- Registered owners
- Schlesinger Henry RSchlesinger Bonnie L
- Location
- Castalian Springs, TN
- Owner type
- Partnership
- Serial number
- 172RG0580
- Year built
- 1980
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 1, 1980
- Certificate issued
- June 27, 2026
- Expires
- June 30, 2033
- Mode S code
- A7F1D9
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.
On this page
Airworthiness directives that may apply · 78
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 |
| 1968 | 1 |
| 1969 | 3 |
| 1971 | 2 |
| 1973 | 2 |
| 1974 | 2 |
| 1977 | 3 |
| 1979 | 2 |
| 1980 | 5 |
| 1981 | 5 |
| 1982 | 1 |
| 1983 | 2 |
| 1985 | 1 |
| 1986 | 1 |
| 1988 | 2 |
| 1989 | 2 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 4 |
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 6 |
| 2007 | 1 |
| 2008 | 2 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 1 |
See all 84 ADs
Information bulletins that may apply · 21
Advisory, not mandatory.
See all 33 bulletins
NTSB investigations
No NTSB investigations matched to N6105VMatched 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 172RG aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 95ZZZX6168Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6167Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6166Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6165Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6163Cylinder · crackedENGINE BECAME ROUGH DURING FLIGHT. UPON LANDING AND INSPECTION, IT WAS DETERMINED THAT CYLINDER NR 4 WOULD NOT PASS CYLINDER LEAKAGE TEST. AFTER FURTHER INSPECTION, CYLINDER WAS FOUND TO BE CRACKED ONE-HALF WAY AROUND CIRCUMFERENCE BETWEEN FINS AT JUNCTION O
STCs that may be installed · 310
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 172RG
STC SA00709CHInstallation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev.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.