- Registered owner
- Air Force Life Cycle Management Center
- Location
- Lexington, MA
- Owner type
- Government
- Serial number
- U20606200
- Year built
- 1981
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, research and development, crew training
- Airworthiness date
- August 7, 2026
- Certificate issued
- July 6, 2016
- Expires
- July 31, 2029
- Mode S code
- A21113
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 65
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 1 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 5 |
| 1980 | 3 |
| 1981 | 2 |
| 1985 | 2 |
| 1986 | 4 |
| 1987 | 1 |
| 1988 | 5 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 3 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 3 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 2 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 6 |
| 2024 | 1 |
See all 73 ADs
Information bulletins that may apply · 16
Advisory, not mandatory.
See all 16 bulletins
NTSB investigations
No NTSB investigations matched to N232MTMatched 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 TU206G aircraft
FAA incident reports
No FAA accident or incident reports matched to N232MTMatched 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 TU206G 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 2012FA0000157Bolt · looseDURING TROUBLESHOOTING FOR ALTERNATOR NOISE, INSPECTED ALTERNATOR AND FOUND BOLT LOOSE INSIDE ALTERNATOR CASE. REMOVED ALTERNATOR AND DISASSEMBLED, FOUND DIODE RECTIFIER BRIDGE BOLT HAD BACKED OUT AND HAD CONTACTED THE ROTOR, BENDING THE BOLT AND ELONGATING TSDR 20010508CW009Coil · inoperativeMAGNETO INOPERATIVE BELOW 1,000 RPMS. OK AT 1,700 RPMS PER THE P.O.M. PILOTS HAD DONE A MAG CHECK AT IDLE WHICH LEAD TO THE DISCOVERY. OPENED MAGNETO FOR INSPECTION. TESTED COIL AND FOUND SECONDARY WINDING. RESISTANCE TOO HIGH BY FACTOR OF 10.SDR 20010508CW008Frame · crackedOBSERVED AN OIL LEAK FROM MAG BASE. FOUND MOUNTING FLANGE CRACKED AROUND LOWER CLAMPING WASHER. REMOVED MAG AND FOUND APPROX 2 INCH PIECE OF MOUNTING FLANGE BROKEN OFF.SDR 20000417SH014Alternator · failedALTERNATOR FAILED DURING FLIGHT. TROUBLESHOOTING WITH ALTERNATOR TEST BOX SHOWED NO OUTPUT. CHECKING FIELD WINDING RESISTANCE PER CESSNA MM SHOWED EXCESSIVELY HIGH RESISTANCE. ALTERNATOR REPLACED. (X)SDR 99ZZZX118Switch · inoperativeDURING ANNUAL INSPECTION, FOUND STALL WARNING LIFT DETECTOR INOPERABLE DUE TO HIGH RESISTANCE. ALSO DISCOVERED THE WRONG LIFT SWITCH WAS INSTALLED PER CONVERSATION WITH SAFE FLIGHT. REPLACED P/N 146 WITH CORRECT P/N 150.SDR 98ZZZX4528Switch · wornDURING ANNUAL, DISCOVERED AD 93-05-06 NOT C/W. INSPECTED IGNITION SWITCH AND FOUND SIGNS OF MODIFIED STARTER RELAY IAW CESSNA SEB 91-5- R1. NOTE: AD IS RECURRING EVERY 2,000 HOURS AFTER INITIAL COMPLIANCE.
STCs that may be installed · 473
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna TU206G
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA3247NMInstallation of an air to air intercooler in the engine induction system downstream of the turbocharger. (TU206G S/N U20603522 thru U20606921 and up)STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.