| SA00024NY | | Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. | | Amended | | 10/3/2012 |
| SA00027WI | | Installation of flap and aileron gap seals. | | Issued | | 2/11/1993 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00066SE | | Fabrication of interchangeable float spreader bars. | | Amended | | 10/10/2000 |
| 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 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| 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 |
| SA00186AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00188AT | | Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-26A. | | Reissued | | 11/14/1994 |
| SA00194AT | | Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-40. | | Reissued | | 11/14/1994 |
| SA00194BO | | Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. | | Reissued | | 1/23/2009 |
| SA00211AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/17/1994 |
| SA00212AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/17/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00240AT | | Installation of a wing mounted camera pod. Approved for installation on serial number R172-0297 ONLY. | | Amended | | 1/17/2002 |
| SA00243BO (2 OF 5) | | Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). | | Amended | | 7/21/2011 |
| SA00269BO (1OF 3) | | Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. | | Reissued | | 4/9/2010 |
| SA00270WI | | Installation of fiberglass replacement wing tips. | | Amended | | 6/23/2000 |
| SA00272WI | | Replacement of hydraulic system pressure switch. | | Reissued | | 11/8/2007 |
| 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 |
| SA00297NY | | Conversion of tricycle landing gear to tail dragger. | | Issued | | 4/4/1995 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00406WI | | Installation of replacement flap trailing edge bulbs. (R172K XP) | | Amended | | 9/9/1999 |
| SA00419NY | | Installation of cockpit utility light. | | Reissued | | 12/31/2002 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00459WI | | Energy absorbing seat. | | Amended | | 1/28/1997 |
| SA00461SE | | Install a Lycoming O-360 series engine and Hartzell McCauley or Sensenich propeller (See STC for specifications). | | Amended | | 10/24/2002 |
| SA00465NY | | Installation of Meterological Measurement System Model A1MMS-10 with optional installation of Telemetry Module Model AIRDAT-9600. | | Amended | | 10/28/1998 |
| SA00496SE | | Installation of Oregon Aircraft Design Engine Mount Heat Shields. | | Amended | | 12/20/2000 |
| SA00648SE | | Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. | | Issued | | 11/30/1998 |
| SA00671NY | | Installation of AIRDAT Telemetry module. | | Amended | | 10/28/1998 |
| SA00674CH | | Installation of Wipaire 2100 amphibian/seaplane floats. | | Amended | | 8/24/2005 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00679SE | | Installation of interior fiberglass trim panels. | | Amended | | 5/2/2011 |
| SA00680SE (3 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00709CH | | Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2 no rev both dtd 8/30/96 or later FAA app rev. | | Issued | | 7/9/1997 |
| SA00709LA | | Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. | | Reissued | | 5/14/2002 |
| SA00709SE | | Installation of replacement control surface skin panels. | | Issued | | 6/28/1999 |
| SA00726SE | | Installation of a Lycoming O-360-A1AD engine and Hartzell HC-C2YK-1BF/7666A-2 propeller. | | Issued | | 8/10/1999 |
| SA00728SE | | Installation of various models of the Continental IO360 Engine | | Amended | | 3/21/2013 |
| SA00760SE | | Installation of glare shield. | | Reissued | | 5/20/2010 |
| SA00780SE (PAGE 1) | | 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 |
| SA00795CH | | Installation of Baumann Model BF-2550 floats. | | Reissued | | 4/27/2005 |
| SA00796SE | | Installation of vortex generators on the wings and tail surfaces of the above model aircraft | | Amended | | 5/27/2004 |
| SA00812CH | | Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. | | Reissued | | 6/30/2006 |
| SA00831SE | | Installation of vortex generators on wings and tail surfaces. | | Issued | | 8/4/2000 |
| SA00834SE | | Installation of vortex generators on wings and tail surfaces. | | Issued | | 8/11/2000 |
| 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 |
| 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 |
| SA00900CH | | Installation of Wipaire Model 2350 Amphibian/Seaplane Floats and McCauley Model 1A200/WFA propeller. | | Amended | | 9/28/2011 |
| SA00919SE | | : Installation of vacuum stall warning system as either the primary or as a secondary stall warning system in accordance with drawings and instructions listed in AML SA00919SE.
