Cessna 210 F

Number of Active Aircraft: NA Active- Map

Description:

Years Produced: 1966 The F model was the first year a turbo charged option was offered. 300 of the F model were built.

Wikipedia Cessna 210 reference:

217
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1865 lbs
Max Weight 3300 lbs
Useful Load: 1435 lbs
Engine Name Continental IO-520-A
Engine Number 1
Horsepower 285 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 19900 ft
Max Fuel 65 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 165 kts
GPH (75% BHP): 14
MPG (75% BHP) 11.8
Range (75% BHP): 660 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 84 $
MPG per 1000 lbs of Payload 16.91
F-T (Speed^2/FuelBurn) 19.4 HP
F-T Payload 27.8 kts
MPH To HP: 5.8 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1265 ft

SA00030NY Installation of freon-type electric motor driven air conditioning system. Issued 8/18/1993
SA00032WI Installation of flap and aileron gap seals. Issued 2/11/1993
SA00033SE Installation of modified exhause system Issued 11/2/1993
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
SA00147AT Installation of Type A sun visor. Amended 7/28/1993
SA00150BO Installation of Continental TSIO-520-R engine McCauley D3A34C402/90DFA10 propeller. Approved for installation on serial number 21063886 ONLY. Issued 6/18/2002
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
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
SA00172WI Installation of TKS anti-icing system components with placard stating Flight into known icing conditions is prohibited.  Amended 7/8/2008
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00206AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00207WI Installation of 18 gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 64 gallon capacity bladder tank or 62 gallon fiberglass fuel tanks. Reissued 5/3/2004
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
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
SA00272WI Replacement of hydraulic system pressure switch. Reissued 11/8/2007
SA00274AT Installation of a Teledyne Continental model IO-550L engine and a McCauley model D3A34C402/90DFA-10 or a Hartzell model PHC-J3FY-1RF/F7691 propeller with associated spinner. Amended 1/14/2009
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
SA00306DE Installation of an external infrared imaging system. Amended 10/11/2007
SA00367DE Installation of an Oilamatic Preoiler system. Issued 1/20/1999
SA00368DE Installation of an Aircraft Noise Control System. Reissued 1/28/2000
SA00393SE Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. Issued 12/6/1996
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00419NY Installation of cockpit utility light. Reissued 12/31/2002
SA00422WI  Installation of McCauley Propeller Model D3A34C402/90DFA -8 -10 and associated changes. Reissued 9/22/2005
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
SA00426WI Installation of McCauley Propeller Model D3A34C402/90DFA -8 -10 and associated changes. Reissued 9/22/2005
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00455DE Installation of a large vertical left hand side window and/or an optional Del Air One Passenger Observation Rear Seat Assembly. Issued 7/20/2001
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
SA00473SE Installation of Speedbrake Amended 11/7/2003
SA00540DE Modification to right hand cabin door and step installation for skydiving operations.  Issued 2/23/2004
SA00553AT Installation of either a Hartzell model PHC-J3YF-1RF/F7691() or PHC-J3YF-1RF/F8468A() -6R propeller and associated spinner assembly in accordance either Bonaire Aviation Company Propeller Installation Instructions in Cessna 201 Series Aircraft (Continental IO-520L Powered) Reissued 5/10/2011
SA00560AT Modification of middle seats into a bench seat. (210G S/N 210-58925 only) Issued 9/7/1994
SA00588CH Install Vertical Fin De-Ice Boot. Issued 12/11/1996
SA00606NY Installation of O & N Aircraft Modifications low fuel warning device. Amended 12/15/1997
SA00631WI Installation of additional equipment for flight into icing. Amended 4/16/1998
SA00648SE Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. Issued 11/30/1998
SA00669AT Installation of a replacement auxiliary fuel pump. Reissued 3/11/2010
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
SA00695SE Replacement of certain Rotomaster and Rayjay scavenge pumps Amended 2/14/2003
SA00702AT Installation of a Basic Type BAE-14/28 Model 2025 deployable air driven alternator system. Reissued 12/16/2010
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
