| SA00040LB | | Installation of a modified exhaust tail pipe. | | Amended | | 11/27/1996 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00063LA | | Installation of Acoustical/Thermal insulation. | | Reissued | | 1/5/2005 |
| 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 |
| SA00110BO | | Installation of Cessna 9910181-4 electric windshield heated panel. | | Amended | | 12/11/2001 |
| SA00155BO | | Installation of Aircraft Monitoring Systems LLC Annunciator System and ancillary components. Approval limited to installation on Cessna 340 serial number 206 ONLY. | | Issued | | 9/9/2002 |
| 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 |
| SA00228NY | | Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. | | Amended | | 1/24/1997 |
| SA00243BO (2 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 |
| SA00251DE | | Installation of a stainless steel heat shield assembly. | | Amended | | 6/21/2012 |
| 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 |
| SA00279NY | | Installation of .250 inch thick replacement windshield. | | Issued | | 2/7/1995 |
| 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 |
| SA00332DE | | Installation of Wastegate Exhaust Inlet elbow. | | Issued | | 1/14/1998 |
| SA00405WI | | Installation of starter engagement indication system. | | Issued | | 2/8/1996 |
| SA00419NY | | Installation of cockpit utility light. | | Reissued | | 12/31/2002 |
| SA00419WI | | Modifications to cabin chair to add underseat drawers. | | Issued | | 4/11/1996 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00476DE | | Installation of Aircraft Noise Control (ANC) System. | | Amended | | 7/29/2002 |
| SA00556DE | | Installation of a left-hand exhaust stack assembly. | | Issued | | 9/23/2004 |
| SA00571SE | | Replacement of certain BF Goodrich pneumatic deicer boots. | | Reissued | | 6/13/2001 |
| SA00680SE (3 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00709LA | | Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. | | Reissued | | 5/14/2002 |
| 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 |
| SA00763AT | | Installation of left hand and right hand fuel cell assemblies. (310 S/N PO240 and up 401 S/N 1 thru B1200 402 S/N 1 thru B1200) | | Reissued | | 4/29/2009 |
| SA00780SE (PAGE 2) | | 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 |
| SA00823CH | | Installation of various de-icer wire harnesses. | | Reissued | | 10/10/2002 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| 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 |
| SA00948CH | | Installation of various de-icer wire harnesses. (E90 modified by STC SA3593NM F90 modified by STC SA4131NM B200 modified by STC SA2698NM-S DHC-6 Series modified by STC SA3532NM) | | Amended | | 1/29/2004 |
| SA009574SC | | Installation of RAM series VII 335 horsepower engines increase takeoff weight to 6 390 pounds and increase landing weight to 6 075 pounds. | | Issued | | 2/29/2000 |
| SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
| 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 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01118WI | | Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 | | Amended | | 11/30/2013 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01158WI (1 OF 2) | | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | Amended | | 3/29/2005 |
| 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 |
| SA01210AT | | Installation of Composite Spinner. | | Amended | | 10/13/2000 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (2 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 |
| SA01284WI | | Installation of MT-Propeller Model MTV-14-D-C-F/CF188-30g hydraulic 4-blade variable pitch propeller.
);INSERT INTO stc_table VALUES ( | | Reissued | | 3/20/2007 |
| SA01330LA (PAGE 1) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 |
| SA01370SE | | Installation of BAS Inc. Shoulder Harness in accordance with BAS Inc. Drawing List which includes Installation Instructions and Instructions for Continued Airworthiness listed on FAA AML SA01370SE dated January 26 2004 or later FAA approved revision. | | Amended | | 12/2/2010 |
| SA01408AT | | Installation of National AirParts Model N300 alternators as replacement for belt-driven generators in accordance with National AirParts Inc. Document Number NAPI310 Cessna 310/320 Alternator Conversion | | Reissued | | 6/24/2011 |
| SA01420WI | | Installation of Garmin GNS 430A / 530A COMM/NAV/GPS Systems. Data required: (1) Scandinavian Avionics Design GmbH Drawing List 2027438-DL-02 Issue 2 or later EASA approved revisions. (2) Scandinavian Avionics Design GmbH Approved Aircraft Flight Manual Supplement Doc. 2027438-AM-02A Issue 1 and Doc. 2027438-AM-02B Issue 2 both approved by EASA under approval No. EASA.A.S.01389 dated 07-09-2005 or later EASA approved revision.