);INSERT INTO stc_table VALUES ( | | Issued | | 5/24/2001 |
| 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 |
| SA01015SE | | Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. | | Amended | | 10/4/2012 |
| SA01026SE (PAGE 2) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01032WI | | Installation of external aerodynamic Vortelator Kit on airplanes | | Amended | | 7/11/2008 |
| 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 |
| 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 |
| 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 |
| SA01204LA | | Installation of replacement wing tip fairing assembly. | | Issued | | 10/3/2001 |
| SA01205WI-D (1 OF 2) | | Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.
);INSERT INTO stc_table VALUES ( | | Amended | | 11/20/2007 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01233SE | | Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision. | | Amended | | 5/22/2012 |
| 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 |
| SA01298SE | | Installation of interior trim parts. | | Reissued | | 5/20/2010 |
| 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 |
| SA01330LA (PAGE 1) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 |
| SA01356SE | | Installation of Instrument Panel and Y | | Issued | | 12/22/2003 |
| SA01386NY | | Installation of Fibre Glass Reinforced Plastic Nacelle Fairing Trade Name Exhaust Fairing . | | Reissued | | 10/9/2002 |
| 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 |
| SA01646SE | | Installation of vortex generators on wings horizontal and vertical tail surfaces. | | Issued | | 2/28/2006 |
| SA01660SE | | Installation of interior fiberglass panels. | | Reissued | | 5/20/2010 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01679CH | | Install BRS-172 parachute recovery system. | | Amended | | 8/29/2012 |
| 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 |
| SA01714WI (Page 1) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
| SA01765SE | | Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. | | Amended | | 10/11/2012 |
| SA01800SE (PG 1) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01815CH | | Installation of Baumann Model BF2550A floats. For models 172I through 172P a gross weight of 2350 lbs. at a center of gravity range of plus 39.5 inches to plus 45.5 inches is approved. For models R172K and R172K with STCs SA1436CE and SA1437CE the maximum gross weight is limited to 2550 lbs. at a center og gravity range of plus 39.5 inches to plus 45.5 inches. | | Reissued | | 1/10/2005 |
| 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 |
| SA01923LA | | Installation of the P-1000 Digital Electronic Tachometer. | | Issued | | 1/23/2007 |
| 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 (2 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
| SA01944CH (1 OF 2) | | Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. | | Issued | | 3/5/2004 |
| 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 |
| 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 |
| 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 |
| 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 |
| SA02138AT | | Installation of Lord Corporation nose wheel shimmy damper part number SE-1051-2/3. | | Amended | | 8/11/2006 |
| 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 |
| SA02155AK | | Installation of Hartzell model HC-C2YR-1BF/F8477-4 propeller and Hartzell model C-1576 damper assembly. | | Reissued | | 1/15/2004 |
| SA02186AK | | Installation of Hartzell HC-C2YR-1BF/F8477-4 or HC-C2YK-1BF/F8477-4 propeller and Hartzell model C1576 damper assembly. | | Reissued | | 6/16/2004 |
| SA02203AK (PAGE 1) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02211CH | | Installation of a Three Point Torso Restraint System | | Issued | | 11/15/2005 |
| SA02212AK (PG 1) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems | | Amended | | 5/4/2011 |
| 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 |
| SA02231AK | | Installation of Cleveland Main Wheels and Brakes. | | Reissued | | 3/17/2008 |
| SA02245CH | | Installation of a MT-Propeller model MTV-15-() propeller and P-237-12 or P-277-B spinner assembly | | Amended | | 5/1/2008 |
| SA02246LA | | Installation of a flap handle extension. | | Amended | | 11/16/2010 |
| 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 1) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02276AK | | Installation of AMSAFE Aviation Inflatable Restraints | | Amended | | 3/12/2013 |
| SA02282AK | | Installation of Lycoming IO-360 (200 or 180 hp) engine and associated powerplant components including propeller modified exhaust baffling cowling modifications. | | Amended | | 4/19/2010 |
