- Registered owner
- Pace Richard
- Location
- Leighton, AL
- Owner type
- Individual
- Serial number
- 32R-7885121
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Certificate issued
- January 3, 2019
- Expires
- January 31, 2029
- Mode S code
- A3634C
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-540 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 |
| 1973 | 1 |
| 1975 | 1 |
| 1977 | 2 |
| 1978 | 4 |
| 1979 | 2 |
| 1980 | 4 |
| 1981 | 2 |
| 1982 | 1 |
| 1983 | 1 |
| 1986 | 1 |
| 1989 | 2 |
| 1992 | 1 |
| 1993 | 1 |
| 1995 | 1 |
| 1996 | 5 |
| 1997 | 2 |
| 1998 | 4 |
| 1999 | 2 |
| 2000 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 4 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 1 |
| 2015 | 2 |
| 2017 | 2 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 2 |
Airframe · Piper PA-32RT-300
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-26-16Wing SparInformation bulletins that may apply · 27
Advisory, not mandatory.
See all 30 bulletins
NTSB investigations
No NTSB investigations matched to N31709Matched 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-32RT-300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N31709Matched 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-32RT-300 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2006FA0000604Control Cable · separatedCABLE TURNBUCKLE MALE END SEPARATED AT FITTING DURING ROLLOUT AFTER LANDING. FITTING SEEMS TO HAVE CORRODED FROM THE SHANK CORE AND PROGRESSED OUTWARD TO THE SURFACE OVER TIME. (K)SDR 2006FA0000611Control Cable · separatedUP ELEVATOR CABLE SEPARATED DURING LANDING FLARE.SDR 2006FA0000610Control Cable · separatedUP ELEVATOR CABLE SEPARATED DURING LANDING FLARE.SDR 2006FA0000609Control Cable · separatedUP ELEVATOR CABLE SEPARATED DURING LANDING FLARE.SDR 2006FA0000608Control Cable · separatedUP ELEVATOR CABLE SEPARATED IN LANDING FLARE.
STCs that may be installed · 324
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-32RT-300
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