BE BACKED OUT ON BOTH THE PILOT AND CO-PILOTS WHEEL BY A .2500 TURN. WHEN THE SCREW BACKS OUT ENOUGH, IT FALLS OUT ALLOWING THE WHEEL TO ROTATE FREELY AROUND THE YOKE. THIS RESULTS IN NO FLIGHT
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
Earlier aircraft with this N-number · 1
This aircraft carried N445PA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.