Cessna TurboCharged 207

Number of Active Aircraft: 76 Active- Map

Description:

Years Produced: 1968-86 In 1968 they introduced the 207 turbo charged version. The same as the 207 series but with a turbo charged engine making for better performance at high altitude and the engine also increased power by 10 hp down low. In 1979 the A model was introduced which was certified for 8 seats.

Wikipedia Cessna 206 reference:

408
Fuel Cost ($):
General Stats:
Seat Capacity: 8
Empty Weight: 2254 lbs
Max Weight 3800 lbs
Useful Load: 1546 lbs
Engine Name Continental TSIO-520-G
Engine Number 1
Horsepower 310 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 26000 ft
Max Fuel 61 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 161 kts
GPH (75% BHP): 15.8
MPG (75% BHP) 10.2
Range (75% BHP): 521 nm
Fuel Cost Per Seat Mile 0.07 $
Fuel Cost Per Hour 94.8 $
MPG per 1000 lbs of Payload 15.75
F-T (Speed^2/FuelBurn) 16.4 HP
F-T Payload 25.4 kts
MPH To HP: 5.2 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1860 ft

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
SA00123DE Installation of Oilamatic preoiler system. Issued 9/6/1994
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
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00173AT Installation of a Teledyne Continental model IO-550F engine and various Hartzell and McCauley propellers. Reissued 2/18/1999
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00200AT Installation of carbon steel brake discs that have the melonite surface treatment P/N AA-36. Reissued 11/14/1994
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
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
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
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00636AT Installation of various Hartzell propellers. Issued 1/13/1995
SA00648SE Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. Issued 11/30/1998
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (3 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00680SE (4 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
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
SA00709SE Installation of replacement control surface skin panels. Issued 6/28/1999
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
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
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
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
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
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
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
SA01119CH Replace Cessna Sun visor assemblies with Aircraft Recycled Flying controls tinted Sun Visor Assemblies Reissued 3/20/2006
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
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
SA01206SE Fabrication of Robair middle gear leg fairing assembly Issued 4/18/2003
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
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
SA01283WI Installation of McCauley D3A34C401/90DFA-6 -8 and -10 Propeller on Cessna Model 207 Series airplanes equipped with TCM IO-520F IO-550F TSIO-520-G and TSIO-520-M engines. Reissued 9/22/2005
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
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
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
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
SA01657SE Fabrication of Robair main landing gear lower support fairing . Issued 3/14/2006
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
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
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
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
SA01744SE Installation of forward left and forward right cabin door step assemblies and installation of aft right cargo door cabin step assembly. Issued 4/19/2007
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01777SE Installation of interior fiberglass extended bag compartment Reissued 5/20/2010
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
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
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
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
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
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
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
SA02169NY Installation of Cessna 206/207 Secondary Heat Muffler manufactured to Acorn Welding Manufacturing Control Process NAM-0301. Issued 10/31/2005
SA02195NY Installation of STOL Kit. Descriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Cessna Model 207 Serial Number 207007061. . Reissued 1/24/2006
SA02202AK-D Fabrication and installation of remote nose gear strut service port. Issued 2/17/2003
SA02203AK (PAGE 3)  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
SA02257AT Installation of a BAE-14/28 Air Driven Alternator. Issued 12/19/2000
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
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
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
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
SA02415CH Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. Issued 5/10/2007
SA02417AK Installation of a Continental IO-520-F engine Issued 10/21/2013
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
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
SA02547AT (PG 1) Installation of a Voice Alert System. Amended 8/28/2007
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
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
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
SA02774CH Installation of a mounting device for a Class II Electronic Flight Bag on the instrument panel Amended 9/11/2011
