| 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 |
| 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 |
| 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 (1 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 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00478CH (PAGE 1) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| SA00478CH (PAGE 3) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| SA00695SE | | Replacement of certain Rotomaster and Rayjay scavenge pumps | | Amended | | 2/14/2003 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| 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 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| 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 (2 OF 2) | | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | Amended | | 3/29/2005 1:00 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (3 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 |
| SA01435DE | | Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine. | | Reissued | | 5/25/2011 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01473SE (1 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 |
| 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 |
| SA01800SE (PG 1) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01860NY (1 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 1) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01933LA-D Page 1 | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
);INSERT INTO stc_table VALUES ( System | | Amended | | 4/1/2013 |
| SA01933LA (1 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 |
| SA01988SE (PAGE 2) | | 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 1) | | Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. | | Amended | | 7/25/2008 |
| 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 |
| 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 (1 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 |
| SA02268CH (PAGE 1) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| 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 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 1) | | 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 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03286CH | | Install an electronic engine ignition system | | Issued | | 1/13/2014 |
| SA09145AC-D | | Installation of S-TEC System 55two axis automatic flight guidance system Model ST-615 with optional autotrim system. | | Amended | | 10/3/2001 |
| SA09365AC-D | | Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems Model ST-818-20/30. | | Issued | | 5/22/1998 |
| SA09367AC-D | | Installation of S-TEC system 30 alt altitude hold system Model ST-819. | | Issued | | 6/1/1998 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA1008WE | | Installation of Poly-Fiber covering material. | | Reissued | | 5/27/2003 |
| SA10126SC (1 OF 2) | | Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision. | | Amended | | 10/23/2003 |
| SA10236SC (1 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA108GL | | Installation of Continental IO-520D engine and McCauley D2A34C58/90AT-10 propeller. | | Issued | | 2/11/1976 |
| SA1195SW | | Mitchell automatic flight system AS309 consisting of Century I automatic aileron stabilizer with omni tracker. | | Reissued | | 7/9/1984 |
| SA1196SW | | Installation of Mitchell automatic flight system model AK309consisting of Century I automatic aileron stabilizer with omni tracker. | | Reissued | | 7/9/1984 |
| 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 |
| SA1351WE (PG 1) | | Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) | | Amended | | 8/19/1983 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA203GL | | Installation of McCauley2A34C66-N/S-90AT-12 propeller manufacturer s installation with instruction. | | Issued | | 12/8/1977 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2511NM | | Installation of inflatable door seal. | | Issued | | 8/27/1984 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA2586NM (PAGE 1) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 |
| SA2683NM | | Installation of Precise Flight Inc. stand-by vacuum system (SVS) | | Amended | | 3/10/2005 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA292GL | | Install Cleveland wheel 40-75E and brake 30-52M on main gear. | | Issued | | 1/31/1979 |
| SA294GL | | Install Cleveland wheel 40-97A and brake 30-63A. | | Issued | | 3/22/1979 |
| SA334SW | | Installation of InterAv Alternator. | | Reissued | | 7/20/1981 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3780WE | | Installation of Continental IO-502-K engine Hartzell propellers and associated installation components. | | Issued | | 11/29/1978 |
| SA4-1127 | | Ceconite 101 covering of entire aircraft | | Issued | | 1/1/1960 |
| SA4-1269 | | Full flow oil filter 30409A with element 1A0235. | | Issued | | 1/1/1960 |
| SA4-1283 | | Ceconite 103 covering of plywood portions of the aircraft. | | Issued | | 1/1/1960 |
| SA4-867 | | Autopilot. | | Reissued | | 10/1/1973 |
| SA4-883 | | Autopilot. | | Reissued | | 10/1/1973 |
| SA4-909 | | Autopilot. | | Reissued | | 10/1/1973 |
| SA4-925 | | Magnetic flight director 2000. | | Issued | | 1/1/1960 |
| SA4005NM (PG 1) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA486SW | | Automatic pilot AK143 AK143E and AK143E-3. | | Issued | | 1/1/1960 |
| SA489EA | | Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. | | Amended | | 12/5/2002 |
| 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 |
| SA5581SW | | Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. | | Amended | | 9/30/2002 |
| SA589WE | | Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. | | Reissued | | 10/5/1976 |
| 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 |
| SA6031SW-D | | Installation of S-TEC System 60two axis automatic flight guidance system Model ST-151 with optional automatic electric trim system. | | Reissued | | 10/12/1990 |
| SA6032SW-D | | Installation of S-TEC System 60 pitch stabilization system Model ST-152 with optional automatic electric trim system. | | Issued | | 8/1/1985 |
| SA6033SW-D | | Installation of S-TEC System 60single axis automatic flight guidance system Model ST-150. | | Issued | | 8/1/1985 |
| SA6034SW-D | | Installation of S-TEC System40/50 single and two axis automatic flight guidance systems Model ST-216-40/50. | | Issued | | 8/1/1985 |
| SA6035SW-D | | Installation of S-TEC manual electric trim system Model ST-273. | | Issued | | 8/2/1985 |
| 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 |
| SA630WE | | Installation of oil filter assemblies. (NAVION A AND B with optional engine) | | Reissued | | 8/29/1974 |
| SA645SW | | AK125 automatic flight system. | | Reissued | | 6/25/1984 |
| SA655NW | | Installation of a 12 volt 50 amp Ford alternator (Part no C5AF10300F) and an alternator adapter | | Issued | | 8/25/1978 |
| SA666NW | | Installation of Teflon control yoke bail or control yoke bushings. | | Amended | | 5/15/1996 |
| SA7965SW | | Application of fabric and polyurethane finishing system. | | Amended | | 7/15/1994 |
| SA798EA | | Installation of Monitair exhaust gas combustion monitor kit. | | Reissued | | 2/14/1972 |
| SA798WE | | Installation of George M. Adams DGA-2000 or Bodell BMI-2000 Wheel Assemblies in lieu of Firestone DFA180 wheel assembly. Firestone CFA252 brakes or Bodell BMI252brakes required with this installation. | | Reissued | | 6/25/2003 |
| SA800EA (PAGE 1) | | 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 |
| SA8075SW (PAGE 1) | | Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) | | Reissued | | 11/10/2003 |
| SA808SW | | Installation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW. | | Reissued | | 6/29/1984 |
| SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
| SA845SW | | Nose gear doors. | | Reissued | | 1/4/1979 |
| SA846SW | | Wing root fairings. | | Reissued | | 1/24/1979 |
| SA847SW | | Main landing wheel doors. | | Reissued | | 11/27/1978 |
| SA869SW | | Mitchell automatic flight system AK233 consisting of Century III autopilot with optional automatic pitch trim aileron stabilizer radio coupler glide slope coupler. | | Reissued | | 6/29/1984 |
| SA874SW | | Hartzell/Wren Beta System reverse pitch propeller. | | Reissued | | 9/20/1977 |
| SA903SO | | Reposition of fuel pump. | | Issued | | 7/30/1976 |
| SA981SW | | Installation of Manual Electric Trim AK276. | | Reissued | | 7/9/1984 |
| ST01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| 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 |
| ST02547AT (1 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
