| 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 |
| SA00192AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| 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 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 (2 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 |
| 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 |
| 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 |
| SA01375AT | | Installation of adapter ring P/N J1001-1 and fuel cap assembly (usher type) P/N UO-3. | | Reissued | | 3/1/2001 |
| 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 |
| 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 2 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03286CH | | Install an electronic engine ignition system | | Issued | | 1/13/2014 |
| SA09146AC-D | | Installation of S-TEC System 55two axis automatic flight guidance system Model ST-615 with optional autotrim system. | | Amended | | 10/3/2001 |
| SA09366AC-D | | Installation of S-TEC system 20/30 single and two axcis automatic flight guidance systems Model ST-818-20/30. | | Issued | | 5/22/1998 |
| SA09368AC-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 |
| SA09555SC | | Installation of Cablecraft cables: P/N 565-550-A-G-37.5 for throttle P/N 565-550-B-G-32 for mixture and P/N 565-550-C-G-69.5 for propeller. | | Issued | | 6/7/1999 |
| 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 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1118SW | | Installation of EDO-AIRE system Model 276.Mitchell manual electric trim | | Reissued | | 7/9/1984 |
| SA1195SW | | Mitchell automatic flight system AS309 consisting of Century I automatic aileron stabilizer with omni tracker. | | Reissued | | 7/9/1984 |
| SA1235SW | | Mitchell automatic flight system AK215 consisting of Century II autopilot with optional automatic aileron stabilizer and radio coupler. | | Reissued | | 7/9/1984 |
| SA1236SW | | Mitchell automatic flight system AK233 consisting of Century III autopilot with optional command/automatic pitch trim radio coupler and aileron stabilizer. | | Reissued | | 7/9/1984 |
| SA1257CE | | Installation of King KFC 200 2 axis flight control system with a KI 255 (or -256) flight command indicator or a KG 258 attitude horizon gyro with a KC 292 mode controller or stand alone electric trim. | | Reissued | | 2/28/2000 |
| SA1344CE | | Chrome-plated brake disc installation. | | Issued | | 8/18/1977 |
| SA1400GL | | Installation of Pamco emergency backup pneumatic system. | | Issued | | 8/4/1989 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1494SW | | Installation of Mitchell flight director remote annunciator Model AK375. | | Amended | | 7/10/1984 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1626NM Page 1 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1811SW | | Mitchell automatic flight system AK466 and AK466FD consisting of Century IV autopilot and Century IV flight director with electronic command/automatic pitch trim. | | Reissued | | 8/1/1984 |
| SA1812SW | | Mitchell automatic flight system AK465 consisting of Century III autopilot with optional electronic command/automatic pitch trim optional radio coupler and optional glide slope coupler. | | Reissued | | 8/1/1984 |
| SA2176SO | | Replacement of Cleveland brake discs P/N 164-15A or164-115A with Appalachian Accessories stainless steel brake discs P/N 75-15A. | | Issued | | 9/25/1987 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2510NM | | Installation of inflatable door seal. | | Issued | | 8/27/1984 |
| 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 |
| 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 |
| SA2831SO | | Installation of modified lower engine.cowling and addition nose gear doors. | | Amended | | 8/25/1994 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA3000SO | | Installation of Appalachian stainless steel brake discs No. 75-15A. | | Reissued | | 9/29/1995 |
| SA3047SO | | Replacement of air intake pipes with aluminum pipe assembly. | | Issued | | 10/28/1991 |
| SA3059SW-D | | Mitchell AK466 and AK466FD consisting of Century IV autopilot and Century IV flight director autopilot with optional annunciator. | | Reissued | | 8/16/1984 |
| SA3060SW-D | | Mitchell flight system Model AK465consisting of Century III autopilot with optional electronic command/ automatic pitch trim optional radio coupler and optional glide slope coupler. | | Reissued | | 8/16/1984 |
| SA3061SW-D | | Mitchell automatic flight system Model AK495 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 8/16/1984 |
| SA3071SW-D | | Mitchell automatic flight system AK546 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/20/1984 |
| SA3083SW-D | | Mitchell command electric trim AK545. | | Reissued | | 6/19/1984 |
| SA3267WE | | Modification of aileron control system by addition of aileron centering spring and installation of Pathfinder autopilot systems and/or pitch trim systems. | | Reissued | | 9/30/1998 |
| SA3461SW-D | | Installation of Century automatic flight system Model AK966consisting of a2010/2030/2031/2050/2051 autopilot. | | Amended | | 2/14/1997 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3571SW | | Installation of electrically driven standby vacuum pump. | | Reissued | | 4/6/2007 |
| SA3688WE | | 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 |
| SA4005NM (PG 1) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4302NM (PAGE 1) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4304WE | | Installation of Hoskins CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
| SA5158SW-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 |
| SA5159SW-D | | S-TEC System 60 pitch stabilization system ST-152 with optional automatic electric trim. | | Issued | | 5/2/1983 |
| SA5174SW-D | | S-TEC System 60 single axis automatic flight guidance system ST-150. | | Issued | | 6/29/1983 |
| SA5352SW-D | | Installation of S-TEC manual electric trim system Model ST-273. | | Issued | | 11/6/1984 |
| SA574SO | | Installation of Bendix FCS-810automatic flight control system including manual electric pitch trim and optional flight director indicator DH-841. | | Issued | | 2/1/1974 |
| 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 |
| 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 |
| SA7965SW | | Application of fabric and polyurethane finishing system. | | Amended | | 7/15/1994 |
| 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 |
| SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
| SA846SW | | Wing root fairings. | | Reissued | | 1/24/1979 |
| SA847SW | | Main landing wheel doors. | | Reissued | | 11/27/1978 |
| 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 |
| SA903SO | | Reposition of fuel pump. | | Issued | | 7/30/1976 |
| 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 |
