- Registered owner
- Arizaga Diana M
- Location
- Mamaroneck, NY
- Owner type
- Individual
- Serial number
- 28R-30069
- Year built
- 1967
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Certificate issued
- June 23, 2009
- Expires
- July 31, 2027
- Mode S code
- A44C7F
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N3760TMatched 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX2655Rib · corrodedDURING ANNUAL INSPECTION, FOUND BOTH LT AND RT FLAP OTBD HINGE BRACKETS ATTACHED TO FLAPS WERE WORKING FREE DUE TO CORROSION ON END CAPS. REMOVED AND REPLACED CAPS AND REATTACHED BRACKETS. CAUSE OF FAILURE APPEARS TO BE DISSIMILAR METAL CORROSION.SDR 97ZZZX2654Rib · corrodedDURING ANNUAL INSPECTION, FOUND BOTH LT AND RT FLAP OTBD HINGE BRACKETS ATTACHED TO FLAPS WORKING WERE FREE DUE TO CORROSION ON END CAPS. REMOVED AND REPLACED CAPS AND REATTACHED BRACKETS. CAUSE OF FAILURE APPEARS TO BE DISSIMILAR METAL CORROSION.SDR 97ZZZX2653Spar · corrodedDURING ANNUAL INSPECTION, FOUND LT WING MAIN SPAR UPPER CAP SEVERELY CORRODED ON FWD FLANGE. ONLY WAY TO DETECT IS WITH A MIRROR THROUGH FWD WHEELWELL INSPECTION PANEL. WING REMOVED AND SPAR REPLACED. SUBMITTER STATED INTERGRANULAR CORROSION IS THE CAUSE.
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