);INSERT INTO stc_table VALUES ( | | Issued | | 4/6/2007 |
| SA01436SE (1 OF 2) | | Cockpit sunvisor retrofit kit. | | 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 |
| 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 |
| SA01750SE | | Fabrication of Dahlia Doubler. | | Reissued | | 8/24/2011 |
| SA01751SE | | Fabrication of Panida Doubler. | | Reissued | | 8/24/2011 |
| SA01752SE | | Fabrication of Panida Doubler. | | Reissued | | 8/24/2011 |
| SA01800SE (PG 2) | | 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 |
| SA01860NY (3 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 |
| 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 3) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA02003NY | | Installation of SMR Technologies pneumatic deicer models. | | Reissued | | 8/29/2006 |
| 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 2) | | 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 |
| SA02095AK | | Installation of hourmeter airspeed switch. | | Issued | | 12/10/1997 |
| 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 1) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02217AK (2 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 0:00 |
| SA02239SE | | Installation of a Skymech rear spar replacement kit | | Issued | | 8/21/2012 |
| 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 |
| SA02293AK (1 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02366AT-D | | Installation of replacement fuel cell assemblies | | Reissued | | 4/16/2009 |
| SA02378NY | | ONE ONLY - Installation of a Remote Sensing Equipment Port S/N 340A0533 | | Issued | | 5/14/2007 |
| SA02503NY | | Battery Relocation. | | Issued | | 1/23/2008 |
| SA02510NY | | Installation of a 4-blade MT-Propeller Model MTV-14-D-C-F/CF188-30g propellers | | Issued | | 2/20/2008 |
| 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 |
| SA02546NY | | Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1090-1 | | Issued | | 7/9/2008 |
| SA02547AT (PG 2) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| SA02634AT-D | | Installation of fuel cell modifications consistent | | Reissued | | 4/16/2009 |
| SA02696CH | | Replaces Southwind combustion heater 84720D for Cessna 340 340A S/N 340A-0001 thru 340A-0200 w/SA03118NY turbine conversion and C&D Associates combustion heater Kit 32 P/N CD14076K32 or replaces Janitrol combustion heaters 02E17-2 13E55-2(EL) for Cessna 340A S/N 340A-201 and up w/SA03118NY turbine conversion and C&D combustion heater Kit 32 P/N CD14028K32 | | Issued | | 8/16/2012 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 5) | | 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 |
| SA03074CH | | Installation of the Hartzell Engine Technologies turbocharger Model TE06 (P/N 406610-0018) with optional wastegate (P/N 490001-0000) on TCM engine model TSIO-470-B -C -D equipped on Cessna model 320 airframe in accordance with Turbo Solutions Installation Instructions Revision 3 FAA approved on 2/22/2012 and Drawing List No. 4 Revised on 11/12/2010 or later FAA approved revision. | | Issued | | 2/22/2012 |
| SA03118NY | | Installation of Rolls-Royce 250 B17F/2 turbine engines Hartzell HCB3TF7A/T9212DNK7 propellers and associated structures and equipment | | Issued | | 7/19/2012 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09016AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-594 with optional autotrim system. | | Amended | | 5/11/2001 |
| SA09355AC-D | | Installation of S-TEC system 20/30 single and two axis automatic flight guidance system. | | Issued | | 4/14/1998 |
| SA09357AC-D | | Installation of S-TEC System 30 alt altitude hold system. | | Issued | | 4/13/1998 |
| SA09472SC | | Conversion of existing Cessna air conditioning system from R12 to R134a refrigerant. | | Amended | | 2/14/2000 |
| SA09499AC-D | | Installation of S-TEC System 40X/50X Single and Two Axis Automatic flight Guidance Systems Model ST-790-40X/50X. | | Issued | | 6/30/2000 |
| SA09544SC | | Installation of a wastegate in-line oil strainer. Required placard P/N 1737-9 located on screen housing P/N 9052V states: RAM RECOMMENDS WASTEGATE IN-LINE OIL STRAINER SHOULD BE REPLACED AT EVERY OIL FILTER CHANGE. FAILURE TO DO SO MAY RESULT IN REDUCTION OF TURBO BOOST. USE REPLACEMENT STRAINER AND O-RING KIT P/N EK9052V. | | Reissued | | 10/8/2001 |
| SA09574SC-D | | Installation of RAM Series VII 335 horsepower (hp) series increase takeoff weight to 6 390 pounds andincrease landing weight to 6 075 pounds. | | Reissued | | 9/11/2008 |