SA00712CH Installation of Insight Avionics Strike Finder model SF 2000. Reissued 9/4/1997
SA00744AT Installation of Avalex AVR1000R video processing unit (VPU). Issued 4/3/1995
SA00760SE Installation of glare shield. Reissued 5/20/2010
SA00773AT Installation of a Hartzell PHC-J3YF-1RF/F7691( ) Model Propeller and C-4582-(P) Spinner  Amended 11/30/2009
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
SA00819SE Installation of Visual Instruments flap position indicating system. Issued 7/18/2000
SA00846WI Installation of B&C Specialty products BC 425-1 standby alternator. Issued 12/23/1999
SA00855SE Installation of BAS Inc. duel belt shoulder harness with inertia reel in accordance with BAS Report 1002 dated April 1 2000 or later FAA approved revision. Amended 12/2/2010
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
SA00864SE Installation of fiberglass nosebowl. Reissued 5/20/2010
SA00871SE Cockpit sunvisor installation. Amended 5/11/2010
SA00897CH Installation of Domed (Bubble) Window Amended 12/4/2013
SA00897WI Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Issued 8/11/2000
SA00920CH Installation of McCauley Propeller Model D3A36C435/80VEA-0 spinner assembly and C290D3[X]/T35 governor. Reissued 9/23/2005
SA00925WI Installation of MT-Propeller model MTV-14-D/195-30a hydraulic 4-blade constant speed propeller. Reissued 3/20/2007
SA00941SE Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156 Revision IR dated April 18 2001 and Installation Manual MA2157 Revision IR dated July 3 2001 or later FAA approved revision to either of these documents. If more than five vortex generators are damaged or missing the aircraft is not airworthy. Issued 7/17/2001
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
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01032WI Installation of external aerodynamic Vortelator Kit on airplanes Amended 7/11/2008
SA01058SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2165 Revision IR dated February 14 2002 and Installation Manual MA2166 Revision IR dated February 25 2002 or later FAA approved revision of either of these documents. Issued 2/28/2002
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
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
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
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
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
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
SA01192SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2178 Revision IR dated January 17 2003 and Installation Manual MA2179 Revision IR dated February 24 2003 or later FAA approved revision to either of these documents. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( NOTE: If more than five vortex generators are damaged or missing the aircraft is not airworthy. Issued 3/21/2003
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
SA01217SE Installation of Zeiss Aerial Survey Camera System.  Issued 5/19/2003
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
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
SA01323WI Installation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved with a date of April 27 2005 or later. Conformity data for Drawing List 114-1 is derived from Drawing List 114-1 Revision C and STC Issued 4/27/2005
SA01324WI Installation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped FAA approved Issued 4/27/2005
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
SA01362WI-D Installation of Bendix/King KFC 225 Automatic Flight Control System. Issued 12/2/2005
SA01363WI-D Installation of a Roll Disable System for Bendix/King KFC 225 Automatic Flight Control System. Issued 12/2/2005
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
SA01437NY Installation of a 135 amp alternator. Issued 1/2/2002
SA01447LA Installation of Pilot Door Window Lock Pilot Door and Baggage Door Locks.  Issued 4/3/2003
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
SA01574AT Installation of the Inframetrics Model IRTV-445G or the FLIR Systems Inc. Model 2000 Thermal Imaging System (TIS). Amended 2/14/2006
SA01590AT Installation of Composite Spinner. Amended 10/13/2000
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 (1 OF 5) Installation of an antenna Amended 2/15/2007
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
SA01780CH Replacement of certain BFGoodrich pneumatic deicer boots per SMR Technologies Inc. Installation Instructions as listed on AML No. SA01780CH latest FAA approved revision. Issued 3/5/2003
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
