| SA00068SE (PAGE 1) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 |
| SA00068SE (PAGE 2) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 0:00 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| 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 |
| 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 |
| 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 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA01026SE (PAGE 1) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01101AT | | Installation of Madras Air Service (MAS) wing tips. | | Issued | | 8/2/1996 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| 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 |
| 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 |
| SA01714WI (Page 1) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
| SA01800SE (PG 1) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| 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 |
| SA01944CH (2 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 0:00 |
| SA01988SE (PAGE 1) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 |
| 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 |
| 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 |
| 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 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| 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 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| 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 |
| SA1080SW | | Mitchell automatic flight system AK293 consisting of Century II autopilot with optional radio coupler. | | Reissued | | 7/9/1984 |
| SA1081SW | | Mitchell automatic flight system AK294 consisting of automatic stabilizer and optional omni tracker. | | Reissued | | 7/9/1984 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| 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 |
| SA1398WE | | Removal of right-hand door to permit aircraft to engage in special operations such as aerial photography parachute jumping etc. | | Issued | | 1/1/1960 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1635GL | | Installation of Cleveland main wheels 40-86A and brakes 30-56F. | | Issued | | 8/14/1991 |
| SA2040WE | | Installation of Brittain Industries B2C or ACS-1 flight control system. | | Reissued | | 10/20/1972 |
| SA2103CE | | Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. Intermixing with aviation gasoline also approved. | | Amended | | 6/23/1992 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| 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 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| 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 |
| 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 (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA593CH (2 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
| 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 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA798EA | | Installation of Monitair exhaust gas combustion monitor kit. | | Reissued | | 2/14/1972 |
| 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 |
| SA851GL | | Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index STC SE800GL approved. | | Surrendered | | 3/5/2004 |