| 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 |
| 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 |
| SA02343AK | | Installation of Lycoming Engine Model IO-390-A1A6 or IO-390-A3A6 Hartzell model HC-C2YR-1BFP/F8477-4 or MT propeller model MTV-15-B/210-58 | | Issued | | 6/22/2010 |
| SA02359AK-D | | Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp | | Issued | | 11/6/2009 |
| SA02376AK | | Replacement of tricycle landing gear with conventional (tail-wheel) landing gear | | Issued | | 12/12/2010 |
| SA02386AT | | Installation of engine cowling and firewall fasteners. | | Issued | | 8/29/2001 |
| SA02411CH | | Installation of the Aero Vent Cabin Ventilation System. | | Issued | | 7/25/2008 |
| SA02415CH | | Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. | | Issued | | 5/10/2007 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02446CH | | Installation of the Courtesy Light Kit. | | Issued | | 6/25/2007 |
| SA02462CH | | Installation of Flight Boss LTD S-RPE-CO Rudder Pedal Extensions | | Issued | | 8/29/2007 |
| 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 |
| SA02648AT | | Installation of Lycoming model O-360-A4M engine McCauley model 1A200/DFA8242 propeller two oil coolers engine exhaust system four NACA scoops for cabin and oil cooler ram air and a triple banner tow/release mechanism. Limited to installation on Cessna 175 serial number 55238 ONLY. | | Issued | | 4/1/2003 |
| 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 |
| 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 |
| 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 |
| SA02987CH | | Installation of the Electroair Electronic Ignition System | | Amended | | 7/23/2013 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09133AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-612 with optional autotrim. | | Amended | | 2/28/2001 |
| SA09149AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-627 with optional autotrim system. | | Amended | | 2/20/2001 |
| SA09149SC | | Modification of nose gear fork P/N SK150-11 to the SK182-34 configuration. | | Amended | | 2/22/1996 |
| SA09154AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-616 with Optional Autotrim System. | | Amended | | 10/12/2001 |
| SA09157AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-633 with Optional Autotrim System. | | Amended | | 10/18/2001 |
| SA09161AC-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-182-40/50. | | Issued | | 8/7/1996 |
| SA09209AC-D | | Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-671-20/30. | | Amended | | 8/27/1999 |
| SA09215AC-D | | Installation of S-TEC System 30 ALT altitude hold system Model ST-673. | | Issued | | 5/16/1997 |
| SA09225AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems. | | Issued | | 5/23/1997 |
| SA09229AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-686. | | Issued | | 6/4/1997 |
| SA09238AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-674-20/30. | | Issued | | 6/16/1997 |
| SA09279AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-675. | | Issued | | 10/10/1997 |
| SA09427AC-D | | Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-868-40X/50X. | | Issued | | 3/17/2000 |
| SA09442AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-874-20/30. | | Issued | | 7/24/2000 |
| SA09445AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-875. | | Issued | | 5/1/2000 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA1-124 | | Lube oil filter BP55-1. | | Issued | | |
| SA1-219 | | Gyro-stabilizer 69A122. | | Issued | | |
| SA1-252 | | Safety gear Model A. | | Issued | | |
| SA1-426 | | Auxiliary seat in baggage compartment. | | Reissued | | 10/25/2001 |
| SA1-516 | | Griswold lateralizer and heading lock. | | Amended | | |
| SA1-545 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| SA1-610 | | Wet-to-dry vacuum pump conversion kit 300-2. | | Reissued | | 4/22/2003 |
| SA1-612 | | Installation of Tactair T-101 autopilot and optional installation of Tactair T-201 autopilot accessory kit (for use with Tactair T-101 autopilot). | | Reissued | | 8/7/1972 |
| SA10005SC | | Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. | | Reissued | | 12/29/2006 |
| SA1005SC | | Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. | | Issued | | 7/23/2002 |
| SA10077SC | | Installation of push-button starter system. | | Amended | | 4/26/2005 |
| 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 |
| SA1017NE | | Installation of .187 in thick windshield. | | Issued | | 10/16/1992 |
