| 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 |
Cessna 210 M - Detailed Data
