Cessna TurboCharged 206

Number of Active Aircraft: 1113 Active- Map


Years Produced: 1965-86 Turbo Charged version of the 206, increases the power from 285 to 310 and but the model also has a much higher empty weight effectively decreasing the usable load.

Wikipedia Cessna 206 reference:

Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2279 lbs
Max Weight 3600 lbs
Useful Load: 1321 lbs
Engine Name Lycoming TIO-540-AJ1A
Engine Number 1
Horsepower 310 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 27000 ft
Max Fuel 66.8 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 164 kts
GPH (75% BHP): 19.1
MPG (75% BHP) 8.6
Range (75% BHP): 474 nm
Fuel Cost Per Seat Mile 0.12 $
Fuel Cost Per Hour 114.6 $
MPG per 1000 lbs of Payload 11.34
F-T (Speed^2/FuelBurn) 14.1 HP
F-T Payload 18.6 kts
MPH To HP: 5.3 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1740 ft

SA00003SE Installation of Model 3500 seaplane floats. Amended 2/3/2006
SA00018SE Fabrication of interchangeable float attachment gear parts. Issued 10/20/1993
SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00096SE Installation of Aercet 206 Cargo Pack manufactured and installed in accordance with Master Drawing List STC Cargo Pod 206 Document 10-10005N-1 Revision B dated );INSERT INTO stc_table VALUES ( August 5 2005 and maintained in accordance with Instructions for Continued Airworthiness A-10033 Revision 0) dated April 20 2006 or later FAA approved revisions. Amended 6/28/2006
SA00124DE Installation of Oilamatic preoiler system. Amended 2/14/2001
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
SA00162SE Installation of telemetry antennas. Reissued 5/28/1997
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
SA00194LA Installation of a Pink Bollworm dispenser system. (U206G S/N U20605393) Issued 5/7/1996
SA00200AT Installation of carbon steel brake discs that have the melonite surface treatment P/N AA-36. Reissued 11/14/1994
SA00209AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-89. Reissued 11/14/1994
SA00210AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-90. Reissued 11/14/1994
SA00213AT Installation of carbon steel brake discs P/N AA-96. Reissued 11/17/1994
SA00214AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-89. Reissued 11/17/1994
SA00238SE Installation of Aviation Development Corporation s sump mounted chip detector Issued 10/31/1995
SA00243BO (2 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (1OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00270WI Installation of fiberglass replacement wing tips. Amended 6/23/2000
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO (PAGE 1 ) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010
SA00295DE Installation of an external infrared imaging system. Amended 4/8/2004
SA00312WI Installation of 15 and 17-gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 61 or65 gallon capacity bladder tank or62 gallon fiberglass fuel tanks. (thru S/N U20604649) Reissued 5/3/2004
SA00332AT Installation of a Teledyne Continental model IO-550F engine and a McCauley model D3A34C401/90DFA-10 propeller with associated spinner. (Landplane only) Reissued and Amended 3/8/1994
SA00393WI Installation of McCauley D3A34C401/90DFA -2 -4 -6 -8 and -10 propeller and associated changes. Reissued 9/22/2005
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00406WI Installation of replacement flap trailing edge bulbs. (R172K XP) Amended 9/9/1999
SA00419NY Installation of cockpit utility light. Reissued 12/31/2002
SA00425DE Installation of model FB-02 Fixed Arm Pilot Arm Rest on R/H side of pilot seat and optional GPS Support Arm System. Amended 6/12/2001
SA00426DE Installation of Model FB-01 Swing Arm Pilot Arm Rest System on R/H side of pilot seat. Amended 6/12/2001
SA00428WI Installation of McMauley D3A34C402/90DFA -2 -4 -6 -8 & -10 propellers and associated changes Reissued 11/1/2011
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00433WI Add a removable panel in the nose gear tunnel for service access. Issued 5/10/1996
SA00462AT Replacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47. Reissued 12/7/1994
SA00465NY Installation of Meterological Measurement System Model A1MMS-10 with optional installation of Telemetry Module Model AIRDAT-9600. Amended 10/28/1998