| SA10236SC (2 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1087GL | | Installation of a Shadin Co. fuel flow indicating system. | | Reissued | | 6/8/2006 |
| SA109SW | | Automatic pilot AK106. | | Issued | | 1/1/1961 |
| SA10WE | | Arens Vernier type throttle control. | | Issued | | 1/1/1961 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1117NW | | Installation of an 18 inch diameter camera hole in the rear passenger area floor and an optical scanner mounted in the left pilot s window | | Issued | | 1/16/1981 |
| SA115NW | | Modification of R.H. Door and the addition of a jump seat. | | Amended | | 4/30/1981 |
| SA1168SO | | Installation of Aqua Model 2200 floats. | | Amended | | 8/15/2001 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA11SO | | Tank type end plates. | | Issued | | 1/1/1960 |
| SA1210GL | | Install SAT-T-STOP auxiliary seat stop device. | | Reissued | | 6/15/2012 |
| SA121CE | | Nose and main gear wheel fairing(Jetstreams) using standard unaltered Cessna landing gear and nose gear fork for model and year using 500 x 5 nose and 600 x 6 main gear tires. | | Amended | | 3/1/1977 |
| SA122NW | | Installation of a Continental O-470 series engine McCauley propeller engine mount cowling baffles and associated parts on the Cessna 175 and P172D series aircraft | | Reissued | | 10/24/2012 |
| SA1261WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1295SO | | Installation of an adjustable nine-inch trim tab on left aileron. | | Issued | | 11/13/1981 |
| SA12CE | | Removal of right cabin door. | | Issued | | 2/25/1962 |
| SA12WE | | Installation of fiberglass wing tips. | | Reissued | | 5/4/2010 |
| 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 |
| SA1371SW | | Wing leading cuff wing tips and upper surface flow fences. | | Amended | | 4/14/1983 |
| SA1399SO | | Remove drain plug Cessna P/N MS20913-1 or MS20913-1D from bottom of fuel selector valve body and replace with drain valve Middle Tennessee P/N MT-1075. (175 S/N 28700A 55001-56238) (175A 619 56239-56777) (175B 17556778-17557002) (175C 17557003-17557119 ) | | Amended | | 2/17/2004 |
| SA13GL | | Installation of Cleveland wheel No. 40-97A and brake No. 30-63A. (140A S/N 13400 AND UP) | | Amended | | 4/1/1981 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1431WE | | Installation of rudder trim system. | | Amended | | 4/2/1978 |
| SA1437CE | | Continental IO-360-K or KB engine installation rerated to 210 hp (2800 rpm) at takeoff and 195 hp(2600 rpm) maximum continuous. Rerated engine designation IO-360-KC/STC SE1436CE or IO-360-KBC/STC SE1436CE. (R172K LANDPLANE AND FLOATPLANE) | | Reissued | | 4/7/2008 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| SA1455WE | | Installation of Brittain Industries Model CSA-1 Flight Control System | | Amended | | 9/12/1979 |
| SA1473WE | | Installation of Brittain Model B2C Flight Control System. | | Reissued | | 10/20/1972 |
| SA1474SW | | Installation of MASA 1223000-7 and -8 wing tip. | | Reissued | | 9/5/1979 |
| SA147CE | | Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. | | Issued | | 1/1/1960 |
| SA1491CE | | Installation of flap and aileron gap seals. | | Amended | | 2/24/2005 |
| SA1492CE | | Installation of flap and aileron gap seals. | | Reissued | | 1/27/1993 |
| SA1500GL | | Installation of on-board engine analyzer system. | | Issued | | 7/18/1990 |
| 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 |
| SA1518GL | | Install shoulder harness and seat belt assembly. | | Issued | | 8/31/1990 |
| SA1568CE-D | | Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system. | | Reissued | | 2/28/2000 |
| SA156NW | | Installation of baggage hatch with cover on EDO Model 2200 floats | | Issued | | 7/15/1975 |
| 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 |
| SA158CE | | Cessna wing tips and attached lights 1223000-1 left 1223000-2 right tips and 1423006-12 left 0423006-13 right lights or an eqivalent. | | Issued | | 1/1/1960 |
| SA1614WE | | Installation of one 12-gallon auxiliary fuel tank in each outboard wing panel. | | Amended | | 12/6/2006 |
| SA1626NM Page 1 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1643GL | | Installation of V-type or Y-type shoulder harness. (182 SERIES EXCEPT R182 & TR182) | | Amended | | 8/31/1995 |
| SA1668CE | | Installation strut/wing and strut/fuselage fairings lightning hole covers and aerodynamic putty. | | Reissued | | 1/27/1993 |
| 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 |
| SA170CH | | Install a control yoke and instrument panel. | | Amended | | 7/1/2009 |
