- Registered owner
- Kopp Michael
- Location
- Reno, NV
- Owner type
- Individual
- Serial number
- E-1462
- Year built
- 1979
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- February 27, 1979
- Certificate issued
- April 23, 2020
- Expires
- April 30, 2030
- Mode S code
- A00CDC
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
Airworthiness directives that may apply · 86
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1970 | 1 |
|---|---|
| 1972 | 3 |
| 1973 | 2 |
| 1974 | 4 |
| 1975 | 2 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1981 | 2 |
| 1984 | 1 |
| 1986 | 1 |
| 1987 | 2 |
| 1988 | 6 |
| 1991 | 4 |
| 1992 | 1 |
| 1993 | 4 |
| 1994 | 2 |
| 1995 | 3 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 3 |
| 1999 | 3 |
| 2000 | 4 |
| 2001 | 7 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 3 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2019 | 2 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 101 ADs
Information bulletins that may apply · 17
Advisory, not mandatory.
See all 17 bulletins
NTSB investigations
No NTSB investigations matched to N102HLMatched 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 A36 aircraft
FAA incident reports
No FAA accident or incident reports matched to N102HLMatched 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 A36 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 2021FA0000103Hose · detachedPILOT HEARD A "POP" AND LOST ENGINE POWER. VERIFIED POWER LOSS BY MANIFOLD PRESSURE. COMPLETE ENGINE POWER LOSS WAS NOT REPORTED ONLY A PARTIAL POWER LOSS. PILOT DIVERTED TO ANOTHER AIRPORT AN LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING AND SHUTDOWN, INSPECSDR 2013FA0000672Adapter · crackedMECHANIC WAS PERFORMING MX ON THE AIRFRAME AND NOTICED EXHAUST STAINING ON THE OUTSIDE OF THE COWLING. ON OPENING THE COWLING THE MECHANIC DISCOVERED THE EXHAUST HAS BEEN PRESSURIZED AT EVERY ANNUAL SINCE INSTALLATION. THE CRACK WAS NOT EVIDENT AT THE LAST ASDR WS9R2013FA0000568Adapter · crackedEXHAUST STAINING ON THE OUTSIDE OF COWLING. DISCOVERED EXHAUST HAS BEEN PRESSURIZED AT EVERY ANNUAL SINCE INSTALLATION. CRACK WAS NOT EVIDENT IN AT THE LAST ANNUAL APPROX 90 HRS AGO. IT WOULD APPEAR THAT THE CRACK WAS CAUSED BY EXCESSIVE STRESS ON THE EXHA
STCs that may be installed · 577
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech A36
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