- Registered owners
- Watson Keith AVan Breda Arelis
- Location
- Sale Creek, TN
- Owner type
- Co-owned
- Serial number
- 28R-7335072
- Year built
- 1972
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- November 14, 1972
- Certificate issued
- April 1, 2014
- Expires
- April 30, 2027
- Mode S code
- A0E075
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 · 76
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 | 2 |
| 1969 | 3 |
| 1971 | 2 |
| 1972 | 4 |
| 1973 | 2 |
| 1974 | 1 |
| 1975 | 3 |
| 1976 | 1 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1981 | 1 |
| 1982 | 2 |
| 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 | 3 |
| 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-200
AD 2024-14-03Autopilot SystemAD 2022-03-15Fuel Quantity IndicatorAD 2020-26-16Wing SparInformation bulletins that may apply · 28
Advisory, not mandatory.
See all 32 bulletins
NTSB investigations
No NTSB investigations matched to N15597Matched 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-200 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX1699Filler Neck · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION. FOUND THE FUEL TANK FILLER NECK CORRODED THROUGH INTO THE FUEL SDR 97ZZZX1698Fitting · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.SDR 97ZZZX1697Fitting · corrodedDURING ANNUAL INSPECTION, FOUND AFT WING FITTINGS AND ADJACENT STRUCTURE CORRODED. PIPER SB977 ADDRESSES THIS PROBLEM. CAUSE DUE TO WINDOW SEALS FAILING AND MOISTURE REMAINING IN THE INSULATION.SDR 97ZZZX1702Mount · crackedMOST OF THE TUBES ON THIS ENGINE/LANDING GEAR MOUNT HAD TO BE REPLACED DUE TO CORROSION, CRACKS, OR CHAFING. THE CHAFING WAS FROM OLD LOOP-TYPE (ADEL) CLAMPS THAT HAD NOT BEEN REPLACED WHEN THE RUBBER CUSHIONS DRIED OUT. THE AIRCRAFT HAD BEEN IN AN ACCIDENT SDR 97ZZZX1701Pitot Head · corrodedTHE PITOT MAST WAS SO CORRODED THE AIR INLET HOLES WERE CLOSED APPROXIMATELY ONE-FOURTH DUE TO THE BUILD-UP OF THE CORROSION. SUBMITTER STATED THE AIRCRAFT HAD BEEN BASED IN A CORROSIVE ENVIRONMENT (FLORIDA).SDR 97ZZZX1700Belt · failedA COMMON PROBLEM THAT SUBMITTER HAS FOUND OVER THE YEARS, WITH PIPER PRODUCTS ESPECIALLY, IS THE USE OF AUTOMOTIVE OR UNAPPROVED ALTERNATOR DRIVE BELTS. IN THIS CASE, A NAPA AUTOMOTIVE BELT WAS INSTALLED.
STCs that may be installed · 398
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-200
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