- Registered owner
- International Air Services Inc Trustee
- Location
- Carson City, NV
- Owner type
- Corporation
- Serial number
- 21061679
- Year built
- 1976
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 4, 1977
- Certificate issued
- April 10, 2012
- Expires
- April 30, 2028
- Mode S code
- A9D3D8
From the FAA registry file of October 27, 2026. The registry lists only the engine series, so ADs for every Continental IO-520 model are included below.
On this page
NTSB investigations
No NTSB investigations matched to N732QAMatched 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 210M 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.
Airworthiness directives that may apply · 72
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 |
|---|---|
| 1972 | 1 |
| 1974 | 2 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 6 |
| 1980 | 3 |
| 1981 | 2 |
| 1982 | 1 |
| 1985 | 2 |
| 1986 | 1 |
| 1987 | 3 |
| 1988 | 5 |
| 1990 | 1 |
| 1991 | 2 |
| 1993 | 3 |
| 1994 | 2 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 3 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 3 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
See all 83 ADs
Information bulletins that may apply · 22
Advisory, not mandatory.
See all 23 bulletins
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 99ZZZX122Cylinder · crackedCOMPRESSION TEST REVEALED 71/80 FOR NR 1 CYLINDER AND 25/80 FOR NR 2 CYLINDER. UPON APPLICATION OF LEAK DETECTOR LIQUID, A CRACK WAS FOUND IN NR 1 CYLINDER ADJACENT TO INTAKE PORT BETWEEN 16TH AND 17TH FIN. CRACK EXTENDS FROM EXHAUST VALVE TO SPARK PLUG HOLESDR 99ZZZX121Cylinder · crackedCOMPRESSION TEST REVEALED 71/80 FOR NR 1 CYLINDER AND 25/80 FOR NR 2 CYLINDER. UPON APPLICATION OF LEAK DETECTOR LIQUID, A CRACK WAS FOUND IN NR 1 CYLINDER ADJACENT TO INTAKE PORT BETWEEN 16TH AND 17TH FIN. CRACK EXTENDS FROM EXHAUST VALVE TO SPARK PLUG HOLESDR 98ZZZX3668Pump · failedAIRCRAFT BROUGHT IN FOR MAINTENANCE. FOUND PUMP MOTOR CONTINUING TO RUN. TROUBLESHOOTING REVEALED THAT UNIT WOULD NOT PRODUCE PROPER PRESSURE TO TRIP PRESSURE SWITCH. REMOVED AND INSTALLED OVERHAULED UNIT. SYSTEM OPS NORMAL.
STCs that may be installed · 442
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 210M
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA04211CHInstallation of an engine modified per STC SE0417CHSTC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.