| SA00014WI | | Installation of stabilator tips. | | Issued | | 1/6/1993 |
| SA00015WI | | Installation of wing tips. | | Issued | | 1/6/1993 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| SA00230BO | | Installation of Lycoming Model O-360-A1F6 engine to replace existing Lycoming O-360-F1A6 engine. This approval is limited to the installation made in Cessna Model 177 Serial Number 17700380 ONLY. | | Issued | | 2/27/2006 |
| 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 |
| 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 |
| SA00382NY | | Installation of replacement windshields. | | Issued | | 12/7/1995 |
| SA00393SE | | Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. | | Issued | | 12/6/1996 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00419NY | | Installation of cockpit utility light. | | Reissued | | 12/31/2002 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| 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 |
| 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 |
| SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
| 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 |
| SA00790CH | | Installation of a Hoffman variostat two-blade propeller Model HO-V72L-A/VC180DU with Textron Lycoming O-320E2D engine. Approved for serial number 17701153 only. | | Issued | | 10/29/1997 |
| 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 |
| SA00895LA | | Installation of instrument panel. | | Reissued | | 5/14/2002 |
| SA00897WI | | Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. | | Issued | | 8/11/2000 |
| SA00908NY | | Installation of Fiberglass stabilator tips. | | Issued | | 11/6/1998 |
| 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 |
| SA00958SE | | Manufacture and installation of audio control panel in accordance with wiring diagrams specifications and photographs contained within the FAA project file. Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval for change in type design is limited to Cessna Model 177 Serial Numbers 17700123 and 17700674 only. | | Issued | | 8/22/2001 |
| SA01026SE (PAGE 2) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01033SE | | Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2162 Revision IR dated November 1 2001 and Installation Manual MA2163 Revision IR dated December 3 2001 or later FAA approved revisions. If more than five vortex generators are damaged or missing the aircraft is not airworthy. | | Issued | | 1/8/2002 |
| SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
| SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
| SA01105WI-D (1 OF 2) | | Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). | | Amended | | 5/31/2007 |
| 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 |
| SA01163AT | | Installation of Composite Spinner. | | Amended | | 10/13/2000 |
| SA01170NY | | Installation of NPX138N-XXX FM Transceiver. | | Amended | | 1/17/2007 |
| 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 |
| SA01224AT | | Installation of wheel hub cabs with valve stem access door. | | Amended | | 4/17/1998 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (2 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01280CH | | Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) | | Issued | | 8/29/2000 |
| 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 |
| 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 |
| SA01442WI | | Installation of Lycoming IO-360-A1B6D engine McCauley B2D34C207/78TCA propeller and associated systems modifications. | | Issued | | 6/14/2007 |
| 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 |
| SA01548SE | | Installation of a Lycoming O-320-E2D engine modified by STC SE3692SW. | | Issued | | 5/17/2005 |
| 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 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01692SE (Page 1 OF 2) | | Installation of a Garmin GMX 200 Multi-Function Display | | Reissued | | 10/3/2012 |
| SA01695SE (1 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
| 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 |
| 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 |
| SA01889NY | | Fabrication and installation of an FRP Lower Cowl Fairing. | | Reissued | | 8/3/2004 |
| 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 |
| 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 |
| 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 |
| SA02072AK | | Installation of hourmeter airspeed switch. | | Amended | | 11/14/1997 |
| SA02105AT | | Modification of engine exhaust system for improved engine performance by installation of a Laminar Flow System Extractor Exhaust System. | | Amended | | 8/25/2000 |
| SA02115AT | | Modification of engine exhaust system for improved engine performance by installation of a Laminar Flow System extractor exhaust system. | | Reissued | | 8/25/2000 |
| SA02119SE Page 1 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
| SA02153LA-D (Page 1) | | Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System | | Amended | | 12/16/2013 |
| SA02154AK (PAGE 1 ) | | Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. | | Amended | | 1/12/2005 |
