| 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 |
| SA00033WI | | Installation of flap and aileron gap seaps. | | Issued | | 2/11/1993 |
| SA00039LB | | Installation of an Ashtech AV-12 Global Positioning System and a Aero GPS Antenna. | | Reissued | | 11/5/1999 |
| 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 |
| SA00087NY | | Installation of Cu-Sonde Meteorological Measurement/system models CS-1A or CS-1B and installation of Cu-Sonde Model CS-1B-RF with AIRDAT-9600. | | Reissued and Amended | | 8/22/1995 |
| SA00103BO | | Installation of Weemax cabin air vent. | | Issued | | 6/16/1999 |
| SA00147AT | | Installation of Type A sun visor. | | Amended | | 7/28/1993 |
| 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 |
| 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 |
| SA00261SE | | Installation of Lycoming O-320-E2D engines modified by STC SE00252SE O-320-D2G or O-320-D2J engine and McCauley 1C160/CTM 7557 or 1C160/DTM 7557 or 1A175/ETM (seaplane only) propeller. (Landplanes and Seaplanes) | | Amended | | 12/3/1998 |
| 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 |
| 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 |
| SA00335LA | | Conversion of tricycle landing gear to tail wheel type (conventional) landing gear. (S/N 28058) | | Issued | | 1/8/1997 |
| 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 |
| 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 |
| SA00433 | | Installation of Airwolf remote mounted engine oil filter Model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less. (with Franklin engines) | | Amended | | 5/7/1997 |
| SA00433NY | | Installation of Airwolf remote mounted engine oil filter model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less. | | Amended | | 10/31/2012 |
| SA00455SE | | Modification of carburetor heat box. | | Issued | | 7/3/1997 |
| 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 |
| SA00506WI | | Installation of a pallet assembly that houses a special mission camera and computer in the baggage area | | Issued | | 3/11/1997 |
| SA00520WI | | Installation of engine mount gussets. | | Issued | | 5/13/1997 |
| SA00545NY | | Installation of an Argus 5000/CE Moving Map Display. | | Issued | | 1/14/1997 |
| SA00548AT | | Installation of camera hole. | | Issued | | 7/28/1994 |
| SA00622DE | | Installation of John Deere AGRI Services Inc. JD3 Aerial Imaging System | | Reissued | | 11/15/2007 |
| 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 |
| SA00728SE | | Installation of various models of the Continental IO360 Engine | | Amended | | 3/21/2013 |
| SA00744DE | | Installation of Automatic Dependent Surveillance | | Amended | | 3/28/2013 |
| 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 |
| SA00811WI | | Heat Air Induction System on above model. | | Issued | | 8/23/1999 |
| SA00812CH | | Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. | | Reissued | | 6/30/2006 |
| SA00812NY | | Installation of Technisonic Industries Limited TFM-138 A and B (does not include TFM-138 s/n 1540 and up TFM-138B s/n 1500 and up). | | Amended | | 9/12/2005 |
| SA00819SE | | Installation of Visual Instruments flap position indicating system. | | Issued | | 7/18/2000 |
| SA00831SE | | Installation of vortex generators on wings and tail surfaces. | | Issued | | 8/4/2000 |
| SA00843NY | | Aircraft fuel quantity transmitter replacement-from Stewart Warner Model 390 to Stewart Warner Model 385. | | Issued | | 5/28/1998 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00865NY | | Installation of nose gear strut fairing. | | Amended | | 9/20/1999 |
| 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 |
| SA00910WI-D | | Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. | | Issued | | 11/1/2000 |
| 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 |
| SA00926WI | | Installation of MT-Propeller MTV-18-B/183-17 electric 3-blade constant speed propeller. | | Reissued | | 3/20/2007 |
| 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 |
| SA01001SE | | Installation of 12 volt cabin power system for portable electronic devices in accordance with Olympic Aero Services Inc. Master Drawing List OAS-54-0001 Revision G dated September 26 2002 or later FAA approved revision. This system shall be maintained in accordance with Instructions for Continued Airworthiness Document OAS-54-23.1529 Revision B dated August 22 2001 or later FAA approved revision. | | Reissued | | 4/9/2012 |
| 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 |
| SA01026CH | | Change maximum gross weight limit to 2250 lbs. (172N s/n 17267616) | | Issued | | 4/13/1999 |
| SA01026SE (PAGE 2) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01032WI | | Installation of external aerodynamic Vortelator Kit on airplanes | | Amended | | 7/11/2008 |
| SA01070WI-D | | Installation of Bendix/King KDR 510 VHF Data Link System. | | Issued | | 4/9/2002 |
| 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 |
