| 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 |
| 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 |
| SA00192AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00197AT | | Installation of Appalachian carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00236BO | | Installation of a Lycoming IO-580-B1A engine/Hartzell HC-C3YR-1RF/F7693F propeller. This approval is considered inadequate for duplication in other aircraft. Limited to Commander Model 114 serial no. 14405. | | Issued | | 6/8/2006 |
| SA00241BO | | Installation of a Lycoming IO-580-B1A engine/Hartzell HC-C3YR-1RF/F7693F or HC-M3YR-1RF/F7693F propeller. | | Issued | | 7/27/2006 |
| 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 |
| SA00246BO | | Installation of a Lycoming IO-540-T4B5 engine. | | Issued | | 12/4/2006 |
| SA00249WI-D | | Installation of Bendix/King KFC 200 Automatic Flight Control System. For serial numbers 20003 20008 and above | | Reissued | | 2/28/2000 |
| 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 |
| 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 |
| SA00291BO | | Installation of a Lycoming IO-390-A1A6 engine and MT-Propeller MTV-12-B/188-59b propeller. | | Issued | | 11/12/2009 |
| SA00302BO | | Installation of a Lycoming IO-390-A1A6 engine and MT-Propeller MTV-12-B/188-59b propeller | | Issued | | 7/2/2010 |
| SA00306BO | | Change the horizontal stabilizer angle of incidence in accordance with Aerodyme Installation Instructions AD1225-01 Revision 1 dated December 15 2010 or later FAA approved revision. | | Issued | | 1/3/2011 |
| SA00326BO | | Installation of a Hartzell HC-C3YR-1RF/F7693F or HC-C3YR-1RF/F7693F-1 propeller | | Issued | | 10/5/2012 |
| SA00356DE | | Installation of modified Textron Lycoming engine equipped with turbo normalizing system. | | Reissued | | 4/12/2012 |
| 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 |
| SA00499SE | | Installation of a Hartzell HC-E3YR-1RF/F7392 propeller and C-3535-1(P) spinner. | | Amended | | 2/2/2002 |
| SA00556WI | | Installation of a functioning TKS ice protection system. | | Reissued | | 7/8/2008 |
| SA00680SE (5 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00769CH | | Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540 AEIO-540 and HIO-540 engines. | | Reissued | | 2/10/2009 |
| SA00780SE (PAGE 4) | | 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 |
| SA00817WI-D | | Installation of Bendix/King KFC 225 Automatic flight Control System. | | Reissued | | 2/28/2000 |
| SA00847WI | | Installation of a dual/single Garbin GNS 430 GPS/COM/NAV System. | | Issued | | 1/3/2000 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00865SE | | Installation of vortex generators on the wings horizontal tail surfaces and vertical fin. | | Issued | | 1/9/2001 |
| SA00893WI | | Installation of a Garmin GNS 530 VHF COM/NAV/GPS system. | | Issued | | 7/28/2000 |
| SA00929WI | | Installation of Garmin Model GTX 327 transponder. | | Issued | | 12/1/2000 |
| 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 |
| SA01026SE (PAGE 1) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01105WI-D (2 OF 2) | | Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). | | Amended | | 5/31/2007 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| 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 (4 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 |
| 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 |
| SA01437SE | | The manufacture of a Commander Sunvisor System in accordance with Rosen Sunvisor Systems Drawing List No. 1430000-DL Revision D dated
);INSERT INTO stc_table VALUES ( July 19 2004 or later Federal Aviation Administration (FAA) approved revision. The sunvisor system must be installed and maintained in accordance with Rosen Sunvisor Systems Installation and Continued Airworthiness Instructions Document 9050-0143-001 Revision C dated June 29 2004 or later FAA approved revision. | | Issued | | 8/2/2004 |
| 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 |
| 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 |
| SA01647WI | | Installation of the Elevator Spar Outboard Hinge Bracket Assembly on the Commander 112 series and 114 series aircraft in accordance with Harrison Aero Drawing List DL-HA1050 Revision IR dated August 23 2011 or later FAA approved revisions. | | Issued | | 10/14/2011 |
| 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 (2 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 2) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01860NY (2 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 2) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01923LA | | Installation of the P-1000 Digital Electronic Tachometer. | | Issued | | 1/23/2007 |
