- Registered owner
- Martin Rolf M
- Location
- Wellsburg, NY
- Owner type
- Individual
- Serial number
- 24-1000
- Year built
- 1980
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- May 7, 1980
- Certificate issued
- November 27, 2017
- Expires
- November 30, 2027
- Mode S code
- A7C66B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 32
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 1 |
|---|---|
| 1977 | 3 |
| 1978 | 2 |
| 1979 | 1 |
| 1980 | 3 |
| 1981 | 2 |
| 1986 | 3 |
| 1989 | 1 |
| 1992 | 1 |
| 1996 | 1 |
| 1998 | 5 |
| 2000 | 1 |
| 2001 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2012 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 32 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N60RPMatched 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 Mooney M20J aircraft
FAA incident reports
No FAA accident or incident reports matched to N60RPMatched 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 Mooney M20J aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BQVD201506090001Ring · seizedNR 4 CYLINDER WAS REMOVED AND DISCOVERED THE FOLLOWING: OIL CONTROL RING WAS SEIZED IN PISTON. PISTON, PISTON BORES WORN IN AREA WHERE PIN RESIDES ON BOTH SIDES OF PISTON. NO WRIST PIN CAP WEAR FOUND. CONTACT BEING MADE BETWEEN PISTON SKIRT END SURFACE & CSDR 2011FA0000532Tube · failedRT MAIN TIRE FLAT AT RUN UP AREA. REMOVED WHEEL. DISASSEMBLED AND FOUND BUTYL TYPE G15-G00-6 TUBE WITH HALF INCH LONG SLIT IN SIDEWALL. INSPECTED TIRE AND FOUND NO HOLES OR SLITS IN SIDEWALL AND NO ABNORMALITY ON INSIDE OF TIRE. THIS IS THE THIRD BUTYL TYP
STCs that may be installed · 376
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Mooney M20J
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
Earlier aircraft with this N-number · 1
This aircraft carried N60RP before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.