SA01951NY-D Installation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system. Reissued 3/18/2005
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA01995SE ONE-ONLY: Pilot Operating Handbook revision to provide loading and tie down instructions for cargo operations Issued 6/30/2009
SA01997SE Pilot Operating Handbook revision to provide loading and tie down instructions for cargo operations. Issued 6/30/2009
SA02007NY Installation of SMR Technologies pneumatic deicer models. Issued 10/6/2004
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
SA02029AT-D Installation of Teledyne Continental IO-550-P engine and Hartzell PHC-J3YF-1RF/F7691( ) propeller. Issued 5/26/2000
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
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
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
SA02203AK (PAGE 1) 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
SA02246CH-D Installation of a Hartzell HC-C2YF-1BF/F8468A-2 propeller and C-3568-(P) spinner.  Issued 3/13/2006
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
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
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
SA02283LA Installation of Century Model 2000 Autopilot. Issued 1/5/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (1 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
SA02319CH-D Installation of a Hartzell HC-J3YF-1RF/F7691+2 propeller and C-4582-(P) spinner. Amended 2/6/2009
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
SA02422AT-D Installation of a Stainless Steel Exhaust System Amended 4/23/2010
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02492AT Installation of FLIR Systems Inc. Model UM LE Camera System. STC limited to serial number 21061058 ONLY. Reissued 1/8/2007
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 4) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
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
SA02918CH Replace original Teledyne Continental Motors (TCM) TSIO-520 engine with TCM IO-550-P model aircraft engine turbo normalized not to exceed the rating of 310 BHP Maximum Continuous Power for both the aircraft engine and propellers in accordance with Vitatoe Aviation Installation Instructions report V0701-3 Rev. A dated May 20 2011 or later approved revision. Issued 6/2/2011
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
SA03141AT Installation of Teledyne Continental Motors Model IO-550-L engine and McCauley Model D3A34C402/90DFA-10 or a Hartzell Model PHC-J3YF-1RF/F7691 propeller with associated spinner Amended 1/14/2009
SA03148NY ( PAGE 1 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
SA09010AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-589 with optional autotrim system. Amended 6/1/2001
SA09140AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-621 with Optional Autotrim System. Amended 5/3/1996
SA09232AC-D Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-687-20/30. Issued 5/30/1997
SA09234AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-688. Issued 6/11/1997
SA09293AC-D Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System Model ST-717 with Optional Autotrim System. Amended 8/30/2001
SA09314AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-755-20/30. Issued 12/10/1997
SA09315AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-756. Issued 12/15/1997
SA09340AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-770-20/30. Issued 2/11/1998
SA09341AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-771. Issued 2/16/1998
SA09381AC-D Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems model ST-814-20/30. Amended 12/12/2001
SA09383AC-D Installation of S-TEC system 30 alt altitude hold system model ST-815. Amended 2/1/2002
SA09399AC-D Installation of S-TEC Manual Trim System Model ST-850 Issued 12/18/1998
SA09447AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight guidance Systems Model ST-788-40X/50X Issued 4/21/2000
SA09453AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems model ST-876-20/30. Issued 6/12/2001
SA09467SC Installation of Teledyne Continental motors model no IO-550-F engine and Hartzell model no PHC-C3YF-1RF/F8468A-6R propeller. Amended 8/13/2002
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09513AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-877. Issued 7/20/2001
SA09520SC Installation of Valley Aero Inc. Hydraulic system Pressure Status Annunciator Amended 3/1/2000
SA09952SC Installation of Teledyne Continental Motors IO-550 engine. Issued 9/19/2001
SA1-576 External electrical power receptacle. Reissued 10/15/1974