| SA01080LA | | Installation of Accessory Power Receptable in accordance with FAA Approved Master Drawing List Document No. 172-APR-100 Rev IR dtd 8/15/00 or later FAA approved revision. | | Reissued | | 3/2/2001 |
| SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
| SA01088SE | | Installation of Dynamic Propellers induction air inlet on carburetor air box. | | Issued | | 5/14/2002 |
| SA01095WI | | Installation of Gomolzig C172R-606550 engine exhaust system silencer. | | Reissued | | 3/20/2007 |
| 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 |
| SA01158WI (1 OF 2) | | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | Amended | | 3/29/2005 |
| SA01170NY | | Installation of NPX138N-XXX FM Transceiver. | | Amended | | 1/17/2007 |
| SA01183AT | | Installation of a Cockpit glare shield. | | Issued | | 10/29/1996 |
| SA01202LA | | Installation of Becker Avionics SAR DF-517 Search and Rescue Direction Finding System | | Reissued | | 2/13/2012 |
| 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 |
| SA01220WI | | Installation of hydraulically controlled variable pitch 3 blade MTV-12-B/183-17 propeller. | | Issued | | 4/5/2004 |
| 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 |
| 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 |
| SA01265AT | | Installation of Composite Spinner Assemblies. | | Amended | | 10/13/2000 |
| 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 |
| SA01289AT | | Manufacture of composite engine cowlings. | | Reissued | | 5/21/2007 |
| SA01298SE | | Installation of interior trim parts. | | Reissued | | 5/20/2010 |
| SA01303WI | | Installation of a Thielert TAE-125-01 aircraft diesel engine associated systems and gross weight changes. | | Amended | | 11/23/2009 |
| 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 |
| SA01386NY | | Installation of Fibre Glass Reinforced Plastic Nacelle Fairing Trade Name Exhaust Fairing . | | Reissued | | 10/9/2002 |
| SA01388SE | | Installation of 7-gallon or 15-gallon extended range wing fuel tanks manufactured and installed | | Amended | | 10/18/2007 |
| SA01428LA | | Installation of CO Guardian Carbon Monoxide Detector Instrument. | | Issued | | 2/10/2003 |
| 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 |
| SA01454SE | | Incorporation of a nylon sleeve on the carburetor heat cable housing to prevent abrasion of the cable | | Issued | | 9/20/2004 |
| SA01456NY | | Installation of Technisonic Industries Ltd OSAT-100 Airborne Position/Data Communicator. | | Issued | | 1/31/2002 |
| 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 |
| SA01531LA | | Installation of CO Guardian Remote Carbon Monoxide Detector Instrument. | | Issued | | 8/28/2003 |
| SA01538SE | | Incorporation of bushing on carburetor hot air box control arm in accordance with Dynamic Propeller Installation Instructions No. 7000 Revision A dated February 24 2005 or later FAA approved revision to this document. | | Issued | | 4/27/2005 |
| SA01551AT | | Installation of a Lycoming O-360-A1-A engine and a Hartzell HC-C3YF-1RF/F7282 propeller. | | Reissued | | 7/14/1998 |
| 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 |
| SA01626WI | | One Aircraft Only installation of a Teledyne Continental Motors IO-360-D engine with two-bladed McCauley constant speed propeller powerplant installation and fuel system modifications.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( Data Required:
);INSERT INTO stc_table VALUES ( 1. A copy of this certificate and
);INSERT INTO stc_table VALUES ( 2. Installation Drawing No. 210-172-001 Rev. D dated April 25 2011 and
);INSERT INTO stc_table VALUES ( 3. Supplemental Airplane Flight Manual No. SAFM-17248124 dated April 25 2011 and
);INSERT INTO stc_table VALUES ( 4. Instructions for Continued Airworthiness No. 210-172-002 Rev (-) dated April 25 2011 or
);INSERT INTO stc_table VALUES ( later FAA approved revisions thereof. | | Issued | | 4/25/2011 |
| 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 |
| SA01686AT | | Installation of a Lycoming Model O-360-A1A engine and a Hartzell model HC-C3YR-1RF/F7282. | | Issued | | 1/1/1961 |
| 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 |
| SA01700LA | | Installation of AMSAFE Aviation Inflatable Restraint (AAIR) system. | | Issued | | 12/3/2004 |
| 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 |
| SA01768SE | | Install oil cooler system. | | Issued | | 6/8/2007 |
| SA01800SE (PG 1) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01801AT | | For the Cessna 172 airplane models incorporating Lycoming O-320 engines: Modification of the standard exhaust system as documented in Laminar Flow Systems Installation Instructions Document Laminar Flow System Extractor Exhaust System Revision A dated November 20 1998 and Technical Drawing List Book No. PFS-B-800 dated November 16 1998 or per Power Flow Systems Inc. Installation Instructions Document PFS-0058-00 Rev. A dated October 5 2001 and Master Drawing List Report No. PFS-0032-00 Rev. IR dated August 10 2000 or later FAA approved revisions.
