- Registered owner
- Claridge Management Group LLC
- Location
- Sunrise, FL
- Owner type
- LLC
- Serial number
- 32R 7780018
- Year built
- 1976
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- January 15, 2024
- Expires
- January 31, 2031
- Mode S code
- A75550
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 31
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1976 | 3 |
|---|---|
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 4 |
| 1981 | 2 |
| 1986 | 1 |
| 1989 | 1 |
| 1993 | 1 |
| 1996 | 2 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2010 | 1 |
| 2013 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
Airframe · Piper PA-32R-300
AD 2024-14-03Autopilot SystemAD 2023-09-09Exhaust Turbine System (Recip)AD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Piper PA-32R-300
SAIB 2022-20Wing SparSAIB AIR-21-10Wing, Attach Fittings (JASC 5740)SAIB AIR-21-07WING SPAR, Verification of Correct Washers used with Wing Spar Attach BoltsSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-11-12R1Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach FittingSAIB CE-14-23Powerplant; Air IntakeSAIB CE-11-42Flight Controls: Control Cable/Pulley InspectionsSAIB CE-11-14Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point CorrosionSAIB CE-11-13Wings - Piper PA-28, PA-32, PA-34 Forward Spar CorrosionSAIB CE-11-11Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting CorrosionSAIB CE-11-10Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and RibsSAIB CE-11-01Stabilizers -Horizontal Stabilator TurnbuckleSAIB CE-09-23Fuel: Piper PA-28, PA-32, PA-34SAIB CE-09-12Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 InstallationsHistorical bulletins · 1
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB IAD97LA092Accident · No injuriesLimited investigationFinal reportDefiance, OHThe failure of a wheel rim due to overstress separation with no clear evidence initiating event.NTSB NYC94LA105Accident · No injuriesLimited investigationFinal reportPut-In-Bay, OHThe pilot's inadequate control and failure to maintain directional control which resulted in collision with a sign.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 19970620015339ADefiance, OH(-23) Pilot reported that during take-off roll on runway 30 at Defiance memorial (CFI) left main tire went flat. The left main wheel inner half was noted to have 6 inches of rim area missing and the tire has a 4 inch cut in the inner side wall above the bead…Incident 19941017040949IFcd/Prec Ldg From Cruise · Cincinnati, OHOn test flight to check auto gear. Circuit breaker popped gear intransit. Landed gear up. Frayed wire shorted out.Accident 19940702017489ARoll-Out (Fixed Wing) · Put In Bay, OHLanded short of threshold. Veered into a steel property sign. Left gear collapsed and left wing seperated.
Service difficulty reports
No reports matched to N5716FGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Piper PA-32R-300 aircraft
STCs that may be installed · 290
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-32R-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