| SA02203AK (PAGE 2) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02208AK | | Installation of Lycoming O-320-E2D modified engine. Limited to installation on model 177 serial number 01049 ONLY. | | Amended | | 7/22/2004 |
| 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 |
| SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
| SA02268CH (PAGE 2) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02268CH (PAGE 3) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02276AK | | Installation of AMSAFE Aviation Inflatable Restraints | | Amended | | 3/12/2013 |
| 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 |
| 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 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02446CH | | Installation of the Courtesy Light Kit. | | Issued | | 6/25/2007 |
| SA02547AT (PG 1) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 |
| SA02674AT | | Modification of engine exhaust system for improved engine performance by installation of Power Flow Systems Inc. Tuned Exhaust System per Master Drawing List PFS-13740-00 Revision IR dated: 06/05/03 or Master Drawing List PFS-13741-00 Revision IR dated: 11/26/03 and Installation Instructions Report PFS-13750-00 Revision A dated: 08/30/02 or Installation Instructions contained in Report PFS-13751-00 Revision IR dated: 11/26/03 or later FAA approved revision. | | Amended | | 12/4/2003 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 5) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02795AT | | Installation of a PXE7300SR In-Flight Entertainment System | | Issued | | 2/12/2004 |
| SA02867NY | | Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1088-1 in accordance with Lord Corporation Installation Drawing List Document No. SE-1088-IDL Revision IR dated 4/22/2008 or later FAA approved revisions. | | Issued | | 12/21/2010 |
| 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 |
| SA03108AT | | Manufacture of engine cowling fasteners in accordance with MilSpec Products Inc. Master Drawing List No. C177KDL Revision A dated February 22 2005 or later FAA approved revision. Installation of engine cowling fasteners in accordance with MilSpec Products Inc. Installation Instructions Document No. MS-C177C Revision A dated February 22 2005 or later FAA approved revision. | | Issued | | 5/24/2005 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09125AC-D | | Installation of S-TEC System 55 Two Axis automatic flight guidsance system Model ST-608 with optional autotrim system. | | Amended | | 4/30/2001 |
| SA09295AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-741-20/30. | | Issued | | 11/7/1997 |
| SA09299AC-D | | Installation of S-TEC System 20/30 single and two axis automatic Flight Guidance Systems Model ST-752-20/30. | | Issued | | 11/6/1997 |
| SA09335AC-D | | Installation of S-TEC system 30 alt altitude hold system. | | Issued | | 1/30/1998 |
| SA09388AC-D | | Installation of S-TEC manual electric trim system model ST-836. | | Amended | | 10/6/1998 |
| SA09433AC-D | | Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-783-40X/50X. | | Issued | | 3/23/2000 |
| SA09455AC-D | | Installation of S-TEC system 55 two axis automatic flight guidance system Model ST-878. | | Amended | | 10/23/2001 |
| 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 |
| SA1005SC | | Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. | | Issued | | 7/23/2002 |
| SA1008SW | | Installation of Lycoming O-360-A1A or O-360-A3A engine and Sensenich M76EM8S5-0-60 propeller. | | Amended | | 9/8/2009 |
| 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 |
| SA10222SC | | Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot in accordance with Master Drawing List No. MS-005-12 Rev. F dated February 3 2004 or later FAA approved revision. FAA approved Airplane Flight Manual MS-005-14 Rev. I. R. dated February 5 2004 or later FAA approved revision is required. | | Issued | | 2/5/2004 |
| SA10236SC (2 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1043SW | | Installation of Lycoming O-360-A1A or O-360-A3A engine and Hartzell Constant-Speed Propeller Model HC-C2YK-1B/7666A-2. | | Amended | | 1/26/2010 |
| SA1060CE | | Installation of wing leading edge cuffs and vortex generators on vertical stabilizer. | | Reissued | | 5/1/1977 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1261WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1320GL | | Installation of PAMCO Emergency Backup Pneumatic System. | | Issued | | 8/25/1988 |
| SA1347CE | | Chrome-plate brake disc installation. | | Issued | | 8/22/1977 |
| SA1371SW | | Wing leading cuff wing tips and upper surface flow fences. | | Amended | | 4/14/1983 |
| SA1400SO | | Remove drain plug Cessna Part Number MS20913-10 or MS20913-ID from the fuel selector valve and replace with CAV-110D (MT-1077) or CAV-110H-4D (MT-1077) in accordance with instructions dated January 12 2004 or later FAA revisions. (See page 2 for model serial numbers.) | | Amended | | 3/17/2004 |
| 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 |
