- Registered owner
- Gregg Flying Service Inc
- Location
- Durango, CO
- Owner type
- Corporation
- Serial number
- U20603340
- Year built
- 1976
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 20, 2013
- Certificate issued
- June 15, 2001
- Expires
- August 31, 2027
- Mode S code
- ABA03E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 2 |
|---|---|
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 3 |
| 1978 | 1 |
| 1979 | 4 |
| 1980 | 3 |
| 1981 | 2 |
| 1985 | 2 |
| 1986 | 2 |
| 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 72 ADs
Information bulletins that may apply · 15
Advisory, not mandatory.
Airframe · Cessna TU206F
SAIB CE-12-41Flight Controls Loose Glide ScrewSAIB CE-12-14Three Alternative Methods of Compliance for AD 2011-10-09SAIB CE-10-40R1Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanesSAIB CE-09-39Leveling and Weighing: Maximum landing gross weight limitation for Cessna U206F, U206G, TU206F, TU206G series airplanes equipped with Flint Aero STC SA4366WESAIB CE-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsEngine · Continental TSIO-520-M
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB NE-17-11POWERPLANT Engine damage as a result of kickbackSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-10-07Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.SAIB NE-09-08Reciprocating Engine Cylinder SectionSAIB NE-07-09R1Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum HeadNTSB investigations
No NTSB investigations matched to N8482QMatched 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 TU206F 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR IKJ2007F00000Cylinder · crackedCYLINDER DEVELOPED CRACK FROM INTAKE SEAT AROUND THE OUTER PORTION OF CYLINDER TO SPARK PLUG HOLE. CRACK FOLLOWED THE PATH OF 1 OR 2 FINS AND WENT JUST AFT (CASE SIDE) OF FUEL INJECTOR PORT. THE CRACK WAS ALLOWING NOTICABLE FUEL LEAK/STAIN NEAR INJECTOR PORTSDR 99ZZZX2133Wheel · failedWHEEL FAILED WHILE TAXIING. APPARENTLY, ONE OF THE 6 BOLTS ON OUTSIDE FLANGE LOOSENED TORQUE OVER TIME. A FEW BOLTS BROKE AND CENTER HUB FRACTURED AT REMAINING BOLT LOCATION. SUBMITTER RECOMMENDED EITHER A LIFE-LIMIT ON PART, OR THE OPTION TO INSTALL BOLT T
STCs that may be installed · 466
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna TU206F
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.