| 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 |
