- Registered owner
- Skywest Leasing Inc
- Location
- St George, UT
- Owner type
- Corporation
- Serial number
- 2843438
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- March 27, 2001
- Certificate issued
- July 7, 2025
- Expires
- July 31, 2032
- Mode S code
- A4EBB0
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 60
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 | 3 |
| 1980 | 4 |
| 1982 | 1 |
| 1986 | 2 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 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 · 22
Advisory, not mandatory.
See all 24 bulletins
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB GAA16CA237Accident · No injuriesData collectionFinal reportWickenburg, AZThe pilot's failure to monitor the parked vehicle, which resulted in a ground collision and substantial damage to the left wing.NTSB LAX08CA076Accident · No injuriesData collectionFinal reportPhoenix, AZThe pilot's inadequate compensation for the crosswind condition and failure to maintain directional control during the landing roll. Contributing to the accident was the crosswind condition.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20160512008799ATaxi · Wickenburg, AZWhile taxing to parking area at E25 airport, pilot was focused on avoiding a parked aircraft off his right wing. After clearing the parked aircraft, the pilot saw a parked airport operations truck on the left side of the aircraft next to a hangar. Pilot tried…Accident 20080315013169ARoll-Out (Fixed Wing) · Phoenix, AZ(-23) The solo student pilot landed on runway 25R at kdvt. He attempted to vacate the runway at too high a speed and lost control of the aircraft. He hit the dirt on the left side (south side) and collapsed the gear. The aircraft suffered substantial damage.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20180919050Wire · deterioratedDURING A SCHEDULED INSPECTION, FOUND THE POWER WIRE FOR THE START BADLY DETERIORATED WITH NUMEROUS BARE SECTIONS OF WIRE EXPOSED. THE WIRE APPEARS TO BE AUTOMOTIVE TYPE WIRE AND WAS SUPPLIED AS PART OF THE INSTALLATION KIT.SDR FQAR20170802072Channel · crackedA CHANNEL IN THE LEFT WING WAS FOUND CRACKED. CHANNEL IS LOCATED INBOARD ON THE WING'S LOWER SURFACE AND IS RIVETED TO SKIN PANEL.SDR FQAR20170614047Magneto · malfunctionedPILOT COULD NOT START ENGINE AFTER SIX ATTEMPTS. INSPECTION BY MAINTENANCE PERSONELL REVEALED THE NEWLY INSTALLED LEFT MAGNETO WAS MALFUNCTIONING.SDR FQAR20170611038Window Frame · corrodedCORROSION WAS FOUND TO LEFT WINDSCREEN FRAME STRUTURE. CORRODED AREA WAS ALONG OUTBOARD, LOWER END OF WINDSCREEN. IT IS SUSPECTED THAT CORROSON WAS CAUSED BY LEAKAGE FROM IMPROPERLY FITTED WINDSCREEN OR CONDENSATION.SDR FQAR20170327013Tube · splitTHE RIGHT MAIN TIRE WENT FLAT AS THE PILOTS EGRESSED. VISUAL INSPECTION OF THE TIRE TUBE REVEALED A SLIT .125" IN LENGTH. THERE WERE NO FOLDS TO THE TUBE THAT WOULD HAVE CAUSED A HOLE TO APPEAR.SDR FQAR20161117058Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO, 2 INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. THESE CRACKS CAN ONLY BE SEEN WHEN THE ELT TRAY IS REMOVED.SDR FQAR20150524050Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 4 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-02908.SDR FQAR20150524049Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 3 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE AND AT THE EXHAUST VALVE SEAT. THE CYLINDER HEAD CASTING NR C-02883.SDR FQAR20150524048Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 2 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-02284.SDR FQAR20150524047Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 1 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-02859.SDR FQAR20140617038Pump · blockedDURING TAKEOFF, FUEL PRESSURE GAUGE GAVE A READING OF 0 PSI. THE ACFT HAD TO ABORT TAKEOFF AND RETURN TO RAMP AT DEPARTING AIRPORT. MAINTENANCE GROUND RAN ACFT WITH SAME RESULTS AND REPLACED THE ELECTRIC FUEL PUMP. AFTER THE FUEL PUMP WAS REPLACED, ACFT OPERSDR FQAR20140129020Sensor · contaminatedTHE PILOT WAS PERFORMING A PREFLIGHT ENGINE RUN, WHEN THE RIGHT MAG WAS SWITCHED OFF, THE ENGINE RAN ROUGH; RETURNED TO THE RAMP AND REPORTED THE PROBLEM. THIS AIRCRAFT IS EQUIPPED WITH AN ELECTRONIC IGNITION SYSTEM (EIS) INSTALLED IAW STC SA02987CH THAT INCOR
STCs that may be installed · 369
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 N416PA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.