| SA1440NM | | Installation of a Descent Rate Control (DRC) system (wing spoilers and speed brakes) including a pneumatic actuating system | | Issued | | 2/3/1982 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1545GL | | Installation of the MAC 170A frequency stability modification to King Radio Corp. KX 170A and KX 175 transceivers. | | Amended | | 12/4/1991 |
| SA1556GL | | Installation of Hartzell 3 bladed propeller model HC-C3YR-1RF/F7282 and associated spinner assembly no. A-2295-1 and mounting kit A-2476-7. | | Amended | | 1/6/1995 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1583SO | | Installation of Appalachian Accessories brake rotor P/N 75-27. | | Issued | | 3/7/1984 |
| SA1588WE | | Installation of supplemental exterior flashing lights. | | Issued | | 1/30/1968 |
| SA1607SW | | Mitchell command/electric trim system model AK419. | | Reissued | | 7/16/1984 |
| SA1608SW | | Mitchell AFS system AK420 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/16/1984 |
| SA1608WE | | Installation of Brittain Industries Inc. Model B2C Flight Control System | | Reissued | | 2/1/2013 |
| SA1609SW | | Mitchell AFS system AK421 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 7/16/1984 |
| SA1626NM Page 1 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1689NM | | Installation of a Lycoming IO-320-B1A Hartzell HC-C2YL-1BF-F7663-4 propeller and associated parts | | Issued | | 3/29/1983 |
| SA1760SO | | Installation of Appalachian Access. stainless steel brake rotors P/N 75-15C. | | Reissued | | 2/6/1995 |
| SA1761SO | | Installation of Appalachian Access stainless steel brake discs. | | Reissued | | 9/29/1995 |
| SA1778NM | | Installation of a descent rate control (DRC) system (wing spoilers and speed brakes) including pneumatic actuating system. | | Reissued | | 5/10/1984 |
| SA1978SO | | Installation of Appalachian Accessories stainless steel brake discs P/N 75-40. | | Reissued | | 2/6/1995 |
| SA1980SO | | Installation of Appalachian Accessories stainless steel brake discs P/N 75-40. | | Amended | | 1/14/1987 |
| SA2-1178 | | Replacement of right front seat with stretcher. | | Amended | | 11/14/2001 |
| SA2010CE | | Operation on unleaded and/or leaded automotive fuel. | | Issued | | 8/10/1984 |
| SA2067NM | | Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System | | Amended | | 7/11/2012 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2137SO | | Fabrication and installation of nose wheel fairings. | | Reissued | | 7/17/1989 |
| SA2162NM | | Installation of the Precise Flight stand-by vacuum system (SVS) | | Amended | | 11/7/2003 |
| SA2166NM | | 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 |
| 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 |
| SA2382SO | | Installation of Appalachian Accessories stainless steel brake discs. (182 SERIES THRU 182Q) | | Reissued | | 9/29/1995 |
| SA2457CE | | Installation of fuel inlets and caps. (177B S/N 17700001 THRU 17702752) | | Reissued | | 5/3/2004 |
| SA2536NM | | Installation of McCauley 2D3614-E/78KM-4 propeller. (177 AS MODIFIED PER STC SA906CE) | | Issued | | 11/20/1984 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA2577NM | | Installation of Lycoming 0-360-F1A6 (modified per STC SE2574NM) and Hartzell HC-C2YK-1BK/FY666A-2 | | Issued | | 6/7/1985 |
| SA2586NM (PAGE 2) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2619WE | | Installation of Pathfinder Model P1-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2620WE | | Installation of Pathfinder Model P2-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2654WE | | Installation of Pathfinder Model P2A( ) autopilot. | | Amended | | 7/3/1979 |
| 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 |
| SA2832SO | | Installation of a combination radio/throttle/gust lock. | | Amended | | 12/3/2001 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA2938NM | | Fabrication and installation of external hinged-plate spoilers and dive brakes. | | Amended | | 5/7/1986 |
| SA2960NM | | Install stay put (seat position locking device). | | Amended | | 3/14/1986 |
| 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 |
| SA316SO | | Carburetor ice detector. | | Amended | | 10/5/1966 |
| SA3180SW-D | | Mitchell automatic flight system AK420 consisting of Century I autopilot with optional omni tracker system. | | Reissued | | 6/18/1984 |
| SA3181SW-D | | Mitchell automatic flight system AK421 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/18/1984 |
| SA3286SO | | Installationof engine cowling and firewall fasteners. (177 S/N 00001 THRU 02752) (177 RG S/N 0001 THRU 1366) | | Amended | | 8/29/2001 |
| SA3318NM | | Installation of a Venting fuel cap and restricting adapter assembly. | | Amended | | 6/23/1988 |
| SA3861WE | | Installation of an air/oil separator. | | Reissued | | 9/28/2001 |
| 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 |
| SA4094NM | | Installation of Oilamatic engine preoiler. | | Amended | | 6/28/1991 |
| 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 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA4302NM (PAGE 1) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4359NM | | Installation of redesigned upper door hinge pin and retainer. | | Amended | | 5/17/1999 |
