- Location
- Columbus, OH
- Owner type
- Government
- Serial number
- 18281581
- Year built
- 2005
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 30, 2005
- Certificate issued
- July 19, 2005
- Expires
- January 31, 2028
- Mode S code
- A99314
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-540 model are included below.
On this page
Airworthiness directives that may apply · 79
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1971 | 1 |
| 1973 | 3 |
| 1974 | 1 |
| 1975 | 2 |
| 1977 | 5 |
| 1978 | 3 |
| 1979 | 3 |
| 1981 | 1 |
| 1982 | 1 |
| 1983 | 1 |
| 1988 | 2 |
| 1989 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 2 |
| 1998 | 4 |
| 1999 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 4 |
| 2005 | 5 |
| 2006 | 5 |
| 2007 | 3 |
| 2008 | 7 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 1 |
| 2015 | 2 |
| 2017 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 2 |
See all 96 ADs
Information bulletins that may apply · 25
Advisory, not mandatory.
See all 29 bulletins
NTSB investigations
No NTSB investigations matched to N716HPMatched 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 Cessna 182T aircraft
FAA incident reports
No FAA accident or incident reports matched to N716HPMatched 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 Cessna 182T aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JRUR20120515003Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING RPM. AIRCRAFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON THE ENGINE AND FOUND THE NR 2 CYLINDER HAD AN ACSDR JRUR201205150002Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING RPM. ACFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON ENGINE AND FOUND NR 4 CYLINDER HAD AN ACCEPTABLE COSDR JRUR201205150001Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING THE RPM. ACFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON ENGINE AND FOUND THE NR 6 CYLINDER HAD A COMPSDR 2009FA0000514Exhaust Valve · stuckDURING COMPLIANCE OF SB 388C, 3 EXHAUST VALVE GUIDES FAILED TO HAVE SERVICEABLE MEASUREMENTS. NR 4 CYL EXHAUST VALVE STUCK FULLY CLOSED. VALVE MOVEABLE WITH MINIMAL PRESSURE, NO DAMAGE TO OTHER COMPONENTS. NR 6 CYL EXHAUST VALVE GUIDE CLEARANCE MEASURED .03
STCs that may be installed · 388
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 182T
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