- Registered owner
- Winkler Jeffery L
- Location
- Brush, CO
- Owner type
- Individual
- Serial number
- U206-0507
- Year built
- 1966
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 8, 1966
- Certificate issued
- March 14, 2001
- Expires
- April 30, 2027
- Mode S code
- A5EBEC
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 1 |
|---|---|
| 1971 | 1 |
| 1974 | 1 |
| 1975 | 2 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 4 |
| 1980 | 1 |
| 1981 | 1 |
| 1984 | 1 |
| 1985 | 2 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 5 |
| 1990 | 1 |
| 1991 | 1 |
| 1993 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2016 | 1 |
| 2020 | 2 |
| 2022 | 2 |
| 2023 | 5 |
See all 62 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Airframe · Cessna TU206A
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-09-10Availability of Secondary Seat Stops for Pilot and Copilot SeatsEngine · Continental GTSIO-520-C
SAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB 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-09-08Reciprocating Engine Cylinder SectionNTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB WPR09CA017Accident · No injuriesData collectionFinal reportBuckeye, AZAnother airplanes total loss of wheel brakes while taxing which resulted in the pilot of the other aircraft colliding with a standing aircraft. Contributing to the accident was the other airplanes low brake hydraulic fluid.NTSB FTW00LA019Accident · No injuriesLimited investigationFinal reportJeanerette, LAThe total loss of power for undetermined reasons and the pilot's failure to maintain airspeed, while clearing a ditch during a forced landing, resulting in an inadvertent stall. A factor was the ditch.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20081019850169AGround/Ramp/Ma · Buckeye, AZ(-23) On the south end of the ramp area east of the runway 17/35, the pilot of the Cessna 206 with the engine running was preparing to taxi to runway 17 with 5 skydivers onboard. The Cessna pilot observed a Piper cub that had been parked 2 spaces to the north…Accident 19991023045119AJeanerette, LA(-23) The pilot stated that the a/c lost power during the descent after completing a parachute drop. The pilot was able to restart the engine during the descent, but lost power again on downwind for landing. The a/c crashed short of the runway after the pilot…
Service difficulty reports
No reports matched to N4807FGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Cessna TU206A aircraft
STCs that may be installed · 398
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna TU206A
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.