| SA175EA | | Installation of wing struts modified to include Wings With Springs Model200 hydraulic-pneumatic shock absorbers and associated airframe modifications. | | Amended | | 8/17/1977 |
| SA1760SO | | Installation of Appalachian Access. stainless steel brake rotors P/N 75-15C. | | Reissued | | 2/6/1995 |
| SA179NW | | Installation of flap gap seals | | Issued | | 11/25/1975 |
| 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 |
| SA1824NM | | Installation of Lompoc Aero Specialties inner plexiglass pane
);INSERT INTO stc_table VALUES ( 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.I | | Reissued | | 1/23/2004 |
| SA1827CE | | Installation of photo bubble in baggage door opening. | | Reissued | | 2/16/1983 |
| SA182CH | | Installation of removable Telonics telemetry antennas. | | Reissued | | 5/4/1994 |
| SA1895NM | | Installation of flap gas fairing. | | Issued | | 8/1/1983 |
| SA2-1178 | | Replacement of right front seat with stretcher. | | Amended | | 11/14/2001 |
| SA2-1533 | | Installation of windshield wiper. | | Reissued | | 1/31/1997 |
| SA2067NM | | Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System | | Amended | | 7/11/2012 |
| SA20NW | | Installation of a Lycoming O-360-A1A engine and a Hartzell propeller | | Issued | | 12/29/1972 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA212GL | | Installation of windshield P/Ns W-2056 W/T-2056 or W/G-2056. | | Reissued | | 1/31/2007 |
| SA2137SO | | Fabrication and installation of nose wheel fairings. | | Reissued | | 7/17/1989 |
| SA2138CE | | Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. | | Amended | | 6/23/1992 |
| SA2162NM | | Installation of the Precise Flight stand-by vacuum system (SVS) | | Amended | | 11/7/2003 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2190SO | | Replacement of Cleveland brake discs P/N 164-40 or 164-140 with Appalachian Accessories stainless steel brake discs P/N 75-40. | | Reissued | | 2/6/1995 |
| SA220SO | | Tow bar release mechanism and safety tow link. | | Reissued | | 10/3/2011 |
| SA221SO | | To remove right door for hauling sky divers picture making and etc. | | Reissued | | 1/2/2013 |
| SA2229WE | | Installation of Madras wing tips | | Amended | | 2/21/1973 |
| SA2256WE | | Installation of leading edge cuff on each wing. | | Reissued | | 1/21/2010 |
| SA2282CE | | Installation of aileron and/or flap gap seals. | | Amended | | 10/10/1991 |
| SA2298SO | | Replacement of Cleveland brake discs P/N 164-26A or 164-126A with Appalachian Accessories stainless steel brake discs P/N 75-27. | | Issued | | 4/18/1988 |
| SA232EA | | Installation of Tactair omni lock model OL-1 and optional installation of Tactair localizer adapter model LA-1 (for use with Tactair model omni lock model OL-1). | | Reissued | | 8/7/1972 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2381NM | | Installation of Knots 2U Ltd Wheel and Body Fairings | | Amended | | 8/19/2008 |
| SA2381SO | | Installation of Appalachian Accessories P/N 75-92 Brake Rotors. (182 SERIES THRU 182A) | | Reissued | | 9/29/1995 |
| SA2382NM | | Installation of Aileron and Flap Gap Seals. | | Amended | | 7/15/2003 |
| SA2382SO | | Installation of Appalachian Accessories stainless steel brake discs. (182 SERIES THRU 182Q) | | Reissued | | 9/29/1995 |
| SA2383SO | | Installation of Appalachian Accessories P/N 75-94 Brake Rotors. | | Reissued | | 9/29/1995 |
| SA238SW | | Installation of cargo door. | | Reissued | | 3/9/1987 |
| SA2518CE | | Installation of replacement wing tips. | | Amended | | 11/4/1992 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA256NW | | Installation of aileron gap seals. | | Amended | | 4/12/1993 |
| SA2586NM (PAGE 2) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2682CE | | Installation of steering rod boots. | | Issued | | 12/19/1990 |
| 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 |
| SA2710WE | | Installation of carburetor heat box bearings. | | Issued | | 6/15/1973 |
| SA2792CE | | Installation of wing mounted convex mirror for inspection of nose and main landing gear position. | | Issued | | 2/6/1992 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA2853SW | | Leading edge cuffs stall fences aileron seals wing tips. | | Amended | | 3/2/1989 |
| SA28WE | | Federal F-300 autopilot. | | Issued | | 1/1/1960 |
| SA293NW | | Installation of Franklin 6A-350-C1 or 6A-350-C2 engines Hartzell HC-C2YF-1BF/F8459A -4 to -8 HC-C2YF-1BF/F8459A-4Q to -8Q or McCauley 2A31C21/84S-4 to -8 propellers in accordance with Seaplane Flying Inc. Assembly and Installation Instructions SF 20690 SF20821 or SF 20820 on Cessna Models 170A 170B 172 172A 172B through P 175 175A 175B and 175C as defined in AML.