SA00473SE Installation of Speedbrake Amended 11/7/2003
SA00474LA Installation of 15 U.S. gallon wing tip transfer tanks with option to install wing stringer modification kit SK-1. Issued 12/18/1997
SA00512AT Installation of either a Hartzell model PHC-C3YF-1RF/F7691() PHC-C3YF-1RF/F8468A()-6R PHC-J3YF-1RF/F7691() or PHC-J3YF-1RF/F8468A()-6R and associated spinner assembly. Reissued 2/18/1999
SA00515DE Modification of aircraft fuselage to add 20 belly hole for camera or other aerial applications Amended 12/27/2013
SA00517DE Modification of left middle cabin passenger window per Straight Flight Master Drawing List 0002-2328. Reissued 4/18/2007
SA00628WI Installation of Ameri-King Model AK-450 Emergency Locator transmitter. Issued 2/11/1998
SA00648SE Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. Issued 11/30/1998
SA00671NY Installation of AIRDAT Telemetry module. Amended 10/28/1998
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (4 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00697NY Installation of left-hand and right-hand EDO model 582-3430 floats. Issued 10/28/1997
SA00709LA Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. Reissued 5/14/2002
SA00748WI Certification of a repair kit for the rudder pedal torque tube assembly for stowable rudder pedal installation. Issued 3/4/1999
SA00760SE Installation of glare shield. Reissued 5/20/2010
SA00780SE (PAGE 2) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00796AT Installation of dual-isolator forward engine mount system. Issued 6/29/1995
SA00812CH Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. Reissued 6/30/2006
SA00812NY Installation of Technisonic Industries Limited TFM-138 A and B (does not include TFM-138 s/n 1540 and up TFM-138B s/n 1500 and up). Amended 9/12/2005
SA00819SE Installation of Visual Instruments flap position indicating system. Issued 7/18/2000
SA00843NY Aircraft fuel quantity transmitter replacement-from Stewart Warner Model 390 to Stewart Warner Model 385. Issued 5/28/1998
SA00858SE Install observation window. Amended 11/10/2004
SA00861LA Modification of lower right nose cowl to provide access to exhaust system and turbo charger. Reissued 5/20/2002
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00871SE Cockpit sunvisor installation. Amended 5/11/2010
SA00887SE Installation of vortex generators on the wings tail surfaces and vertical fin in accordance with Micro AeroDynamics Drawing Package MA2146 Revision A dated );INSERT INTO stc_table VALUES ( March 11 2004 and installed in accordance with Installation Manual MA2147 Revision IR dated January 25 2001 (for the 206 series) or MA2196 Revision IR dated March 11 2004 (for the 207 series) or later FAA approved revisions. Amended 4/27/2004
SA00897WI Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Issued 8/11/2000
SA00910WI-D Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. Issued 11/1/2000
SA00954SE (1 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA0096SE Installation of Aercet 206 Cargo Pack manufactured and installed. Amended 6/28/2006
SA01001SE Installation of 12 volt cabin power system for portable electronic devices in accordance with Olympic Aero Services Inc. Master Drawing List OAS-54-0001 Revision G dated September 26 2002 or later FAA approved revision. This system shall be maintained in accordance with Instructions for Continued Airworthiness Document OAS-54-23.1529 Revision B dated August 22 2001 or later FAA approved revision. Reissued 4/9/2012
SA01003SE Addition of performance data to allow reduced RPM rating on takeoff. Incorporation of this rating requires the prior or concurrent incorporation of STC SA00887SE. Amended 2/4/2011
SA01007SE Installation of interior fiberglass panels. Amended 8/1/2005
SA01013WI-D Installation of Bendix/King KMH 880 Multi-Hazard Awareness System/KTA 870 Traffic Advisory System. Issued 10/16/2001
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01070WI-D Installation of Bendix/King KDR 510 VHF Data Link System. Issued 4/9/2002
SA01072SE Installation of standby battery system to facilitate compliance with 14 CFR Part 135.163(f)(2) Issued 5/5/2002
