- Registered owner
- Hansen Duane D
- Location
- Rockford, IL
- Owner type
- Individual
- Serial number
- 28R-31134
- Year built
- 1969
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 31, 1969
- Certificate issued
- November 29, 2023
- Expires
- November 30, 2030
- Mode S code
- A378D5
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 N3225RMatched 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
No FAA accident or incident reports matched to N3225RMatched 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-28R-180 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2021FA0000335Servo · failedGARMIN GSA28 PITCH TRIM SERVO FAILED AFTER APPROXIMATELY EIGHTEEN MONTHS / 68 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED "SERVO HARDWARE FAULT" AND RED "PTRIM" FLAG DURING FLIGHT, AND ELECTRIC PITCH TRIM BECAME INOPERATIVE. THE SERVO DISPLAYED A "RED" SDR 2021FA0000338Battery · failedGARMIN G5 FLIGHT INSTRUMENT BACKUP BATTERY FAILED AFTER APPROXIMATELY FOUR MONTHS / 16 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED "1%" BATTERY CHARGE STATUS AFTER NOT HAVING USED THE INSTRUMENT ON BACKUP POWER. BATTERY WOULD NOT CHARGE ABOVE 1%. "BATTESDR 2021FA0000337Battery · failedGARMIN G5 FLIGHT INSTRUMENT BACKUP BATTERY FAILED AFTER APPROXIMATELY TWO MONTHS / 8 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED "0%" BATTERY CHARGE STATUS AFTER NOT HAVING USED THE INSTRUMENT ON BACKUP POWER. BATTERY WOULD NOT CHARGE ABOVE 0%. NO "BATTSDR 2021FA0000194Battery · failedGARMIN G5 FLIGHT INSTRUMENT BACKUP BATTERY FAILED AFTER APPROXIMATELY THIRTEEN MONTHS / 50 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED A “BATTERY FAULT” ICON INDICATING THE FAILURE DURING A FUNCTIONAL CHECK.SDR 2021FA0000192Servo · failedGARMIN GSA28 PITCH TRIM SERVO FAILED AFTER APPROXIMATELY ELEVEN MONTHS / 45 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED “AFCS PREFLIGHT TEST FAILED” AND “SERVO HARDWARE FAULT” MESSAGES AND THE AUTOPILOT BECAME INOPERATIVE. THE SERVO DISPLAYED A “RED” STSDR 2021FA0000191Servo · failedGARMIN GSA28 ROLL SERVO FAILED AFTER APPROXIMATELY THREE MONTHS / 20 HOURS IN SERVICE . FLIGHT INSTRUMENTATION DISPLAYED A “SERVO HARDWARE FAULT” MESSAGE AND THE AUTOPILOT BECAME INOPERATIVE. THE SERVO DISPLAYED A “RED” STATUS LIGHT INDICATING FAILURE.
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