| SA466SO | | Removal of right entrance door of cabin for aerial photography. | | Issued | | 5/20/1971 |
| SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
| SA475CH | | Installation of Inline Air Filter Kit P/N CV1J4-C | | Reissued | | 1/15/2013 |
| SA477CH | | Installation of McCauley Propeller model B3D36C428/82NPA-6. | | Reissued | | 9/21/2005 |
| SA4964NM | | Installation of a NSA sunvisor system for the pilot and copilot. | | Reissued | | 3/24/2003 |
| 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 |
| SA516NE | | Installation of nose gear strut fairings. | | Issued | | 6/1/1987 |
| SA5304SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-245 with optional automatic electric trim system. | | Reissued | | 10/22/1990 |
| SA5317SW-D | | Installation of S-TEC System40/50 single and two axis automatic flight guidance systems model ST-243-40/50. | | Issued | | 5/10/1984 |
| SA5333SW-D | | Installation of S-TEC System 60 two axis flight guidance system Model ST-241 with optional automatic electric trim system. | | Reissued | | 3/10/1989 |
| SA5336SW-D | | Installation of S-TEC System 60 pitch stabilization system Model ST-242 with optional automatic electric trim system. | | Issued | | 9/5/1984 |
| SA5339SW-D | | Installation of S-TEC System 60 pitch stabilization system Model ST-246 with optional automatic electric trim system. | | Issued | | 9/11/1984 |
| SA5341SW-D | | Installation of S-TEC System 60 single axis automatic flight guidance system Model ST-244. | | Issued | | 10/2/1984 |
| SA5343SW-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-247-40/50. | | Issued | | 10/3/1984 |
| SA5346SW-D | | Installation of S-TEC System 60 single axis automatic flight guidance system Model ST-240. | | Issued | | 10/10/1984 |
| SA5358SW-D | | Installation of S-TEC manual electric trim system Model ST-258. | | Issued | | 12/5/1984 |
| SA545CE | | Installation of Lycoming O-360(180 h.p.) engine and new Hartzell Sensenich or McCauley propellers. Delete limitation pertinent to utility category operation. | | Amended | | 2/22/1989 |
| SA563CH | | Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. | | Reissued | | 2/10/2009 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5696NM | | Repair of the Cabin Door lower hinge | | Issued | | 3/20/1992 |
| SA5697NM | | Repair of upper hinge on the cabin door. | | Amended | | 8/4/2000 |
| SA5701SW | | Installation of electrically driven vacuum pump as a standby auxiliary pump to the existing instrument. | | Reissued | | 4/6/2007 |
| SA582NW | | Fabrication of replacement wire rope cable assemblies | | Issued | | 5/12/1978 |
| 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 (1 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 |
| SA601CE | | Install Hartzell Model HC-C2YK-1B/7666A-2 constant speed propeller. | | Reissued | | 1/28/1983 |
| SA6023NM | | Installation of an electronic digital engine tachometer Model P-1000. | | Reissued | | 1/14/2002 |
| SA602NW | | Installation of a Lycoming O-360-A1F6D engine McCauley B2D34C211/82PCA-6 propeller modified cowling and associated systems | | Issued | | 5/18/1978 |
| 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 |
| SA672NE | | Installation of fiberglass reinforced plastic nose landing gear wheel fairing P/N PD85-1101. | | Amended | | 8/30/1990 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA728NW | | Installation of vented fuel cap. | | Amended | | 10/10/1979 |
| 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 |
| SA800EA (PAGE 2) | | Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. | | Amended | | 7/6/2010 |
| 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 |
| SA803GL | | Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index STC SE800GL approves 87 minimum antiknock index. | | Surrendered | | 3/5/2004 |
| SA839NE | | Installation of William C. Roberts stainless steel brake discs P/N 201-195 SS 201-260 SS 201-440 SS 201-40 SS in lieu of Cessna carbon steel brake discs Cessna P/N B-30195 C164-26A C-30440 C164-40 respectively. | | Reissued | | 6/18/2002 |
| SA8432SW | | Installation of V25101 overvoltage sensor. | | Reissued | | 5/12/1998 |
| SA861SO | | Installation of portable hand control | | Reissued | | 11/15/1976 |
| SA86NW | | Installation of automatic carburetor alternate air control unit. | | Issued | | 12/28/1973 |
| SA890SW | | Medairco Automatic Fuel Alert F-2. | | Issued | | 1/1/1960 |
| 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 |
| SA902NE | | Installation of fiberglass reinforced plastic main anding gear wheel fairings P/N s 89-1102-16 and 89-1102-17. | | Issued | | 10/3/1991 |
| SA906CE | | Installation of Lycoming O-360-A1A180 hp engine and Hartzell HC-C2YK-1B/766A-2 or 7666-2 constant speed propeller. | | Reissued | | 8/5/1981 |
| 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 |
| SA956CE | | Installation of STOL kit (wing leading edge cuffs drooped tips and vortex generators). | | Reissued | | 5/1/1977 |
| 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 |
| 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 |