SA01074WI Installation of McFarlane Aviation Flap Roller Assembly Service Kit MCSK100 on various Cessna single-engine aircraft. Cessna Service Bulletin SEB95-3 must be complied with before this STC is installed. Issued 4/22/2002
SA01075WI-D Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System. (206H S/N 20608174 and after T206H S/N T20608362 and after) Issued 5/23/2002
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01079LA Installation of Accessory Power Receptable in accordance with FAA Approved Master Drawing List Document No. 206-APR-100 Rev IR dtd 8/15/00 or later FAA approved revision. Reissued 3/2/2001
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01105WI-D (1 OF 2) Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Amended 5/31/2007
SA01107SE RMD Aircraft Lighting high intensity discharge wingtip light manufactured Amended 4/2/2003
SA01118WI Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 Amended 11/30/2013
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01152WI-D Installation of the Bendix/King KT 73 Mode S Transponder with Traffic Information Service (TIS) );INSERT INTO stc_table VALUES ( REQUIRED DATA: 1. Master Drawing List 159-08287-0001 Revision A dated 01-09-03. 2. Airplane Flight Manual Supplement 006-10309-0000 Revision - dated 3-14-03. );INSERT INTO stc_table VALUES ( Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Issued 3/14/2003
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01170NY Installation of NPX138N-XXX FM Transceiver. Amended 1/17/2007
SA01185CH Installation of Wipaire Model 3450 amphibian/seaplane floats Hartzell Propeller model HC-F3YR-1RF/F8468A-2R and Parts Kit No 12D1-7330. Amended 8/7/2009
SA01202LA Installation of Becker Avionics SAR DF-517 Search and Rescue Direction Finding System Reissued 2/13/2012
SA01204LA Installation of replacement wing tip fairing assembly. Issued 10/3/2001
SA01205WI-D (1 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01224AT Installation of wheel hub cabs with valve stem access door. Amended 4/17/1998
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01257SE Installation of Aerocet Model 3400 floats Amended 8/28/2003
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01292SE Installation of one piece windshield Issued 11/3/2003
SA01300AT Installation of a Teledyne Continental Motors model IO-550-F engine and either a McCauley or Hartzell various models 3-blade propeller. Reissued 2/18/1999
SA01328LA Modification of right hand side door to provide an openable window. Reissued 3/30/2005
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01380CH Installation of wing fuel tank quick valve drains. Issued 1/25/2001
SA01410LA Modification of right-hand window to provide an openable window. Amended 10/15/2003
SA01435DE Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine.  Reissued 5/25/2011
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01436SE (1 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004
SA01456NY Installation of Technisonic Industries Ltd OSAT-100 Airborne Position/Data Communicator. Issued 1/31/2002
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01539AT-D Installation of Remote Mounted Oil Cooler. Amended 3/25/2010
SA01552WI Installation of Supplemental Audio System including #2 GMA 1347 Audio Panel Amended 11/12/2009
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01598CH Replace existing propeller with Hartzell Propeller model PHC-G3YF-1RF/F8468A-2R or -6R. Amended 11/17/2009
SA01604SE Installation of the full feathering 5-blade constant speed MTV-5-1-E-C-F/CF220-54 propeller installed and maintained. Issued 9/29/2005
SA01606CH Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. Amended 4/16/2010
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01688SE Installation of a revised shoulder harness restraint system and new rear cabin headliner.  Amended 4/9/2009
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (2 OF 5) Installation of an antenna Amended 2/15/2007
SA01700LA Installation of AMSAFE Aviation Inflatable Restraint (AAIR) system. Issued 12/3/2004
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01721SE ONE-ONLY STC: Installation of skydiving provisions in accordance with Skydiving Provisions  Issued 11/27/2006
