| 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 |
| SA00143BO | | Installation of Avidyne Corporation model 700-00004-XXX-( ) multi-function display. | | Amended | | 6/25/2002 |
| SA00152BO | | Installation of Avidyne Engine Instrument Sensor Interface Unit part number 200-00031-000. | | Issued | | 6/25/2002 |
| 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 |
| SA00166BO | | Installation of Avidyne Corporation primary flight display p/n 700-00006-000 and Magnetometer/OAT sensor p/n 700-00011-000. | | Issued | | 2/21/2003 |
| SA00199BO | | Installation of Aerox Oxygen System in accordance with Aviation Oxygen Systems Inc. Drawing No. 4110-100 Rev. A dated June 19 2004 or later FAA-approved revisions. | | Amended | | 1/10/2006 |
| 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 (2 OF 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 |
| SA00282BO | | Installation of Avidyne Corporation Entegra Integrated Flight Display System | | Amended | | 4/4/2013 |
| 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 |
| SA00296BO | | Installation of: | | Amended | | 6/27/2013 |
| 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 |
| SA00780SE (PAGE 3) | | 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 |
| 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 |
| SA01009SE | | Installation of modified landing and taxi light system. Manufactured in accordance with Manufacturing Drawing List #1 Revision 1 dated August 27 2001 or later FAA approved revision. Installed and maintained in accordance with Installation Data List #1 Revision 1 dated August 27 2001 or later FAA approved revision. | | Issued | | 10/24/2001 |
| SA01016SE | | Installation of an engine control lever friction bolt retainer | | Issued | | 11/14/2001 |
| SA01040SE | | Installation of EMM-35 engine monitoring system installed using Arnav document Engine Monitoring Accessing Kit p/n 570-1210 Rev D dtd 10/18/02 or later rev. EMM-35 must be manufactured using TSO authorization for TSO C113. | | Amended | | 7/18/2002 |
| SA01071SE | | Installation of vacuum pump and battery cooling system. Installed and maintained in accordance with Installation Data List #1 Revision 0 dated February 10 2002 or later FAA approved revision. | | Issued | | 4/4/2002 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01170LA | | : Installation of Sandel Avionics SN3308 Navigation Display Unit in accordance with FAA Approved Sandel Avionics Master Drawing List Document No. ST8691LA-A-01 Revision B | | Reissued | | 11/10/2011 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01232SE | | Installation of a Semi-Portable Oxygen System. | | Amended | | 5/7/2007 |
| SA01234WI-D | | Installation of Bendix/King KMH 880 Multi-Hazard Awareness System or Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). | | Issued | | 4/16/2004 |
| SA01240SE (3 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 |
| SA01285SE | | The manufacture of a Cirrus sunvisor system | | Issued | | 10/27/2003 |
| SA01304WI | | Installation of the Concorde CB24-11M or CB24-11MXC Lead Acid Battery or RG24-11M or RG24-15M VRSLA Battery. | | Amended | | 11/1/2012 |
| SA01355WI-D | | Installation of the Bendix/King KR 87 ADB and/or the KN 62A DME. | | Reissued | | 4/4/2006 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| 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 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01695SE (2 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
| SA01708SE | | Installation of the fixed oxygen system. | | Amended | | 4/13/2010 |
| 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 2) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01861SE (PAGE 2) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01870CH | | Installation of McCauley Propeller Systems 3-blade propeller model D3A34C443/78CYA-0 with spinner no. D7779-3 assembly. | | Reissued | | 7/19/2006 |
| SA01933LA-D Page 1 | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
);INSERT INTO stc_table VALUES ( System | | Amended | | 4/1/2013 |
| SA01933LA (2 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
| 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 |
| SA02033AT (PAGE 6) | | 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 0:00 |
| SA02110CH (PAGE 2) | | 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 |
| 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 |
| SA02216SE | | Removal of mechanical link between engine throttle control and propeller RPM control. Installation of a separate RPM control lever linkage between Cirrus RPM cable/cam followers center console to accommodate three-lever configuration new knobs for all levers and new installation hardware (nuts bolts etc). | | Amended | | 6/15/2012 |
| 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 |
| SA02247SE | | Removal of rear seats and installation of cargo shelf and restraint system controlled by Cirrus Master Drawing List (MDL) TAG-CRT-205 Revision B dated October 23 2012 or later Federal Aviation Administration (FAA) approved revision. | | Reissued | | 12/21/2012 |
| 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 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| SA02329AK | | Installation of a fixed-mounted Max-Viz | | Amended | | 7/10/2012 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02547AT (PG 3) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| SA02558CH | | Installation of a L-3 Communications Avionics Systems SmartDeck Flight Guidance and Display System | | Issued | | 5/21/2008 |
| 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 |
| SA02924CH | | Installation of M-T Propeller model MTV-14-D/195-30( ) 4 bladed propeller. | | Amended | | 9/27/2013 |
| 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 |
| SA03407AT | | Installation of Alakai Passive | | Amended | | 11/18/2008 |
| SA03962AT | | Installation of Continental Motors Inc. TSIO-550-N engine on SR22 aircraft previously modified by STC SA10588SC | | Issued | | 4/19/2012 |
| SA09541AC-D | | Installation of S-TEC System 55X Automatic Flight Guidance System Roll Servo | | Amended | | 12/14/2006 |
| SA10195SC | | Installation of an engine driven vapor cycle air conditioning system | | Reissued | | 5/17/2013 |
| SA10236SC (1 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA10532SC | | Installation of XM Satellite Radio Wireless equipment. | | Issued | | 5/15/2006 |
| SA10588SC | | Installation of modified Teledyne Continental Motors IO-550-N engine equipped with turbonormalizing system. | | Issued | | 11/8/2006 |
| SA10675SC | | Installation of Teledyne Continental Motors IOF-550-N engine. | | Issued | | 3/15/2004 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA10925SC | | Installation of BAR Air LLC supercharged Teledyne Continental Motors IO-550-N Engines in Cirrus Design SR22 aircraft. | | Reissued | | 11/1/2010 |
| SA10980SC | | Installation of cowl louvers and louver covers Cirrus SR22 aircraft | | Issued | | 8/24/2010 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA2586NM (PAGE 3) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2693NM (PAGE 1) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 |
| SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
| 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 |
| SA593CH (2 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