| 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 |
| SA01988SE (PAGE 4) | | 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 |
| SA02183LA | | Installation of Door Gas Springs in accordance with FAA approved Master Drawing List FIV-1000 Revision B | | Amended | | 8/3/2011 |
| SA02203AK (PAGE 2) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| 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 |
| 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 |
| 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 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02532AT | | Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. | | Issued | | 6/5/2002 |
| SA02547AT (PG 2) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| 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 |
| SA09195AC-D | | Installation of S-TEC System 55 Two Axis Automatic flight guidance system Model ST-658 with Optional Autotrim System. | | Amended | | 5/23/2001 |
| SA09258AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-713-20/30. | | Amended | | 11/16/1998 |
| SA09259AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-714. | | Amended | | 10/12/1998 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA09632AC | | Installation of the hydraulically controlled variable pitch 3-blade MTV-9-B/190-18b propeller in accordance with installation instruction No. E-551-E dated July 19 2002 or later FAA approved revision. FAA approved Airplane Flight Manual Supplement E-842-E dated September 29 2004 or later approved revision is required. | | Issued | | 10/4/2004 |
| SA09832SC | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-658. | | Issued | | 10/31/2000 |
| 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 |
| SA10442SC | | Installation of Chelton Aviation Corporation (CAC) AP-3C autopilot. | | Issued | | 9/12/2005 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1229CE | | Installation of King KFC-200 2 axis(3 optional) flight control system with KCS 55/55A compass and 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 |
| SA1245SO | | Installation of an adjustable trim tab on the left aileron. | | Issued | | 6/29/1981 |
| SA1389GL | | Installation of Pamco emergency backup pneumatic system. (114A S/N 14350 AND AFTER) | | Issued | | 6/23/1989 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1502SW | | Mitchell automatic flight system AK364 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/10/1984 |
| SA1503SW | | Mitchell automatic flight system AK 363 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 7/10/1984 |
| SA1504SW | | Mitchell automatic flight system AK362 consisting of Century III autopilot with optional command/ electric pitch trim optional radio and glide slope couplers. | | Reissued | | 7/10/1984 |
| SA1505SW | | Mitchell command/electric pitch trim system. | | Reissued | | 7/10/1984 |
| SA1512WE (2 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 0:00 |
| 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 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1728SW | | Cabin air scoop. | | Amended | | 3/14/1983 |
| SA2190NM Page 2 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2350NM Page 2 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA237GL | | Install edge landing lights. | | Reissued | | 9/12/2005 |
| SA243NW | | Installation of Lycoming IO-540 engine with 3-bladed Hoffman 3-bladed Hartzell or 2-bladed Hartzell propeller. | | Amended | | 11/1/1998 |
| SA2586NM (PAGE 3) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2677CE | | Installation of aileron and flap gap seals per Horton-STOL Craft Drawing List #15 with an approval date of August 18 1994 or later FAA approved revision. | | Amended | | 7/30/2003 |
| SA2683NM | | Installation of Precise Flight Inc. stand-by vacuum system (SVS) | | Amended | | 3/10/2005 |
| SA2687NM (PAGE 2) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 0:00 |
| SA2693NM (PAGE 1) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA2900WE | | Installation of Pathfinder autopilots. | | Reissued | | 9/30/1998 |
| SA3000SO | | Installation of Appalachian stainless steel brake discs No. 75-15A. | | Reissued | | 9/29/1995 |
| SA3001SO | | Installation of Appalachian Accessories stainless steel brake discs P/N 75-43. | | Reissued | | 9/29/1995 |
| SA300CE | | Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) | | Amended | | 5/14/1992 |
| SA3120SW-D | | Mitchell automatic flight system AK572 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 6/5/1984 |
| SA3121SW-D | | Mitchell automatic flight system AK473 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/5/1984 |