SA01734SE (PG 4) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01743SE Installation of forward left and forward right cabin door step assemblies and installation of aft right cargo door cabin step in. Amended 5/8/2007
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01777AT Installation of either a McCauley model D3A34C401/90DFA-10 or D3A34C402/90DFA-10 propeller and associated spinner assembly. Reissued 2/18/1999
SA01777SE Installation of interior fiberglass extended bag compartment Reissued 5/20/2010
SA01782LA Installation of 130 ampere alternator Issued 4/15/2005
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01878SE Installation of Rolls-Royce 250-B17F/2 series engine with a Hartzell Model HC-B3TF-7A/T10173FN(K)-11R Propeller.  Issued 10/29/2008
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (1 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01951NY-D Installation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system. Reissued 3/18/2005
SA01984SE Installation of AeroAcoustics Aircraft Systems (AASI) Payload Extender XL gross weight increase system Amended 12/23/2009
SA01985SE Installation of new rear observation seat.  Amended 8/24/2012
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02003AK Fabrication and installation of main gear gravel deflector kit no. GD6-200. Amended 9/3/1999
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 2) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008
SA02041AK Fabrication and installation of exhaust deflector assembly(P/N 3238). Issued 5/17/1996
SA02048SE Fabrication of Stene Aviation Inc. Wing Tip Part Numbers SA-1223000-7 and SA-1223000-8  Issued 2/2/2010
SA02049SE Fabrication of Stene Aviation Inc. Wing Tip Part Numbers SA-0523565-29 and SA-0523565-30 Issued 2/2/2010
SA02064AK Install McCauley D3A34C404 propeller. Issued 11/13/1996
SA02069AK Fabrication and Installation of the Airglas PA32-206LA Nose Fork equipped with Goodyear 8.50 x 6 tires. Amended 6/5/2006
SA02072AK Installation of hourmeter airspeed switch. Amended 11/14/1997
SA02076AK Fabrication of left hand and right hand exhaust stack assemblies(P/N LEES1250256-3 and LEES1250257-3). Issued 5/30/1997
SA02088AK Fabrication and installation of a boarding ladder equipped with EDO Float Model 582-3430. Issued 9/9/1997
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02167AK-D Fabrication and installation of single place folding seats p/n FS206-100 and Floor Structure Kit No. AFS-206-100. Issued 11/22/2000
SA02169NY Installation of Cessna 206/207 Secondary Heat Muffler manufactured to Acorn Welding Manufacturing Control Process NAM-0301. Issued 10/31/2005
SA02173AK-D Fabrication and installation of Aero Twin Inc. single place folding seats P/N FS206-100 and Floor Structure Kit No. AFS-206-200. Issued 3/29/2001
SA02198AK-D Fabrication and installation of remote nose gear strut service port. Issued 11/5/2002
SA02203AK (PAGE 2)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02217AK (2 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02248LA Installation of Sensor Pod and wiring for a passenger operated monitoring system Reissued 1/30/2014
SA02257AT Installation of a BAE-14/28 Air Driven Alternator. Issued 12/19/2000
SA02262SE Installation of split seam wing strut cuff as replacement parts for the strut fairings Issued 3/8/2013
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02266AK Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401. Reissued 6/19/2006
SA02268CH (PAGE 2) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 3) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02269SE Increased performance based on prerequisite supplemental type certificates (STC). This supplemental type certificate does not make physical modifications to the aircraft. Issued 4/1/2013
SA02271SE Fabrication of Soloy wing mounted LED landing and taxi light kits Reissued 4/9/2013
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
SA02277AT Installation of a passenger seat. STC SA1335SO is a required part of this STC. Issued 2/21/2001
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02289SE Installation of a Supplemental Lighting System Issued 8/20/2013
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02294CH Installation of an MT-Propeller MTV-(9 or 15)-D/205-58 or MTV-(9 or 15)-D/210-58 and spinner assembly Reissued 12/17/2008
