- Registered owners
- Ferrell AlanBrooks Benjamin
- Location
- Arlington, OH
- Owner type
- Co-owned
- Serial number
- D-7112
- Year built
- 1963
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard
- Airworthiness date
- January 17, 1963
- Certificate issued
- February 13, 2018
- Expires
- February 29, 2028
- Mode S code
- A23880
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental I0-470 model are included below.
On this page
Airworthiness directives that may apply · 54
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 |
|---|---|
| 1967 | 1 |
| 1970 | 1 |
| 1972 | 3 |
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 2 |
| 1984 | 1 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 2 |
| 1999 | 2 |
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2007 | 2 |
| 2009 | 1 |
| 2010 | 2 |
| 2012 | 1 |
| 2019 | 1 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 67 ADs
Information bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Beech P35
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-12-36Flight Controls: AileronSAIB CE-12-18Flight Controls: Elevator Control Cable ConditionSAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-09-02Publication error of AD 89-05-02 in the FAA Regulatory Guidance LibraryEngine · Continental I0-470 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-08Reciprocating Engine Cylinder SectionNTSB investigations
No NTSB investigations matched to N242MMatched 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 Beech P35 aircraft
FAA incident reports
No FAA accident or incident reports matched to N242MMatched 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 Beech P35 aircraft
Service difficulty reports
No reports matched to N242MGeneral 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 Beech P35 aircraft
Reports on N242M not matched to an aircraft · 2
They name N242M, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2022FA0000217Mount · crackedENGINE MOUNT TRUSS ASSEMBLY HAS CRACKS APPROXIMATELY HALF WAY THROUGH THE BOTTOM TRUSS TUBE AT THE JUNCTION FOR THE MID-SPAN DOWN TUBE WELDS. THE CRACKS ARE PRESENT ON BOTH SIDES OF THE LOWER TRUSS (INBD AND OUTBD).SDR 2004FA0000549Heat Shield · gougedHEAT SHIELD WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROXIMATELY .200 INCH IN LENGTH AND APPROXIMATELY .045 INCH DEEP.
STCs that may be installed · 540
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech P35
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