);INSERT INTO stc_table VALUES ( 2.) Installation of Franklin 6A-350-C1R engines Hartzell HC-C2YF-1BF/F8459A-4 to -8 HC-C2YF-1BF/F8459-4Q to -8 McCauley 2A31C21/84S-4 to -8 or 2A34C201/90DA-10 to -14 propellers in accordance with Seaplane Flying Inc. Assembly and Installation Instructions SF 20690 on Cessna Models 170A 170B (Serial Numbers 20267 to 26504) as defined in AML. | | Amended | | 4/21/2011 |
| SA2960NM | | Install stay put (seat position locking device). | | Amended | | 3/14/1986 |
| SA3-285 | | 18-gallon auxiliary fuel system. | | Issued | | 1/1/1960 |
| SA3-333 | | Installation of Doyn fiberglass wheel fairings. | | Reissued | | 8/16/2011 |
| SA3-576 | | Installation of speed kit. | | Reissued | | 1/27/1993 |
| SA3-611 | | Model 3000 main ski and Model 2000 nose ski. | | Issued | | 1/1/1960 |
| SA3-674 | | Installation of Lycoming O-360-A1D engine and McCauley 2D36C14/78KM-4 or Hartzell HC-C2YK-1A/7666-2 propeller in accordance with Doyn Aircraft Drawing List for Model 1700 conversion dated May 6 1964 for Cessna Model 175B: Atlas Aviation Oil Cooler Installation dated September 12 1967 is required. | | Reissued | | 7/14/2011 |
| SA3-691 | | Installation of Doyn swept-tail assembly kit 1400. | | Reissued | | 8/16/2011 |
| 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 |
| SA308EA (1 OF 2) | | Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) | | Amended | | 11/20/1978 |
| SA3147SO | | Installation of aileron and flap gap seals. | | Reissued | | 1/23/2012 |
| SA3203SO | | Replacement of Cleveland brake disks P/N 164-26A and/or 164-126A with Appalachian Accessories stainless steel brake disks P/N 75-27. | | Reissued | | 9/29/1995 |
| SA3227SW-D | | Mitchell automatic flight system AK699 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 12/7/1983 |
| SA3228SW-D | | Mitchell automatic flight system AK698 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 12/7/1983 |
| SA327GL | | Installation of fuel tank caps. | | Issued | | 7/16/1979 |
| SA3284SW-D | | Installation of Mitchell automatic flight system Model AK730 consisting of a Century I autopilot with optional omni tracking system. | | Reissued | | 3/28/1984 |
| SA3285SO | | Installation of engine cowling and firewall fasteners. (172 S/N 54893 THRU 76673) (R172 SERIES S/N 2000 THRU 3454) | | Amended | | 8/29/2001 |
| SA3285SW-D | | Mitchell automatic flight system AK731 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 3/29/1984 |
| SA3286SW-D | | Mitchell automatic flight system AK732 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 3/29/1984 |
| SA3363SW | | Mitchell automatic flight system AK861 consisting of Century 21 autopilot. | | Reissued | | 3/24/1983 |
| SA3487WE | | Installation of tail flood light. | | Reissued | | 2/28/1980 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA356CH | | Installation of seaplane safety covers. | | Issued | | 5/22/1995 |
| SA3585NM | | Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. | | Issued | | 4/3/1987 |
| SA3691NM | | Cockpit sunvisor installation | | Reissued | | 3/24/2003 |
