- Registered owner
- N7614j LLC
- Location
- Berkeley Heights, NJ
- Owner type
- LLC
- Serial number
- 28R-31006
- Year built
- 1968
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- October 21, 1968
- Certificate issued
- June 22, 2020
- Expires
- June 30, 2027
- Mode S code
- AA482C
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 N7614JMatched 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 N7614JMatched 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 96ZZZX2081Rib Assy · crackedDURING C/W PIPER AD 95-20-7, THE RIB ASSYS ON BOTH SIDES WERE FOUND CRACKED UNDERNEATH THE DRAG BRACE STUD BRACKETS. CRACKS WERE APPROXIMATELY 2 TO 3 INCHES LONG. REPLACEMENT OF THE RIB ASSYS ARE REQUIRED. SUBMITTER STATED THE NEW RIBS ARE MADE OF THICKER MSDR 96ZZZX2080Rib Assy · crackedDURING C/W PIPER AD 95-20-7, THE RIB ASSYS ON BOTH SIDES WERE FOUND CRACKED UNDERNEATH THE DRAG BRACE STUD BRACKETS. CRACKS WERE APPROXIMATELY 2 TO 3 INCHES LONG. REPLACEMENT OF THE RIB ASSYS ARE REQUIRED. SUBMITTER STATED THE NEW RIBS ARE MADE OF THICKER MSDR 96ZZZX2060Support · crackedDURING A ROUTINE ANNUAL INSPECTION, BOTH LOWER AILERON BELLCRANK BRACKETS WERE FOUND CRACKED BY THE FORWARD BOLT. SUBMITTER STATED THIS IS MOST LIKELY CAUSED BY EITHER IMPROPERLY ADJUSTED AILERON STOPS OR BY NOT 'TYING' THE CONTROLS WHILE THE AIRCRAFT IS PARK
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