- Location
- Columbus, OH
- Owner type
- Government
- Serial number
- 18281436
- Year built
- 2004
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- October 11, 2004
- Certificate issued
- January 31, 2005
- Expires
- June 30, 2029
- Mode S code
- A11791
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 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.
| 1969 | 1 |
|---|---|
| 1971 | 2 |
| 1973 | 3 |
| 1974 | 1 |
| 1975 | 2 |
| 1977 | 4 |
| 1978 | 2 |
| 1979 | 4 |
| 1980 | 1 |
| 1981 | 1 |
| 1983 | 1 |
| 1984 | 1 |
| 1988 | 2 |
| 1989 | 2 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 4 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 4 |
| 2005 | 5 |
| 2006 | 5 |
| 2007 | 2 |
| 2008 | 8 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 5 |
| 2013 | 2 |
| 2015 | 2 |
| 2017 | 2 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 2 |
| 2026 | 1 |
See all 100 ADs
Information bulletins that may apply · 21
Advisory, not mandatory.
See all 25 bulletins
NTSB investigations
No NTSB investigations matched to N17HPMatched 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 N17HPMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JRUR2020032560002Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
INSPECTED MAGNETO MODEL NO. 6351 P/N: SDR JRUR202003060001Magneto · unserviceableSUPPLEMENTAL INFORMATION
SLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF SDR JRUR2020030560002Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
INSPECTED MAGNETO MODEL NO. 6351 P/N: SDR JRUR201303060011Exhaust Valve · out of toleranceWHILE PERFORMING SB 388C, NR 6 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE WAS FOUND TO BE .010". BELOW ACCEPTABLE MINIMUM TOLERANCE OF .015". HAD 201 HOURS TIS SINCE SB 388C HAD PREVIOUSLY BEEN PERFORMED. VALVE DRIVEN OUT TO REMOVE IT FOR REAMING OF THE GUISDR JRUR201303060010Exhaust Valve · out of toleranceNR 3 EXHAUST VALVE TO GUIDE CLEARANCE WAS FOUND TO BE .012". BELOW ACCEPTABLE MINIMUM TOLERANCE OF .015". 201 HOURS TIS SINCE SB 388C HAD PREVIOUSLY BEEN PERFORMED. VALVE CLEARANCE MEASUREMENT HAD BEEN .020". VALVE HAD TO BE DRIVEN OUT TO REMOVE IT FOR RESDR 2006FA0000993Exhaust Valve · stuckDURING A PHASE 2 INSPECTION, CYLINDER NR 5 WAS FOUND TO HAVE LOW COMPRESSION (10/80) WITH A STRONG LEAK PASSED THE EXHAUST VALVE. SUBSEQUENT INSPECTION FOLLOWING THE INSTRUCTIONS FOUND IN LYCOMING SB 388C REVEALED THAT THE EXHAUST VALVE WAS PARTIALLY STUCK AN
STCs that may be installed · 357
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