SA02298AK Installation of Horizontal Stabilizer Screw-on Leading Edge on Cessna 206 and 207.  Issued 9/7/2007
SA02328LA Installation of engine exhaust pipe extensions.  Amended 12/12/2012
SA02332AK Installation of a fixed mounted Forward.Vision Enhanced Vision System (EVS) Models 100/600 to include an under-wing conformal fairing with sensor and a glareshield mounted dedicated display monitor Issued 6/24/2009
SA02359AK-D Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp  Issued 11/6/2009
SA02411CH Installation of the Aero Vent Cabin Ventilation System. Issued 7/25/2008
SA02415CH Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. Issued 5/10/2007
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02507AT-D Installation of Teledyne Continental Motors IO-550-N engine and Hartzell PHC-J3YF-1RF/F8068( ) propeller. Issued 6/14/2002
SA02511CH Installation of Saf-Air Products fuel quick drain backing plate C187 and fuel drain valve B187 Issued 1/7/2008
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02655AT (1 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02725CH Installation of North American Surveillance Systems Strut Mount and Optional Cloud Cap Technologies TASE / TASE Dou Gimbals  Issued 5/29/2009
SA02735CH Installation of Hartzell Propeller Model (P)HC-()3YF-1RF/8068(B K)() and /or (P)HC-()3YF-1RF/7693DF(B K)() 3 bladed metal propeller Issued 8/14/2009
SA02738CH (PAGE 5) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02748AT Installation of Wescam Wing Mounted Forward Looking Infrared Camera System Monitor Stand and Microwave Downlink Antenna System in accordance with AirScan Inc. Master Drawing List AS206000 Rev. IR dated 3/25/04 or later FAA approved revision. Reissued 6/28/2010
SA02752CH-D Installation of the Hartzell propeller models (P)HC-C3YF-1RF/F8468AR (P)HC-C3YF-1RF/F8468A-2R and (P)HC-C3YF-1RF/F8468A-4R. Issued 8/26/2009
SA02768CH Installation of Teledyne Continental Motors IO-520-A & -F (as modified by STC SE03704AT) or IO-550 F (as modified by STC SE03705AT) and Hartzell Propeller (P)HC-J3YF-1RF/F8468(B K) 3 bladed metal propeller Amended 8/9/2011
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02809CH Installation of Aerospace Welding Stainless Steel Exhaust System Issued 2/18/2010
SA02846NY Installation of 5-blade propeller MTV-D-C-F-R(A)/CFR210-56 propeller Issued 9/16/2010
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03122AT-D Installation of a Rear Camera Window Amended 7/31/2008
SA03123AT-D Installation of Cabin Skylights Amended 7/2/2008
SA03134NY Installation of Low Noise Silencer Kit CT206H-606570 Exhaust Silencer with Extension  Issued 8/21/2012
SA03147AT-D Installation of an Autopilot Aileron Disconnect System. Amended 7/2/2008
SA03148AT-D Installation of Right Wing Landing and Taxi Lights. Amended 7/2/2008
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03150AT-D Installation of a Wulfsberg P-2000 FM radio. Amended 7/2/2008
SA03162CH Installation of Hartzell HC-F3YR-1ARF/F8068(B K) propeller Issued 5/4/2013
SA03229AT-D Installation of Right Wing HID Landing and Incandescent Taxi Lights. Amended 7/2/2008
SA03286CH Install an electronic engine ignition system Issued 1/13/2014
SA09377AC-D Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems Model ST-829-20/30. Amended 10/6/1998
SA09378AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-830. Issued 9/8/1998
SA09380AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-832. Issued 9/8/1998
SA09389AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-837-20/30. Amended 5/7/1999
SA09391AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-838. Issued 9/17/1998
SA09403AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-556 with optional Autotrim System. Amended 3/13/2001
SA09404AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-837-20/30. Issued 5/7/1999
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09576SC Installation of a Airborne R-134a air conditioning system. Reissued 5/30/2012
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA10010SC Installation of TCM IO-550 engine. Issued 10/24/2002
SA1005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Issued 7/23/2002