| SA09655SC | | Installation of RAM Induction Equalized Fuel Nozzle Set. | | Amended | | 9/20/2002 |
| SA09774AC | | Replacement of certain Goodrich pneumatic deicer boots | | Issued | | 11/9/2012 |
| SA09971SC-D | | Installation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellers | | Reissued | | 9/11/2008 |
| SA1-620 | | Kit No. 2014X for 12-inch RCA AVQ-45 AVQ-47 AVQ-50 AVQ-55 and 12-inch Collins WP-103 radar antenna. | | Reissued | | 7/6/2005 |
| SA1007NW | | Installation of a low thrust detector system. | | Reissued | | 3/6/1998 |
| SA1015SO | | Installation of Bendix FCS-870 automatic flight control system including manual electric trim and optional flight director system. | | Issued | | 8/10/1978 |
| SA101SO | | One right-hand and two left-hand single seats. | | Reissued | | 11/29/1984 |
| SA10236SC (2 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1025SO | | Installation of a Bendix NP-2041A area navigation computer programmer. | | Issued | | 10/4/1978 |
| SA103RM | | Installation of exhaust turbo connector P/N 30477-3 | | Amended | | 11/28/1990 |
| SA104EA | | L-2C autopilot slave cables around existing approved camera opening in lower surface of fuselage. | | Issued | | 1/1/1961 |
| SA1062CE | | Installation of Collins AP-107 autopilot. | | Amended | | 3/15/1976 |
| SA1078GL | | Installation of Great Lakes windshield P/N W-2070 W/T-2070 or WK-2070. | | Reissued | | 1/23/2007 |
| SA107GL | | Conversion of oil lubricated de-ice pumps and related hardware to Airborne dry air pump 400 series conversion kits. | | Issued | | 1/23/1976 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA110GL | | Install Cleveland conversion kit P/N 199-64. (320 SERIES S/N S 0001-D9999 320E0001-F9999) | | Amended | | 4/1/1981 |
| SA110RM | | Modify Cessna exhaust system by replacement of the inter-cylinder expansion joints with a slip fit joint. | | Issued | | 8/17/1977 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1133GL | | Install Egan Aviation air ambulance stretcher P/N 125 using Installation Kit P/N 801. | | Reissued | | 5/1/1997 |
| SA1175WE | | Installation of one-piece windshield. | | Reissued | | 6/25/2001 |
| SA117CE | | L-2C autopilot. | | Issued | | 1/1/1960 |
| SA119SO | | Installation of passenger seats. | | Reissued | | 11/29/1984 |
| SA1263NW | | Installation of Olin Industries cloud seeding equipment | | Reissued | | 7/22/1988 |
| SA1276CE | | Installation of King KFC 200 2-axis (3 optional) flight control system with a KI 255 (or -256) flight command indicator or KG-258 attitude horizon gyro and a KC-292 mode controller. | | Reissued | | 2/28/2000 |
| SA127SW | | Install auxiliary baggage compartment and adjustable seat modification | | Reissued | | 11/5/2012 |
| SA128GL | | Replace existing asbestos or bellows exhaust seal with slip joint. | | Reissued | | 10/9/1987 |
| SA1302CE | | Install Enk Aviation fire suppression system. | | Amended | | 7/28/1981 |
| SA130CE | | L-2C autopilot. | | Issued | | 1/1/1960 |
| 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 |
| SA1357CE | | Chrome-plated brake disc installation. | | Issued | | 1/13/1978 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1441SW | | Mitchell automatic flight system AK367 consisting of Century III autopilot with optional automatic pitch trim radio and glide slope couplers. | | Reissued | | 7/10/1984 |
| SA1442SW | | Mitchell automatic flight system FD/AP282-367 consisting of flight director/autopilot with automatic electric trim. | | Reissued | | 7/10/1984 |
| SA1447GL | | Installation of on-board engine analyzer system. | | Amended | | 5/18/1992 |
| SA1452WE | | Installation of Brittain Model B-4A flight control system. | | Reissued | | 7/2/2013 |
| SA147CE | | Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. | | Issued | | 1/1/1960 |
| SA1494SW | | Installation of Mitchell flight director remote annunciator Model AK375. | | Amended | | 7/10/1984 |
| SA14GL | | Installation of detachable lead strap propeller deicers. | | Reissued | | 3/1/1996 |
| SA150GL | | Install Norton Company radome Kit No. 4131X. | | Amended | | 3/28/1978 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1551CE-D | | Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with flight director installed under STC SA1276CE. | | 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 |