| SA3122SW-D | | Mitchell automatic flight system AK574 consisting of Century III autopilot with optional radio and glide slope. | | Reissued | | 6/5/1984 |
| SA3123SW-D | | Mitchell command electric trim system model AK582. | | Reissued | | 6/5/1984 |
| SA3155WE | | Installation of Pathfinder autopilot systems and/or pitch trim systems. | | Reissued | | 9/30/1998 |
| SA3308WE | | Modification of aileron control system by addition of aileron centering spring and installation of Pathfinder autopilot system and/or pitch trim systems. | | Reissued | | 9/30/1998 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3727WE | | Installation of Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA3778WE | | Installation of retractable landing lights in accordance with Metal Magic Inc. Rockwell Model 112 and 114 Wing Light Installation Procedures dated April 24 1978. Fred W. Jones FAA Approved Airplane Flight Manual Supplement dated November 8 1978 is required. | | Reissued | | 12/18/2003 |
| SA3787WE | | Installation of Model CFS-1000 -1001 FT-100 or FT-101 fuel flow ndicating system. | | Reissued | | 1/30/1998 |
| SA3862NM Page 2 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA3920WE | | Installation of Fueltron IG or IP or Fuelgard digital fuel flow and totalizer system. | | Reissued | | 4/29/1991 |
| SA4005NM (PG 3) | | 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 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4444NM | | Installation of McCauley B3D34C405/90DFA-13 propeller. | | Issued | | 7/9/1982 |
| SA4479NM | | Installation of FC/FT-10 digital fuel flow indicating system. | | Issued | | 6/20/1988 |
| SA4531NM | | Replace 100 watt landing light with a 250 watt lamp. | | Reissued | | 1/25/2006 |
| SA5154SW-D | | S-TEC System 60 two axis automatic flight guidance system ST-143 with optional automatic electric trim system. | | Amended | | 7/21/2000 |
| SA5155SW-D | | S-TEC yaw damper system ST-145. | | Amended | | 7/23/1987 |
| 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 |
| SA5167SW-D | | S-TEC System 60 pitch stabilizer system ST-144 with optional autotrim system. | | Amended | | 9/8/2000 |
| SA5187SW-D | | S-TEC System 60 single axis automatic flight. | | Issued | | 7/29/1983 |
| SA5202NM | | Installation of Avco-Lycoming engine model IO-360-C1D6 modified. | | Amended | | 3/6/1998 |
| SA5283SW-D | | S-TEC System 40/50 single and two axis automatic flight guidance system ST-217-40/50. | | Issued | | 3/9/1984 |
| 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 |
| SA5757SW | | Installation of Alcor tru-flow/ fuel flow/totalizer system. | | Amended | | 9/30/2002 |
| 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 (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 |
| SA7063NM | | Installation of acrylic window liners in accordance with FAA approved Drawing Lists. Drawing lists are listed on FAA approved Model List Number SA7063NM or later FAA approved revision. | | Reissued | | 10/17/2008 |
| SA7155SW-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-420. | | Amended | | 4/9/1996 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA771GL | | Install nose gear shimmey dampener P/N 1001 to replace Gerdes P/N A135-8. | | Amended | | 9/12/1997 |
| SA7801SW-D | | Installation of S-TEC manual electric trim system. | | Issued | | 7/16/1991 |
| SA7816SW-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-481. | | Issued | | 6/25/1992 |
| SA7817SW-D | | Installation of S-TEC yaw damper system Model ST-482. | | Amended | | 8/9/1995 |
| SA7820SW-D | | Installation of System 40/50 single and two axis automatic flight guidance systems Model ST-494-40/50. | | Issued | | 6/26/1992 |
| SA7822SW-D | | Installation of System 60 two axis automatic flight guidance system Model ST-496 with optional automatic electric trim system. | | Issued | | 7/20/1992 |
| SA7823SW-D | | Installation of S-TEC manual electric trim system Model ST-497. | | Issued | | 7/21/1992 |
| SA7855SW | | Installation of McCauley B3D32C419/82NHA-5 propeller. | | Reissued | | 3/3/2006 |
| 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 |
| SA8384SW-D | | Installation of S-TEC System 55/55X Two Axis automatic flight guidance system Model ST-527 with optional automatic electric trim system. | | Amended | | 10/31/2001 |
| SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
| SA8521SW-D | | Installation of a Century Automatic Flight System Model YK1044 consisting of a Century yaw damper. | | Issued | | 3/31/2000 |
| SA8534SW-D | | Installation of a Century Automatic Flight System Model AK1056. | | Amended | | 3/13/2003 |
| 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 |
| ST01085LA (PAGE 2) | | 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 (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
