| 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 2) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 0:00 |
| SA00082SE | | Installation of a baggage door strut. | | Issued | | 4/29/1994 |
| SA00161BO (1 OF 3) | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 |
| 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 |
| SA00192DE | | Installation of a Master advisory system (MAS-1) to the existing aircraft annunciator system. | | Reissued | | 1/9/1996 |
| 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 |
| SA00266DE | | Gross weight increase from 5500 pounds to 5700 pounds. | | Amended | | 10/28/2013 |
| 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 |
| SA00430AT | | Installation of main landing gear torque links. | | Issued | | 3/3/1994 |
| 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 |
| SA00505LA | | Installation of Western Intl Aviation Inc double groove alternator pulley p/n W1A0000A40X-3 on right hand engine and idler pulley p/n W1A000040X-4 on right and left hand engines. | | Issued | | 5/22/1998 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00680SE (2 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00680SE (6 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00682SE | | Installation of a sunvisor system. | | Reissued | | 3/24/2003 |
| SA00729SE | | Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. | | Amended | | 11/30/2005 |
| SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
| 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 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 |
| SA00804SE | | Installation of an engine failure indicator system also referred to as a low Thrust Detector system. | | Amended | | 7/16/2000 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00943SE | | Installation of Merlyn Products Inertia Link on the above model aircraft per Merlyn Top Drawing List 91.50-TDL Revision A dated July 13 2001 and Merlyn Installation Instructions Report 91.50-1 Revision N/C dated June 12 2001 or later FAA approved revision of either of these documents. | | Issued | | 7/18/2001 |
| SA00944CH | | Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) | | Amended | | 6/20/2000 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01105WI-D (1 OF 2) | | Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). | | Amended | | 5/31/2007 |
| SA01111NY-D | | Installation of November Whiskey Inc. seat track connectors. | | Reissued | | 2/28/2002 |
| SA01147WI | | Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. | | Reissued | | 7/30/2012 |
| 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 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (1 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| 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 |
| 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 |
| SA01511SE | | Installation of MTV-14-B propellers | | Issued | | 2/18/2005 |
| 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 |
| SA01701SE | | Allow an increase in the takeoff maximum gross weight of the above model aircraft to 6850 pounds. | | Amended | | 11/8/2006 |
| SA01714WI (Page 1) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
| SA01786CH | | Replacement of certain BFGoodrich pneumatic deicer boots per SMR Technologies Inc. Installation Instructions as listed on AML No. SA01786CH or later FAA approved revision. | | Issued | | 3/5/2003 |
| SA01800SE (PG 1) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01828SE | | Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System | | Reissued | | 5/12/2011 |
| 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 |
| SA01988SE (PAGE 6) | | 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 |
| SA02019SE-D | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/13/2013 |
| SA02024NY | | Installation of constant speed hydraulically controlled variable pitch 4-blade MTV-14-B-C-F/CF (1) 188-30d propellers. | | Issued | | 11/12/2004 |
| 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 |
| SA02085AT | | Install Aero Crafters engine reheater kit. | | Issued | | 3/7/2000 |
| SA02110CH (PAGE 1) | | 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 |
| SA02203AK (PAGE 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| 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 |
| SA02242SE | | Fabrication of blended winglets | | Amended | | 3/12/2013 |
| SA02246AT | | Install propellers MTV-14-B-C-F/CF188-30d 4-blade propeller and spinner assembly. | | Reissued | | 11/13/2002 |
| SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
| SA02268CH (PAGE 1) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02293AK (2 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| 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 |