);INSERT INTO stc_table VALUES ( For the Cessna 172 airplane models incorporating Lycoming O-320 O-360 0r IO-360 engines:
);INSERT INTO stc_table VALUES ( Modify the standard exhaust system as document in Power Flow Systems Inc. Installation Instructions Document PFS-13250-00 Rev B dated December 9 2002 and Master Drawing list PFS-13240-00 Rev IR dated October 3 2002. | | Reissued | | 10/16/2003 |
| 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 (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 |
| SA02006CH | | Installation of air conditioning system. | | Amended | | 12/20/2011 |
| 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 |
| SA02104AK | | Installation and fabrication of R & J Aircraft extended baggage compartment. | | Issued | | 3/4/1998 |
| 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 |
| SA02228AT | | For model 172 airplanes with Lycoming O-360 engines per STC SA332GL or STC SA4428SW modification of standard exhaust system. For model 172 with Lycoming O-360 engines per STC SA647CE or STC SA1324CE modification of standard exhaust system. | | Amended | | 1/16/2001 |
| SA02231AK | | Installation of Cleveland Main Wheels and Brakes. | | Reissued | | 3/17/2008 |
| SA02236AT | | Installation of a Paravion (formerly FSI) Eagle Vision Camera System on the Model 172M (S/N 17262323) and a Spectrolab SX5 Search Light on the Model 172S (S/N 172S8566) both fuselage mounted in accordance with Aero Avionics Master Drawing List No. AA-C172-001 dated September 21 2000 or later FAA approved revision. | | Amended | | 4/17/2003 |
| 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 |
| SA02248LA | | Installation of Sensor Pod and wiring for a passenger operated monitoring system | | Reissued | | 1/30/2014 |
| SA02249SE | | Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor | | Amended | | 9/18/2013 |
| 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 |
| SA02277AK | | Installation of FMK Light Emitting Diode (LED) Instrument Panel Lights. | | Issued | | 9/30/2006 |
| 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 |
| SA02302SE | | Remove standard Scott 3200 tail wheel and fork and replace with a Gar-Aero-32 tail wheel fork 24 spacer and a 4.00 x 4 6 ply tire | | Issued | | 2/4/2014 |
| SA02321AK | | Installation of EDO 89-2000 floats modified | | Issued | | 8/29/2008 |
| 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 |
| SA02376AK | | Replacement of tricycle landing gear with conventional (tail-wheel) landing gear | | Issued | | 12/12/2010 |
| SA02400AK | | Installation of Aerocet 2200 floats | | Issued | | 9/17/2012 |
| 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 |
| SA02419AT | | Manufacture of Composite Engine Cowlings | | Issued | | 11/9/2001 |
| SA02427AT | | Installation of an Avia V503AP propeller in accordance with Turbine Design Inc. Installation Instructions Report No. 2000-008 original revision March 1 2000 or later FAA approved revision. | | Reissued | | 11/14/2003 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02437LA | | Installation of straight tail vertical stabilizer and rudder assembly | | Issued | | 12/14/2012 |
| 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 |
| 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 |
| SA02725CH | | Installation of North American Surveillance Systems Strut Mount and Optional Cloud Cap Technologies TASE / TASE Dou Gimbals | | Issued | | 5/29/2009 |
| SA02738CH (PAGE 4) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| 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 |
| 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 |
| SA03984AT | | Installation of a FreeFlight Systems Universal Access Transceiver - Automatic Dependent Surveillance | | Issued | | 12/13/2012 |
| SA09132AC-D | | Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-612 with optional autotrim. | | Amended | | 2/28/2001 |
| SA09149SC | | Modification of nose gear fork P/N SK150-11 to the SK182-34 configuration. | | Amended | | 2/22/1996 |
| SA09151AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-616 with Optional Autotrim System. | | Amended | | 10/12/2001 |
| SA09152SC | | Installation of a wing mounted video camera VCR and associated equipment. | | Issued | | 1/31/1996 |
| SA09156AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-633 with Optional Autotrim System. | | Amended | | 10/18/2001 |
