Registered owner
Skywest Leasing Inc
Owner type
Corporation
Serial number
2843468
Year built
2001
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
July 6, 2001
Certificate issued
July 7, 2025
Expires
July 31, 2032
Mode S code
A50BC1

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.

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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.

1963In forceSuperseded2026
ADs by the year they took effect: 79 ADs
19631
19641
19661
19671
19692
19774
19794
19806
19811
19821
19862
19881
19893
19911
19921
19951
19964
19971
19982
19991
20001
20011
20021
20042
20053
20067
20071
20083
20091
20103
20122
20131
20151
20161
20172
20182
20212
20222
20243
20261
See all 80 ADs

Information bulletins that may apply · 26

Advisory, not mandatory.

See all 35 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 · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR FQAR202212080009Arm · brokenDURING AN INSPECTION FOUND CONTROL ARM ASSEMBLY FOR RUDDER TRIM/ RUDDER CABLE CRACKED AT ATTACH POINT., CONNECT ARM ASSEM BROKEN, 66661-000Nov 12, 2022 · N424PA · Piper PA28181 · Rudder Tab Control SystemSDR FQAR20191021013Regulator Valve · brokenPILOT SQUAWKED VAC INOP, VAN ANNUNCIATOR INOP, TROUBLESHOOTING REVEALED THAT THE VAC INOP SWITCH HAD FALLEN OFF THE VACUUM REGULATOR, REGULATOR WAS REMOVED AND INSPECTED, FOUND THE REGULATOR TO BE GLUED TOGETHER AT ALL FITTINGS, THE REASON THE INOP SWITCH IS NOct 17, 2019 · N424PA · Piper PA28181 · Vacuum Distribution SystemSDR FQAR20170608044Door Frame · crackedTHE CABIN DOOR PAN THAT COMPRISES THE LOWER INBOARD PART OF DOOR FRAME WAS FOUND CRACKED. CRACK WAS FROM AFT LIGHTENING HOLE TO EDGE OF MATERIAL.Jun 8, 2017 · N424PA · Piper PA28181 · Fuselage Main, StructureSDR FQAR20170608040Fitting · corrodedCORROSION WAS FOUND TO RIGHT UPPER, FWD COCKPIT FITTING. THE FITTING IS LOCATED AT RIGHT, LOWER END OF WINDSCREEN NEAR INSTRUMENT PANEL. IT IS SUSPECTED THAT CORROSON WAS CAUSED BY LEAKAGE FROM IMPROPERLY FITTED WINDSCREEN OR CONDENSATION.Jun 8, 2017 · N424PA · Piper PA28181 · Fuselage Main, StructureSDR FQAR20150105002Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND IS USED TO MOUNT THE FLAP HANDLE ASSY. IT CONTAINS NUT PLATES TO Jan 2, 2015 · N424PA · Piper PA28181 · Fuselage Main, Attach Fittings

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.

See all 383 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N424PA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.