- Registered owner
- Tucker Zane Griffin
- Location
- Albany, OR
- Owner type
- Individual
- Serial number
- 28R-30196
- Year built
- 1967
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 9, 1967
- Certificate issued
- November 6, 2018
- Expires
- November 30, 2028
- Mode S code
- A477FB
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.
On this page
Airworthiness directives that may apply · 75
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1966 | 1 |
| 1967 | 3 |
| 1968 | 2 |
| 1969 | 3 |
| 1971 | 2 |
| 1972 | 4 |
| 1973 | 2 |
| 1975 | 3 |
| 1976 | 1 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1982 | 1 |
| 1986 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 4 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 6 |
| 2007 | 1 |
| 2008 | 4 |
| 2009 | 1 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 1 |
| 2015 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 1 |
Airframe · Piper PA-28R-180
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-26-16Wing SparInformation bulletins that may apply · 27
Advisory, not mandatory.
See all 31 bulletins
NTSB investigations
No NTSB investigations matched to N3872TMatched 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-28R-180 aircraft
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.
Incident 20090313003349ITakeoff · Columbia, CA(-23) Right main landing gear retracted during the takeoff roll. Damage confined to right wing tip, entry step and right stabilator tip. Initial troubleshooting indicates landing gear electrical system at fault. Mechanic will submit m or d.Incident 20050703033179ITakeoff Ground Roll · Minden, NV(-23) During initial take-off roll left landing gear retracted slowly (uncommanded) and pilot was able to abort with minimal damages. Airplane slid to stop on concrete runway with very minimal structural damages (left wing tip, left wing lower protuberances,…
Service difficulty reports · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
STCs that may be installed · 384
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-28R-180
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