| SA09201AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-563 with Optional Autotrim System. | | Amended | | 2/1/2001 |
| SA09202AC-D | | Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-184-40/50. | | Issued | | 4/1/1997 |
| SA09207AC-D | | Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-671-20/30. | | Issued | | 5/12/1997 |
| SA09208AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-671-20/30. | | Amended | | 9/23/1998 |
| SA09213AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-673. | | Issued | | 5/16/1997 |
| SA09214AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-673. | | Amended | | 9/25/1998 |
| SA09224AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-685-20/30. | | Amended | | 9/10/1999 |
| SA09228AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System. | | Issued | | 6/4/1997 |
| SA09237AC-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 |
| SA09278AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-675. | | Issued | | 10/10/1997 |
| SA09350SC | | Approves Aircraft Publications Pilot Operating Handbook as an Airplane Flight Manual (AFM) for aircraft listed on FAA Approved Model List. | | Amended | | 11/28/1997 |
| SA09352SC | | Add exhaust pipe extension. | | Amended | | 6/1/1998 |
| SA09362SC | | Installation of a panel and radio lamp dimmer control system. | | Issued | | 7/24/1997 |
| SA09370SC | | Installation of a 95-ampere alternator. | | Reissued | | 5/30/2012 |
| SA09371SC | | Installation of a vapor cycle air conditioning system. | | Reissued | | 5/30/2012 |
| SA09412AC-D | | Installation of S-TEC manual electric trim system Model ST-157 | | Issued | | 8/25/1999 |
| SA09425AC-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 |
| SA09426AC-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 |
| SA09457SC | | Installation of a vapor-cycle air conditioning system. | | Reissued | | 5/17/2013 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA09491SC | | Installation of a low voltage warning system. | | Amended | | 5/3/2001 |
| SA09524AC-D | | Installation of S-TEC System 60 Pitch Stabilization System Model ST-060. | | Issued | | 3/25/2002 |
| SA09526AC-D | | Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System Model ST-025. | | Issued | | 3/25/2002 |
| SA1-116 | | Federal F-300 autopilot. | | Issued | | |
| SA1-124 | | Lube oil filter BP55-1. | | Issued | | |
| SA1-193 | | Conversion of aircraft for parachute jumping operations. | | Reissued | | 10/18/1995 |
| SA1-219 | | Gyro-stabilizer 69A122. | | Issued | | |
| SA1-252 | | Safety gear Model A. | | Issued | | |
| SA1-426 | | Auxiliary seat in baggage compartment. | | Reissued | | 10/25/2001 |
| SA1-438 | | Lycoming O-360-A1A engine and McCauley 2D36C14/78 KM-4 propeller with Woodward 210105 AA governor. | | Amended | | |
| SA1-516 | | Griswold lateralizer and heading lock. | | Amended | | |
| SA1-545 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| 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 |
| SA1-9 | | 69A115 gyro-stabilizer. | | Issued | | 1/1/1961 |
| SA10005SC | | Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. | | Reissued | | 12/29/2006 |
| SA1000EA | | Installation of Pee-Kay Model 2300 or B2300 (TSO-C27-2) seaplane floats. (172N SEAPLANE) | | Reissued | | 10/13/2000 |
| 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 |
| SA1017NW | | Installation of a Nite Sign Inc Model II Aerial Advertising System | | Issued | | 9/5/1980 |
| SA1018NE | | 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 |
| SA10351SC | | Installation of decorative fiberglass fairing in accordance with Texas Skyways Inc. Master Drawing No. TSFG-100-1 dated November 18 2004 or later FAA approved revisions. | | Issued | | 2/4/2005 |
| SA10406SC | | Installation of a McCauley Model 1A170E/JHA7660 propeller and new 6.00X6 6 ply main tires in accordance with Alamo Aerospace Master Drawing List 1000 dated December 6 2004 or later FAA approved revision. An increase in the takeoff and max-continuous power to 180 horsepower and an increase in the max gross weight to 2550 pounds in accordance with the Airplane Flight Manual Supplement dated May 6 2005 or later FAA approved revision. | | Issued | | 5/6/2005 |
| SA10555SC | | ONE-ONLY STC: Installation of Aluminum Rudder Pedals and Portable Union Aviation Hand Control on Serial Number 17281100. | | Issued | | 8/11/2006 |
