- Registered owner
- Grinch Robert J
- Location
- Ridgewood, NJ
- Owner type
- Individual
- Serial number
- 28-7790452
- Year built
- 1977
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- April 7, 1977
- Certificate issued
- June 19, 2001
- Expires
- July 31, 2027
- Mode S code
- A3A79E
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 N3344QMatched 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 N3344QMatched 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2009FA0000380Alternator · failedALTERNATOR FAILED AFTER 116 HOURS TIME IN SERVICE SINCE OVERHAULED. THESE SHOULD HAVE A LONGER LIFE SPAN.SDR 96ZZZX488Bearing Cup · corrodedOWNER COMPLAINED OF A 'CLUNKING' NOISE COMING FROM ONE WHEEL AS THE PLANE WAS PULLED OUT FROM A HANGAR. INSPECTION SHOWED ALL THREE WHEELS TO HAVE CORRODED WHEEL BEARINGS. BEARINGS WERE REPLACED. THE AIRCRAFT RECEIVED AN ANNUAL INSPECTION ON 11-17-94 AT 1,4SDR 96ZZZX354Control Cable · crossedWHILE PERFORMNG AN ANNUAL INSPECTION, FOUND THE RUDDER CABLES WERE CROSSED IN THE TAIL. THE CONTROL SURFACES WERE REMOVED FOR BALANCE CHECKING AFTER REPAINTING ABOUT SIX MONTHS PRIOR. THIS WAS THE ONLY LOGGED ENTRIES ABOUT THE CONTROL SYSTEM IN THE LAST YEAR
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