| 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 |
| SA09124AC-D | | Installation of S-TEC System Two Axis Automatic Flight Guidance System Model ST-606 with optional autotrim system. | | Amended | | 11/20/2001 |
| SA09422AC-D | | Installation of S-TEC Yaw Damper System Model ST-870. | | Issued | | 5/10/2000 |
| SA1007NW | | Installation of a low thrust detector system. | | Reissued | | 3/6/1998 |
| SA10236SC (1 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1041GL | | Install Egan Aviation air ambulance stretcher P/N 125 using Installation Kit P/N 800. | | Reissued | | 5/1/1997 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1089CE-D | | Installation of Collins Radio Group AP-106 autopilot system and inter- face with Collins FD-112 flight director. | | Amended | | 3/24/1976 |
| SA1090CE-D | | Installation of Collins Radio Group AP-107 3-axis autopilot system and interface with Collins FD-112 flight director indicator. | | Issued | | 3/24/1976 |
| SA1104CE-D | | Installation of Collins Radio Group AP-107 2-axis autopilot system and interface with Collins FD-112 flight director indicator. | | Issued | | 3/24/1976 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1139SO | | Installation of a Bendix FCS-870 automatic flight control system. The following options are included: pre-select altitude yaw damper and flight director system. | | Issued | | 3/13/1980 |
| SA1174CE | | Installation of Aero Space Controls Corp. 100 AMP alternator. | | Issued | | 10/31/1975 |
| SA1175CE | | Installation of Aero Space Controls Corp. air conditioning system. | | Issued | | 10/31/1975 |
| SA1184CE | | Installation of King KFC 200 2 axis(3 optional) Flight Control System with King KCS 55 (or -55A) compass and a King KI 255 (or -256) Flight Command Indicator or a KG 258 Attitude Horizon Gyro with a KC 292 Mode Controller. | | Reissued | | 2/28/2000 |
| SA1277CE | | Installation of Avcon Industries stretcher P/N 4001-101 or4001-102. | | Reissued | | 8/21/1990 |
| SA1305SO | | Installation of an adjustable nine- inch trim tab on the left aileron. | | Amended | | 1/12/1989 |
| SA1308SW | | Addition of toilet provision. | | Reissued | | 8/25/2005 |
| SA1327GL | | Install Cabin Door Ajar Warning System. | | Amended | | 8/10/1989 |
| SA1338SO | | Installation of under seat storage container in accordance with Southern Research & Development Drawing No. CA-3000 Revision No. 1 dated April 14 1982 or later FAA approved revisions. | | Reissued | | 6/27/2003 |
| SA1347SW | | Alternate vent for fuel pressure gages. | | Issued | | 7/22/1971 |
| SA1356SW | | Fabricate and install rib-wing fairing-inboard (flap attachment bracket). | | Issued | | 8/13/1971 |
| SA1362SW | | Storage drawers under cabin seats. | | Issued | | 9/3/1971 |
| SA1363SW | | Installation of pressure relief valves in fuel tanks. | | Issued | | 9/3/1971 |
| SA1382SW | | Modify two passenger seats to face aft. | | Reissued | | 8/25/2005 |
| SA1391SW | | Dual hydraulic pump. | | Issued | | 11/12/1971 |
| SA1452SW | | Modfy Ted Smith control tube P/N A600128-3. | | Issued | | 3/30/1972 |
| SA1512WE (2 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 0:00 |
| SA1530CE-D | | Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director installed under STC SA1184CE. | | Reissued | | 2/28/2000 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1608NM | | Installation of an auxiliary fuel tank system. | | Amended | | 11/1/1998 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1658NM | | Installation of engines and propellers with options of intercooler and maximum takeoff weight increase. | | Amended | | 1/9/2001 |
| SA1664NM | | Installation of engine driven air conditioning compressor. | | Reissued | | 11/27/2001 |
| SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
| SA1720GL | | Installation of wastegate actuator filter kit. | | Reissued | | 9/2/1992 |
| SA1777CE-D | | Installation of KAP 150 two-axis or KFC 150 two-axis flight control system with optional third (yaw) axis and optional KAP 297B Vertical Speed and Altitude Selector. | | Reissued | | 2/28/2000 |
| SA1797SW | | Mitchell automatic flight system AK459 consisting of Century I auto-pilot with optional omni tracker. | | Reissued | | 7/16/1984 |
| SA2121NM | | Installation of a low pressure fuel boost pump system. | | Amended | | 11/1/1998 |
| SA2143NM | | Installation of Vortex generators fairings rudder seals stall strips and strakes. | | Amended | | 11/1/1998 |
| SA2207WE | | Installation of electrically-driven Freon air-conditioning system | | Reissued | | 5/17/2013 |