SA10126SC (1 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA10144SC Installation of an engine driven vapor cycle air conditioning system Reissued 5/17/2013
SA1021SW Flap on switch on control wheel. Reissued 9/20/1977
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1037CE Installation of 26-gallon auxiliary fuel tank in baggage compartment. Reissued 3/18/1988
SA10615SC-D Installation of Hartzell PHC-(C or J) 3YF-1RF/F7693F(B)+2 propeller Reissued 9/11/2008
SA1069CE Enlargement of factory installed camera hole and installation of a view finder hole. Reissued 6/23/2006
SA1070CE Installation of 50-gallon auxiliary fuel tank in aft cabin area. Limited to installation on Cessna model TU206F serial number U20602485. Reissued 6/23/2006
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA10951SC Installation of a WESCAM MX-15 FLIR System in accordance with Index List HDT206-00-0007 Revision IR dated July 15 2009 or later FAA approved revision. Airplane Flight Manual Supplement HDD08-0083 Revision IR dated July 10 2009 or later FAA approved revision is required.  Issued 7/23/2009
SA1107GL Modify the EDO Air Model 696-3500 float brake system. Amended 6/23/1995
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1228GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1255WE Remove left hand cabin door to permit parachute jumping operation Issued 7/18/1966
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1273NW Installation of an outward-opening pilot side door Issued 7/6/1981
SA1284SO Installation of seats and seat tracks. Issued 10/19/1981
SA1301GL Replace Cessna fuel cell drain valve assembly P/N 84C with Safe Air Repair P/N SAR-2. Reissued 4/22/2005
SA1310SO Replacement and relocation of the Pre-select flap switch with a continuous input flap switch which allows simultaneous pilot operation of the throttle and flap controls. Amended 10/7/2002
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA1335SO Installation of seat tracks. Issued 5/7/1982
SA1353CE Chrome-plated brake disc installation. Issued 8/22/1977
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA1381SO Installation of engine fire detector system. Amended 11/16/1982
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1421NM-S An increase in gross weight is approved from 3500 pounds to 3600 pounds when equipped with EDO Model 582-3430 seaplane floats. Reissued 7/31/1998
SA1430SW Mitchell automatic flight system AK350 consisting of Century I autopilot with optional omni tracker. Reissued 7/10/1984
SA1431SW Mitchell automatic flight system AK368 consisting of Century III autopilot with optional automatic electric pitch trim radio and glide slope couplers. Reissued 7/10/1984
SA1449SW Mitchell automatic flight system AK369 consisting of Century II autopilot with optional radio coupler. Reissued 7/10/1984
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1470GL Installation of right front cabin door. Issued 4/17/1990
SA1474SW Installation of MASA 1223000-7 and -8 wing tip. Reissued 9/5/1979
SA1478WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 1/24/2013
SA1480CE Installation of King KFC200 automatic flight control system two axis with or without flight director. Reissued 2/28/2000
SA1482GL Installation of Teledyne Continental Motors IO-550-F engine McCauley D3A34C401/90DFA-10 propeller(U206E F G S/N U20601445 - U20604074) or D3A34C402/90DFA-10(for U206F S/N U20602200 - U20604074 and U206G S/N U20602200 and up) and assoc changes. Amended 4/19/1994
SA1483GL Installation of Wipaire Model 4000 amphibian or seaplane floats. Amended 10/1/1998
SA149SW Automatic pilot AK120 AK120E AK102E-3 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA1506SO Installation of seats. Issued 10/5/1983
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1513WE Installation of flap actuated aileron droop system recontoured wing leading edge and flap actuated elevator trim system. (206 EXCEPT TU206F U206F U206E U206G TU206G) Amended 3/14/2006
SA1515GL Install aero fabricators shoulder harness and seat belt assembly per Aero fabricators Installation Instructions AF-28 No revision dated March 2 1990 or later FAA Approved Revisions. Amended 1/10/2005