SA1-625 Installation of Fram lube oil filter Model PB55-1. Amended 9/11/1967
SA1-629 Install 300 series dry vacuum pump conversion kits. Amended 5/9/2001
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1003NE Installation of an Allison 250 B17F turboprop engine (450 hp) Hartzell HCB3TF7A/T9212K-2 constant speed reversing propeller and a 27.7 gallon auxiliay fuel tank in the fuselage aft baggage compartment. Amended 4/16/2009
SA1005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Issued 7/23/2002
SA1005SO Installation of Bendix FCS-870 automatic flight control system or installation of Bendix FCS-870 automatic flight control system with reduced flap motor speed. Amended 12/13/1979
SA1006SO Installation of Bendix NP-2041A area navigation computer programmer. Issued 6/30/1978
SA10070SC Installation of Hartzell 3-bladed propeller. Issued 11/6/2002
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
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
SA10285SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot. Issued 9/27/2004
SA103SW Automatic pilot AK111. Issued 1/1/1961
SA1042SW Hartzell-Wren beta control system. Reissued 9/20/1977
SA1048CE Installation of STOL kit (wing leading edge cuffs stall fences aileron gap seals and droop wing tips). Amended 4/4/1995
SA1058GL Installation of on-board engine analyzer system. Amended 7/12/1990
SA10615SC-D Installation of Hartzell PHC-(C or J) 3YF-1RF/F7693F(B)+2 propeller Reissued 9/11/2008
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1098WE Installation of Roto-Master (Rajay) turbocharged Continental IO-470-E or IO-470-S engine.  Reissued 7/3/2006
SA1100SW Increase wing leading edge radius. Reissued 4/27/1984
SA1102GL Installation of Pamco emergency backup pneumatic system. (T210N S/N 21059810 21059819-21064897) Amended 7/31/1989
SA110EA Removal of right front door and other modifications. Issued 1/1/1996
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1165NW Installation of a one-piece Cee-Bailey windshield Issued 2/13/1981
SA118EA Installation of Fram Part Flow Lube Oil Filter Model PB 55-1. Amended 9/11/1967
SA1202CE Installation of King Model KFC-200 two axis flight control system with or without flight director. Reissued 2/28/2000
SA1230GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA12WE Installation of fiberglass wing tips. Reissued 5/4/2010
SA1303GL Replace Cessna fuel cell drain valve assembly P/N 84C with Safe Air Repair P/N SAR-2. Reissued 4/22/2005
SA1305WE PCA-1 pitch assist with altitude hold. Reissued 10/1/1973
SA1312CE Chrome-plated brake disc installation. Amended 9/13/1977
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
SA1325SW Mitchell automatic flight system AK331 consisting of Century III autopilot with optional automatic pitch trim radio coupler and glide slope coupler. Reissued 7/9/1984
SA1326SW Mitchell automatic flight system AK334 consisting of Century II autopilot with optional radio coupler and automatic aileron stabilizer. Reissued 7/10/1984
SA1327SW Mitchell automatic flight system AK332 consisting of Century I auto- pilot with optional omni tracker. Reissued 7/10/1984
SA1343GL Installation of the MAC 1700 modification to King Radio Corp. KX-175B/KX-170B Transceivers. Issued 12/2/1988
SA1343WE Installation of Brittain Industries Model B-4 Flight Control System. Reissued 10/1/1973
SA1353SO Installation of Armtex Model 477 fire detector. Amended 11/16/1982
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA1376SW Mitchell automatic flight system AK349 consisting of Century I autopilot with optional omni tracker. Reissued 7/10/1984
SA1388SO Installation of crew seats. Amended 8/23/1989
SA1389SO Installation of Brownline seat tracks. Issued 11/24/1982
SA1405SO Replacement and relocation of pre-select flap switch with a continuous input flap switch. Issued 1/13/1983
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1420CE Install wing leading edge cuffs(with or without de-icer boots) and wing stall fences. Reissued 9/5/1979
SA1420WE Installation of Brittain Industries B-4A flight control system. Reissued 10/20/1972
SA1447GL Installation of on-board engine analyzer system. Amended 5/18/1992
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1457NM Installation of a Continental TSIO-520-M(1) engine and a McCauley D3A34C402/90DFA-10 propeller Issued 2/24/1982
SA1466NM Installation of Descent Rate Control (DRC) (wing spoilers) Issued 2/19/1982
SA1471WE Installation of Brittain Industries Model CSA-1 Stability Augmentation System Reissued 4/3/2013
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
SA147CE Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. Issued 1/1/1960