| SA2336WE | | Installation of Prestolite 70 amp alternators (Avco Lycoming P/N78314) in lieu of existing 50 amp alternators. | | Reissued | | 5/1/1991 |
| SA2346WE | | Installation of turbocharger overboost protection. | | Reissued | | 5/1/1991 |
| SA2357WE | | Installation of auxiliary hydraulic pump. | | Reissued | | 3/10/2009 |
| SA2367WE | | Installaton of Prestolite 70 amp alternators (Avco Lycoming P/N78314). | | Reissued | | 5/1/1991 |
| 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 4) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2612NM | | Installation of fire resistant fuel and oil lines. | | Amended | | 11/1/1998 |
| SA2655WE | | Installation of auxiliary hydraulic pump option. | | Reissued | | 5/1/1991 |
| SA2664WE | | Modification of fuselage structure for pressurization to 3.20 psi operating pressure and installation of pressurization system. | | Reissued | | 5/1/1991 |
| SA2693NM (PAGE 2) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 0:00 |
| SA2714SO | | Installation of Mallen Aerospace Corp. (MACO) engine turbocharger exhaust Y pipe and turbocharger V clamps. (PA-60-601P (AEROSTAR 601P) TURBOCHARGED ONLY) | | Issued | | 3/9/1990 |
| SA2717SO | | Removal of turbochargers previously installed by STC SE6WE and installing modified exhaust tailpipe. | | Amended | | 8/29/1990 |
| 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 |
| SA3029SW-D | | Mitchell automatic flight system AK521 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/20/1984 |
| SA3030SW-D | | Mitchell automatic flight system AK522 or AK522RD consisting of Century IV autopilot or Century IV flight director autopilot with optional remotive annuciator panel. | | Reissued | | 6/20/1984 |
| SA3033SW-D | | Mitchell automatic flight system AK455 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 8/16/1984 |
| SA3343SW-D | | Mitchell automatic flight system AK800/FD consisting of Century41/flight director autopilot. | | Reissued | | 9/21/1983 |
| SA3370WE | | Installation of Silver Instruments fueltron IIIG or IIIP digital fuel flow and totalizer system. (PA-60-601P (AEROSTAR 601P) s/n 60-0266-XX and up and those aircraft with previously installed option #108) | | Issued | | 6/20/1979 |
| SA3372SW-D | | Automatic flight system YK877 consisting of yaw damper system. | | Reissued | | 8/24/1983 |
| SA3589NM | | Installation of Machen Inc. intercooler engine as modified by STC SE3590NM optional Hartzell HC-C3YR-2UF/FC8468DB-14 propellers. | | Amended | | 11/1/1998 |
| SA35GL | | Install Cleveland Acft Products wheel and brake conversion kit P/N 199-51. | | Reissued | | 10/28/1980 |
| SA3643WE | | Installation of vertical tail floodlight. | | Reissued | | 2/28/1980 |
| SA3719SW | | Installation of Lycoming IO-540-AA1A5 engines Hartzell HC-CY-2UF/FC-8468/8R propellers and two Ray-Jay 103599-02 turbochargers on each engine to maintain maximum continuous cruise power. (PA-60-601 (AEROSTAR 601) B) | | Issued | | 1/6/1987 |
| SA3770WE | | Installation of Silver Instruments fueltron IIIG or IIIP digital fuel indicating system. | | Reissued | | 4/29/1991 |
| SA3862NM Page 2 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA3884WE | | Installation of cabin door pneumatic spring counterbalance. | | Reissued | | 7/15/1988 |
| SA4005NM (PG 1) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4009NM | | Installation of the Merlyn Products induction air intercooler system on the Piper Aerostars equipped with Lycoming IO-540-AA1A5/-PIA5/-S1A5 engines. | | Amended | | 8/16/1989 |
| SA4021NM | | Installation of Machen temperature monitoring system. | | Amended | | 11/1/1998 |
| SA4029WE | | Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. (PA-60-602P (AEROSTAR 602P) | | Reissued | | 1/30/1998 |
| SA4144WE | | Installation of 35 ampere-hour batteries. | | Issued | | 5/1/1980 |
| SA4156NM | | Installation of Meryln Products Inc. Induction Air Intercooler System(STC No. SA4009NM) new Rotomaster ME60 turbochargers and Hartzell HC-C3YR-2UF/FC6660 or HC-C3YR-2UF/ FC8468(D)-8 propeller. | | Amended | | 6/27/1994 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4307NM | | Installation of Hartzell (see STC) propellers and increase in maximum continuous power to 300 HP for existing Lycoming IO-540-K1F5 -K1J5 engines installed on the Model 600 and IO-540-S1A5 engine installed on the 601 and 601P models. | | Amended | | 11/1/1998 |
| SA4366NM | | Installation of Spoilers Inc. electric/hydraulic operated wing Spoiler System. | | Issued | | 10/18/1988 |
| SA4367NM | | Installation of Cleveland Model40-128/30-930 (wheel/brake) assembly. | | Issued | | 11/16/1988 |
| SA4389NM | | Installation of Precise Flight Inc. Series 200 Speedbrake System. | | Amended | | 11/7/2003 |