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
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
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03286CH Install an electronic engine ignition system Issued 1/13/2014
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA10011SC 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
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10615SC-D Installation of Hartzell PHC-(C or J) 3YF-1RF/F7693F(B)+2 propeller Reissued 9/11/2008
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1229GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1302GL Replace Cessna fuel cell drain valve assembly P/N 84C with Safe Air Repair P/N SAR-2. Reissued 4/22/2005
SA1328CE Installation of leading edge cuffs droop tips and staff fences. Amended 9/30/1982
SA1354CE Chrome-plated brake disc installation. Issued 8/19/1977
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA1402SW Mitchell automatic flight system AK357 consisting of Century II autopilot with optional radio coupler. Reissued 7/10/1984
SA1403SW Mitchell automatic flight system model AK356 consisting of Century I autopilot with optional omni tracker. Reissued 7/10/1984
SA1404SW Mitchell automatic flight system Model AK361 consisting of command/electric trim system. Reissued 7/10/1984
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1474SW Installation of MASA 1223000-7 and -8 wing tip. Reissued 9/5/1979
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1516GL Install shoulder harness and seat belt assembly. Amended 12/20/2004
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1594NM Installation of replacement exhaust heat exchanger. Amended 5/22/1986
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1822NM 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
SA187RM Installation of wing strut mounted camera pod and/or viewfinder. Reissued 8/7/1987
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2106NM Installation of Precise Flight Speedbrake System. Amended 11/7/2003
SA2121WE Installation of recontoured wing leading edge drooped ailerons in flaps down mode stall fences and elevator trim spring. Reissued 7/21/2005
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2173SO 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
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2256WE Installation of leading edge cuff on each wing. Reissued 1/21/2010
SA2327WE Installation of recontoured wing leading edge stall fences and wing tips. Reissued 7/21/2005
SA2330NM Installation of F. Atlee Dodge filler neck adapter. (T207A UP TO S/N 20700788) Issued 2/12/1986
SA2346SO Replacement of Cleveland brake discs P/N 164-36 or 164-136 with Appalachian Accessories stainless steel brake discs P/N 75-36. Issued 6/3/1988
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2379CE Installation of fuel caps. Reissued 5/3/2004
SA2381NM Installation of Knots 2U Ltd Wheel and Body Fairings Amended 8/19/2008
SA2382NM Installation of Aileron and Flap Gap Seals. Amended 7/15/2003
SA2390NM Installation of Turboplus Intercooler System No. 15000 or 15000-AD. Reissued 10/15/2007
SA2438CE Installation of 62 gallon capacity long range fiberglass fuel tanks in place of original bladder fuel tanks. Reissued 5/3/2004
SA2523CE Installation of replacement wing tips. Issued 7/31/1989
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2577CE Installation of main fuel cell bladders as replacements for original bladders. (T210 SERIES SPECIFIC SERIAL NUMBERS AFFECTED) Reissued 7/31/2002
SA2586NM (PAGE 2) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2676WE Installation of larger fuel containing wing tips. Reissued 2/25/2000
SA2681NM Installation of a wastegate actuator drain line on Continental TSIO-520 series engine on Cessna 206 207 and 210 series aircraft. Amended 11/1/1998
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2704NM Installation of replacement exhaust system riser. Issued 3/28/1985
SA2768NM Installation of replacement left exhaust heat exchanger unit. (T207A THRU 1984 MODEL YEAR) Issued 1/12/1987
SA2809SW Install Hoskins CFS-1000 electronic fuel flow metering system. Reissued 1/30/1998
SA2819CE The use of 20 degree flaps for take-off with the gross weight reduced to 3600 lbs. Amended 6/8/1992
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2856SW Leading edge cuffs stall fences aileron seals wing tips. Reissued 6/6/1980
SA2922NM Modify Cessna fuel bladder cell quick drain P/N 84C. Amended 2/22/1996
SA2960NM Install stay put (seat position locking device). Amended 3/14/1986
SA3000SO Installation of Appalachian stainless steel brake discs No. 75-15A. Reissued 9/29/1995
SA300CE Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) Amended 5/14/1992
SA3318NM Installation of a Venting fuel cap and restricting adapter assembly. Amended 6/23/1988
SA3322NM Installation of the Soloy turbine pac (Allison 250-C20S engine). Reissued 12/2/2004
SA3347NM Use of the Union Aviation portable hand operated rudder and brake model C. Amended 9/30/1987
SA3374NM Installation of Soloy turbine pac exhaust heat exchanger and related changes. Amended 12/2/2004
SA3427WE Installation of tail flood light on horizontal stabilizer. Reissued 2/28/1980
SA3617SW Installation of PK Model C4000 or D4000A floats. Amended 10/14/1986
SA3659SW Installation of Jetton Alert II alarm system. Reissued 3/30/2007
SA3695NM Cockpit Sun Visor installation in accordance with FAA approved Rosen Drawing List Number RCS-00DL dated December 17 1986 or later FAA approved revisions. Reissued 3/24/2003
SA3781NM Installation of engine induction air intercooler. Reissued 9/6/1996
SA3853SW Install three auxiliary bladder type fuel tanks in each wing. Reissued 7/21/2005
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA398NE Installation of Auto-Vac-2 manifold vacuum system per certain engine STC s. Amended 8/15/1990