SA1487CE Installation of King KFC200 AFCS two axis with or without flight director. Reissued 2/28/2000
SA149SW Automatic pilot AK120 AK120E AK102E-3 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA1506SW Mitchell aytomatic flight system AK388 consisting of Century III autopilot with optional automatic pitch trim radio and glide slope coupler. Reissued 7/13/1984
SA1507SW Mitchell automatic flight system AK386 consisting of Century I with optional omni tracker. Reissued 7/13/1984
SA150NW Installation of flap gap seals. Amended 3/22/1994
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
SA1525WE Installation of droop ailerons in flaps down mode recontoured wing leading edge and elevator trim spring (except on T210K L M and210K L and M). Reissued 7/21/2005
SA1526SW Mitchell automatic flight system AK387 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/13/1984
SA1527WE Installation of twelve gallon auxiliary fuel tank in each wing inboard of tip. Amended 2/5/2013
SA1552CE-D Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director installed under STC SA1202CE or SA1487CE. Reissued 2/28/2000
SA1579NM Installation of replacement exhaust heat exchanger. Amended 5/22/1986
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA1606WE Installation of Brittain Industries B-4A Flight Control System. Reissued 7/2/2013
SA1609WE Installation of Brittain Industries Model B-5 flight control system. Reissued 6/14/2013
SA1618CE Installation redundant NASA type fuel vent system and modification of fuel vapor return system. Amended 12/1/1988
SA1618WE Installation of Brittain Industries Inc. Model B2C Flight Control System  Reissued 2/1/2013
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1631WE Installation of Brittain Industries B-5 flight control system. Reissued 6/14/2013
SA1643GL Installation of V-type or Y-type shoulder harness. (182 SERIES EXCEPT R182 & TR182) Amended 8/31/1995
SA1672WE Installation of Brittain Industries Model B-5 Flight Control System Reissued 6/14/2013
SA1684WE Installation of Brittain B2C flight control system. Reissued 10/20/1972
SA1686NM Installation of Descent Rate Control(DRC) (wing spoilers). This modification is applicable only to models previously modified in accordance with STC SA1525WE. Issued 8/19/1982
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
SA17EA Installation of Tactair T-101 auto- pilot and optional installation of Tactair T-201 autopilot accessory kit (for use with Tactair T-101 autopilot). Reissued 8/7/1972
SA180RM Installation of Aero Engineering air-conditioning system. Reissued 4/12/1988
SA1870WE Installation of Brittain Model NAV-2B Flight Control System Reissued 6/14/2013
SA1882WE Installation of Brittain Industries NAV-2B flight control system. Reissued 6/14/2013
SA1887WE Installation of Brittain Model NAV-2B Flight Control System  Reissued 6/14/2013
SA1976SO Installation of Appalachian Acces. stainless steel brake discs P/N 73-47. Amended 1/14/1987
SA197EA Installation of Tactair T-3 automatic pilot and optional installation of Tactair AH-1 altitude hold device(for use with Tactair T-3 autopilot). Reissued 8/7/1972
SA1990CE Increase gross weight from3 800 lbs. to 4 000 lbs. For take-off and flight. Issued 5/1/1984
SA199WE Conversion of aircraft for parachute jumping and aerial photography operations. Issued 8/15/1962
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2-1533 Installation of windshield wiper. Reissued 1/31/1997
SA2050CE-D Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis Flight Control System with optional KAS 297B Vertical Speed and Altitude Selector. Reissued 2/28/2000
SA2066NM Coupling of a previously installed Texas Instruments Model 9100 Loran-C system with the existing Bendix FCS-810 Flight Control System and Sperry Stars Model IV8 Flight Director System Issued 3/21/1983
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA20SW Automatic pilot AK086 AK086E or AK086R. Issued 1/1/1960
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
SA210NW Collins AP-107 low profile 3 axis automatic flight control system. Amended 12/2/1977
SA211NW Installation of Collins AP-107 low profile two axis automatic flight control system. Amended 12/2/1977
SA212NW Installation of AP-107 low profile yaw damper system. Amended 12/2/1977
SA2152NM Installation of an engine exhaust gas waste gate controller by-pass valve system. Issued 7/11/1983
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2169SO Installation of Appalachian stainless steel brake discs P/N 75-15A. Issued 9/22/1987
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)