| SA443SO | | Installation of Bendix RDR-110 weather radar system per Bendix drawing 4009700 Rev. B. Installation of Norton AD4059KX-5 radome approved per STC SA845EA. | | Issued | | 9/25/1970 |
| SA444SO | | Installation of Bendix Model FCS 810 flight control system including flight director indicator DH 841( ). | | Amended | | 6/3/1976 |
| SA4472NM | | Installation of inflatable door seal. | | Amended | | 8/18/1983 |
| SA4485NM | | Installation of FC/FT-10 digital fuel flow indicating system. (PA-60-602P (AEROSTAR 602P) S/N 60-0266-XX AND UP) | | Issued | | 6/20/1988 |
| SA4718NM | | Installation of a pneumatic door seal pressure system. | | Amended | | 4/20/1999 |
| SA4724NM | | Installation of Cleveland brakes. | | Amended | | 4/20/1999 |
| SA4777NM | | Installation of Machen Inc. Oil Breather Separator System. | | Amended | | 4/20/1999 |
| SA4790NM | | Installation of Cleveland slotted brake disks and heavy duty brake linings. | | Amended | | 4/20/1999 |
| SA4798NM | | Installation of an Engine Fire Detection System in each nacelle. | | Amended | | 11/1/1998 |
| SA4827NM | | Installation of exhaust systems. | | Issued | | 1/11/1990 |
| SA4942NM | | Install Lycoming IO-540-AA1A5 or IO-540-S1A5(AE) engine as modified by STC SE4941NM with Rotormaster 600846-01/-02 or600803-01/-02 turbochargers. | | Issued | | 5/30/1990 |
| SA4951NM | | Installation of spoilers. | | Reissued | | 7/31/2013 |
| SA4976NM | | Installation of exhaust system tailpipe redesign. | | Amended | | 11/1/1998 |
| SA511GL | | Installation of a Shadin Model910502 910504 or 910514 fuel flow indicating system. | | Amended | | 2/14/1984 |
| SA5133NM | | Install turbocharger lubrication lines. | | Issued | | 3/6/1991 |
| 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 |
| SA5467NM | | Installation of acrylic window liners. (206 SERIES 402B0301 AND ON) | | Reissued | | 1/23/2004 |
| SA5492SW | | Install auxiliary fuel tank in baggage compartment. | | Reissued | | 5/1/1991 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| 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 |
| SA61GL | | Installation of radome kit P/N 4079KX or 4079X. | | Amended | | 10/12/1984 |
| SA693CE | | Replace existing engine induction air filter with AC Spark Plug filter. | | Reissued | | 6/20/2000 |
| SA7160SW-D | | Installation of S-TEC System 65 two axis automatic flight guidance system with Autotrim Model ST-311. | | Amended | | 5/10/2000 |
| SA7168SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-312 with optional autotrim system. | | Amended | | 8/21/2000 |
| SA7204SW-D | | Installation of S-TEC System 60 Pitch Stabilization System Model ST-454 with Optional Automatic Electric Trim System. | | Issued | | 1/26/1990 |
| SA771CE | | Installation of Woodward propeller unfeathering accumulator kit number213702. | | Reissued | | 3/20/1992 |
| SA788WE | | Mixture monitor (exhaust gas temperature probe and gage). See FAA-approved eligibility list for models. | | Issued | | 1/1/1960 |
| SA798EA | | Installation of Monitair exhaust gas combustion monitor kit. | | Reissued | | 2/14/1972 |
| SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
| SA845EA | | Installation of radome kit P/N 4059KX or 4059X. | | Reissued | | 9/29/1975 |
| SA8705SW | | Installation of R25V0N Alternator Control Unit or R2510N Alternator Control Unit or V2510A Over Voltage Sensor. | | Amended | | 6/21/1996 |
| 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 |
| SA979NW | | Installation of a Lycoming engine Hartzell propellers Woodward propeller synchrophasers and unfeathering accumlators modified pressuriztion system to 4.25 psi Aero-Air Corporation air conditioning system 35 ampere hour batteries interior sound reduction package aerodynamic performance package and associated systems (See STC for models) | | Amended | | 4/10/1981 |
| SA980NW | | Installation of Lycoming engines Hartzell propellers aerodynamic performance package and associated systems. (See STC for model numbers). | | Amended | | 11/1/1998 |
| SA981NW | | Installation of 35 ampere hour batteries. | | Amended | | 11/1/1998 |
| SA982NW | | Installation of an interior sound reduction package. | | Amended | | 11/1/1998 |
| SA983NW | | Installation of a cabin air conditioner system. | | Reissued | | 11/27/2001 |
| ST01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| ST01468CH | | Installation of various SMR Technologies electrical propeller deicer models. | | Amended | | 7/25/2006 |
| ST01494LA (PG 2) | | Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. | | Reissued | | 8/30/2011 |
| ST02547AT (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
