- Registered owner
- Western Flying Club Inc
- Location
- Burlington, NC
- Owner type
- Corporation
- Serial number
- 28-7990206
- Year built
- 1978
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- November 30, 1978
- Certificate issued
- July 8, 1997
- Expires
- November 30, 2027
- Mode S code
- A7C3CA
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.
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 N6NSMatched 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
No FAA accident or incident reports matched to N6NSMatched 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-28-181 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ZB0R201100004Channel · corrodedDURING ANNUAL INSP, FOUND RT WING FWD ATTACH POINT FUSELAGE STEEL FITTINGS RUSTED. SUSPECTED CAUSE IS POORLY FITTING CABIN DOOR SEAL ALLOWING WATER TO COME IN AND DRAIN DOWN ONTO THE FITTINGS. REPLACED BOTH PARTS WITH NEW.SDR ZB0R201100003Fitting · corrodedDURING ANNUAL INSP, FOUND LT WING AFT ATTACH POINT STEEL FITTING SEVERELY CORRODED. REPLACED PART WITH NEW.SDR ZB0R201100002Shaft · wornDURING ANNUAL INSP, FOUND STABILATOR TRIM BARREL AND SHAFT WORN BEYOND LIMITS. PARTS REPLACED WITH NEW.SDR ZB0R201100001Fitting · corrodedDURING ANNUAL INSP, FOUND BOTH LT AND RT WINDOW FITTINGS RUSTED MORE THAN 50 PERCENT THROUGH. THIS IS ATTRIBUTED TO THE WINDOWS NOT BEING SEALED PROPERLY ALLOWING WATER TO GET IN AND CORRODE THE STEEL FITTINGS. BOTH FITTINGS WERE REPLACED WITH NEW. THERE WAS
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