| SA105NW | | Mounting and wiring for occasional installation and use of Barnes Engineering Company airborne fire spotter system. | | Issued | | 4/30/1974 |
| SA1078WE | | Installation of Franklin 6A-335-B engine with McCauley 2A31C/84S-6 propeller using EDO 89-2000 floats. (172B 172C 172D 172E 172F 172G LAND OR SEAPLANE) | | Reissued | | 7/19/2000 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA10921SC | | Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators | | Issued | | 11/10/2008 |
| 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 |
| SA1119NW | | Installation of a Lycoming O-320-E2D engine and associated systems. | | Amended | | 4/10/1981 |
| SA1124GL | | Installation of a Shadin Co. fuel flow indicating system. | | Reissued | | 6/8/2006 |
| SA1150NW | | Installation of a 1976 Cessna 172 wing an updated right wing leading edge late model 172 dorsal fin and later model 172 cowl | | Issued | | 12/24/1980 |
| 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 |
| SA116EA | | Installation of Fram Part flow Lube oil filter model PB 55-1. | | Amended | | 9/11/1963 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA117EA | | Flow lube oil filter PB 55-1. | | Amended | | 9/11/1967 |
| SA1191NW | | Installation of Edo seaplane floats | | Issued | | 3/11/1981 |
| SA1196GL | | Install SAF-T-STOP auxiliary seat stop device. | | Reissued | | 6/15/2012 |
| SA1211EA | | Installation of EPA portable enviro-pod with Tensor-Hasselblad camera configuration. | | Reissued and Amended | | 2/1/1982 |
| 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 |
| SA1221SO | | Fabrication and installation of wheel fairings. | | Reissued | | 7/17/1989 |
| SA1221SW | | Mitchell automatic flight system AK312 consisting of Century I with optional omni tracker. | | Reissued | | 7/9/1984 |
| SA1225CE | | Installation of Lycoming O-320-E2D/ STC SE1226CE or O-320-D2G engine and McCauley 1C160/CTM 7557 or 1C160/DTM 7557 propeller | | Reissued | | 1/25/1996 |
| SA124EA | | Shur-Vent fuel tank filler cap. | | Issued | | 1/1/1960 |
| SA1253NW | | Installation of a Cee Bailey (one-piece) plexiglass windshield | | Issued | | 6/8/1981 |
| SA1258EA | | Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584) | | Amended | | 4/11/1983 |
| SA1261WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1279NW | | Installation of a Harrison Model AP07A006-03 oil cooler and associated parts on a Continental O-300-A engine | | Issued | | 7/27/1981 |
| SA1294SO | | Installation of an adjustable nine-inch trim tab on left aileron. | | Issued | | 11/13/1981 |
| SA12WE | | Installation of fiberglass wing tips. | | Reissued | | 5/4/2010 |
| SA1308WE | | Installation of Brittain Model CSA-1 stability Augmentation System. | | Issued | | 1/1/1960 |
| SA1311CE | | Chrome plated brake disc installation. | | Amended | | 6/20/1977 |
| 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 |
| SA1324CE | | Installation of Lycoming O-360-A1A engine and Hartzell HC-C2YK-1B/7666A-2 propeller. | | Issued | | 5/1/1977 |
| SA1334WE | | Installation of Franklin 6A-350-C2 engine and McCauley 2A31C/84S-6 propeller using Columbia Marine Inc. Kit No. 105. | | Reissued | | 7/19/2000 |
| SA1342GL | | Installation of Porsche Model PFM3200/NO3 engine and Hartzell Model BHC-JTYF-1C/B7421 propeller. | | Issued | | 12/2/1988 |
| SA1356GL | | Installation of Lycoming 0-320-D2J -D2G or -D1A. | | Reissued | | 11/1/2005 |
| 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 |
| SA1395SO | | Remove drain plug Cessna Part Number MS20913-10 or MS20913-1D from the fuel selector valve and replace with Part Number CAV-110D (MT-1072) or CAV-110H-4D (CM-1072) in accordance with installation instructions dated January 12 2004 or later FAA approved revision. See limitations. | | Amended | | 3/17/2004 |
| SA1396SO | | Remove drain plug Cessna Part Number AN814-3DL from the fuel selector valve and replace with CAV-180 (MT-1072-77) or CAV-180H-4 (CM-172-77) in accordance with instructions dated January 12 2004 or later FAA revisions. (*Model: C-172N Serial Nos.: 17261445 17267585 through 17269309 (1977 Model) 17261578 17269310 through 17271034 (1978 Model) (Except 17270050) 17271035 through 17272884 (1979 Model) 17270050 17272885 through 17274009 (1980 Model)) | | Amended | | 3/17/2004 |