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4133NM Installation of an eighth seat. Amended 11/10/2004
SA4166NM Installation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506. Issued 1/25/1988
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4320NM Installation of an oil filter filter base and mounting plate on the firewalls of those airplanes listed on AML No. SA4320NM that are equipped with an FAA approved Continental Model IO-520 engine installation which has been modified by the installation of an external mounted full flow oil adapter and spin-on oil filter Reissued 7/30/1993
SA4579SW S-TEC System 60 two axis automatic flight guidance system ST-067 with optional autotrim system and flight director steering horizon. Issued 1/7/1982
SA4600SW Installation of an auxiliary engine driven vacuum pump system. Reissued 10/8/2001
SA4605NM Installation of main gear gravel deflectors Issued 3/3/1989
SA4623NM Fabrication and installation of TD7-100 cargo tie down kit. Issued 9/15/1989
SA4631SW S-TEC System 60 single axis automatic flight guidance system Model ST-066 (28 volt). Issued 3/22/1982
SA4632SW S-TEC System 60 pitch stabilization system Model ST-068 with optional autotrim system. Issued 3/22/1982
SA4646SW S-TEC System 60 single axis automatic flight guidance system ST-069 (14 volt system). Issued 4/12/1982
SA4647SW S-TEC System 60 two axis automatic flight guidance system Model ST-070 with optional autotrim system optional flight director/ steering horizon(14 volt system). Issued 4/13/1982
SA4715NM Installation of the Soloy bleed air heater and related changes. Amended 12/2/2004
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA4734SW S-TEC System 60 pitch stabilization Model ST-071 with optional autotrim system (14 volt). Issued 8/3/1982
SA5012NM Installation of a modified exhaust system. Amended 1/12/1994
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5214SW-D S-TEC System 60 pitch stabilization system with optional automatic electric trim system. Issued 10/5/1983
SA5232SW-D S-TEC System 40/50 single and two axis automatic flight guidance system ST-211-40/50. Issued 11/2/1983
SA5259SW-D S-TEC System 40/50 single and two axis automatic flight guidance system ST-210-40/50. Amended 2/13/1985
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5727SW-D Installation of SDI Hoskins or ALCOR tru-flow digital fuel flow system. Reissued 8/27/2008
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (2 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA6020NM Installation of an electronic digital engine tachometer Model P-1000. Issued 5/18/1993
SA615EA (PAGE 1) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA696AL For model 207 and 207A installation of Hartzell Propeller HC-C3YF-1RF/F8468A-8R and Hartzell Spinner Model A2295-1() or for model T207 and T207A installation of Hartzell Propeller PHC-C3YF-1RF/F8468A-6R and Hartzell Spinner Model A2295-1(). (207A S/N 20 700363--20700482) Amended 2/27/2006
SA7145SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-067 with optional automatic electric trim system. Issued 4/6/1987
SA7146SW-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-395. Issued 4/6/1987
SA7147SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-070. Issued 4/13/1987
SA7154SW-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-396. Issued 7/15/1987
SA71GL Installation of air filters Reissued 6/20/2000
SA728NW Installation of vented fuel cap. Amended 10/10/1979
SA7438SW Installation of a camera port on the fuselage center line aft of the main landing gear bulkhead. Amended 8/14/2012
SA7838SW Installation of replacement extended range bladder fuel cells. Reissued 7/21/2005
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA8008SW Installation of Zeftronics alternator control units P/N s R25101 (27.7V systems) or R25102 (28.8V systems). Reissued 5/12/1998
SA8018SW Installation of Zeftronics alternator controller unit P/N R15100 (Product configuration file ZOCPCF) or P/N R15V00 )Product configuration file (ZODPCF). Amended 1/6/1992
SA8031SW Installation of Zeftronics alternator controller unit P/N R15100 or R15V00. Amended 1/6/1994
SA8032SW Installation of Zeftronics over-voltage sensor unit P/N V11100 (Product configuration file ZOLPCF). Reissued 5/12/1998
SA8033SW Installation of Zeftronics over-voltage sensor unit V11100 (Product configuration file ZOLPCF). Reissued 5/12/1998
SA8150SW Installation of VENTUBE pilot/co-pilot overhead fresh air valves. (195 SERIES LC-126A LC-126B LC-126C) Reissued 12/29/2006
SA839GL Installation of safety belt extenders. Reissued 10/15/1986
SA8427SW Installation of an R25400 alternator control unit on aircraft. Reissued 5/12/1998
SA8432SW Installation of V25101 overvoltage sensor. Reissued 5/12/1998
SA8922SW Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) Issued 7/21/1994
SA917EA Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). Reissued 6/4/2007
SA995SW Increase wing leading edge radius wing tip fairings and landing light lens. Reissued 4/27/1984
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01494LA (PG 1) Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. Reissued 8/30/2011
ST01540AT-D Installation of remote mounted oil cooler Issued 8/19/1999
ST01700NY (1 OF 2) Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator. Issued 7/8/2003
ST02307CH Installation of Rudder Pedal Extensions. Amended 10/13/2006
ST02547AT (1 OF 2) Installation of a voice alert system. Amended 5/13/2003
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
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
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
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
Limitations
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)