SA1569CE-D Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system and optional KAS 297B vertical speed and altitude selector. Reissued 2/28/2000
SA1572SW Mitchell automatic flight system AK405 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/13/1984
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1580NM Installation of replacement exhaust heat exchanger. Amended 5/22/1986
SA1588GL Install Teledyne Continental Motors engine model TSIO-520-M with McCauley propeller model D3A34C402/90DFA-10 and other associated components. Issued 4/25/1991
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA1591NM Installation of inflight roll-up door and external assit handles when fabricated and installed. Reissued 11/4/2011
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1643GL Installation of V-type or Y-type shoulder harness. (182 SERIES EXCEPT R182 & TR182) Amended 8/31/1995
SA1686WE Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. Amended 10/17/2002
SA172NW Installation of drooped type wing tips. Issued 4/14/1975
SA1807SO Installation of Appalachian Acces. stainless steel brake discs P/N 73-47. Amended 4/9/1987
SA1817NM Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4 1983 together with their FAA sealed Installation Instructions dated September 20 1982 or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6 1982 LAS 1013 dated October 5 1982 and LAS 1014 dated October 6 1982 or later FAA approved sealed revisions. Reissued 1/23/2004
SA182CH Installation of removable Telonics telemetry antennas. Reissued 5/4/1994
SA1845SW Mitchell automatic flight system AK469 consisting of Century I auto- pilot with optional omni tracker. Reissued 7/16/1984
SA1846SW Installation of Mitchell automatic flight system Model AK471 consisting of Century III autopilot autopilot with optional command/ electronic pitch trim optional radio coupler and optional glide slope coupler. Reissued 7/16/1984
SA186RM Installation of wing strut mounted camera pod and/or viewfinder. Reissued 8/7/1987
SA1870WE Installation of Brittain Model NAV-2B Flight Control System Reissued 6/14/2013
SA1887SW Installation of Mitchell automatic flight system Model AK470 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/16/1984
SA1893WE Installation of Brittain Industries Inc. Model B-5 NAV-2B or B2C Flight Control System Reissued 2/6/2013
SA18GL Installation of Wipline Model 3730 amphibious floats. Install Wipline Model 3700 3800 or 3900 seaplane floats. (TU206G SEAPLANE CONFIGURATION ONLY) Amended 4/8/1991
SA1939CE Increase in gross weight from3 300 lbs. to 3 600 lbs. Issued 2/4/1984
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2106NM Installation of Precise Flight Speedbrake System. Amended 11/7/2003
SA2123NM Installation of Lycoming TIO-540-J2BD engine AiResearch Model THO8A60 Turbocharger Hartzell HC-C3YR-1RF/F7854 (Three-Blade) propeller Hartzell Model F4-13 Governor and associated Systems. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( NOTE: This approval is also extended to airplanes of these models that have incorporated the aileron droop system per STC SA1513WE and Flint Aero Wing Tip Tanks per STC SA43689WE. Reissued 12/22/2008
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2163NM Installation of the Precise Flight Inc. Stand-By Vacuum System (SVS) in accordance with Installation Report 08074 Revision - dated January 7 2000 or later FAA approved revision. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( NOTE: As a prerequisite to this change the engine must be modified in accordance with Precise Flight Inc. STC No. SE1780NM dated April 21 2000 or later FAA approved revision. Also modified aircraft must be equipped with a vacuum indicator. Amended 11/7/2003
SA2164WE Installation of Edo Model FD-3500A(TSO C-27-2) amphibious floats. Amended 2/15/2001
SA2172SO Replacement of Cleveland brake discs P/N 164-15A or 164-115A with Appalachian stainless steel brake discs P/N 75-15A. Issued 9/25/1987
SA2256WE Installation of leading edge cuff on each wing. Reissued 1/21/2010
SA2302NM Installation of Schneider Model SWS-4000C-15 SWS-4000C-19 or Model SWS-4000C-23 main wheel skis. Issued 11/25/1983
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)


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