| SA1604WE | | Installation of Brittain B-5 flight control system. | | Reissued | | 6/14/2013 |
| SA1626NM Page 1 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1642WE | | Modification of exhaust system components. | | Amended | | 12/7/1973 |
| SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
| SA16RM | | Installation of freon type air conditioner. | | Reissued | | 5/17/2013 |
| SA1847WE | | Installation of Brittain Up-Command Signal Adapter Kit. | | Reissued | | 10/20/1972 |
| SA186NW | | Installation of Continental TSIO-520-J engine. | | Reissued | | 7/22/1988 |
| SA1880WE | | Installation of Brittain Industries Inc. Model B2C Flight Control System | | Reissued | | 2/6/2013 |
| SA1881SW | | Installation of Continental TSIO-520-J and increase take-off power to 310 h.p. | | Reissued | | 11/29/1984 |
| SA1883SW | | Install Hartzell synchrophase system. | | Reissued | | 11/29/1984 |
| SA1904SW | | Installation of additional auxiliary transfer tanks. | | Reissued | | 11/29/1984 |
| SA193RM | | New slip joint exhaust manifold. | | Issued | | 12/20/1979 |
| SA1979SW | | Installation of in-line fuel pumps for auxiliary tanks. | | Reissued | | 11/29/1984 |
| SA1BO | | Installation of Safeway Model7009-1 deicer kit. | | Reissued | | 5/9/2003 |
| SA2-1533 | | Installation of windshield wiper. | | Reissued | | 1/31/1997 |
| SA2-903 | | Manufacture and installation of 1/4 inch thick plexiglass windshield | | Reissued | | 5/1/1973 |
| SA2082WE | | Installation of two Lycoming TIO-540-A2B or | | Reissued | | 7/31/2012 |
| SA20GL | | Installation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO) | | Reissued | | 4/30/2007 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2122WE | | Installation of two Lycoming TIO-540-A2B turbocharged engines and two Hartzell HC-E3YR-2/C8468-6R propellers or installation of Lycoming TIO-540-J2BD or | | Reissued | | 7/31/2012 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2195SO | | Installation of Aero Safe standby vacuum system. | | Issued | | 10/16/1987 |
| SA2242SW | | Installation of Continental TSIO-520J engines | | Reissued | | 7/31/2012 |
| SA2339WE | | Installation of exhaust bellows. | | Issued | | 4/12/1971 |
| SA2346SW | | Installation of Teledyne TSIO-520-N or J or -NB engines and McCauley or Hartzell propellers. | | Reissued | | 10/8/2001 |
| SA2346SW-D | | Option 1: Install Teledyne Continental Motors Model TSIO-520-J engines (310 horsepower).
);INSERT INTO stc_table VALUES ( Option 2: Install Teledyne Continental Motors Model TSIO-520-N or | | Reissued | | 2/20/2008 |
| SA234EA | | Installation of Chamberlain 2310K-B series radome kit. | | Amended | | 3/11/1970 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA237SO | | Modification of the control wheel. | | Reissued | | 11/29/1984 |
| SA2404WE | | Consolidation of STC | | Reissued | | 9/30/2011 |
| SA240WE | | Consolidation of STCs SA355CE and SA362CE into one STC having MASTER ELIGIBILITY LIST - amended to include improved power supply assembly and subchassis timer assembly for Twilighter MK III high intensity supplementary lighting system. | | Issued | | 8/16/1971 |
| SA2423CE | | Installation of Med-Flite Inc. P/N 4001-201 or 4001-202 stretchers. | | Issued | | 10/11/1988 |
| SA2440SW | | Installation of airstair door saver. | | Reissued | | 3/5/2012 |
| SA2483SW | | Increase seating capacity on aft baggage shelf for a total of 7 occupants. | | Reissued | | 10/8/2001 |
| SA250CE | | Installation of Woodward electronic propeller synchraphaser system. | | Reissued | | 4/30/2007 |
| SA2513CE | | Installation of wing nacelle locker tanks and fuel transfer system. | | Issued | | 10/15/1997 |
| SA2534WE | | Installation of Cessna 310P-type fiberglass tail stinger and yaw reduction adapter. | | Amended | | 5/30/1973 |
| 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 2) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2592NM | | Installation of Hoskins Model CFS-2000A -2001A or FT-200 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA2655SW | | Addition of Hydro seal fluid additive to nose and main gear shock struts. | | Reissued | | 8/8/1980 |
| 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 |
| SA272EA | | Installation of Chamberlain 2014K-B radome kit as follows: Kit No. 2014K-B for Bendix RDR-100 or RDR-110 radar systems with 12-inch antenna and transmitter receiver unit. | | Reissued | | 7/6/2005 |
| SA2750SW | | Installation of Continental TSIO-520-E or -EB engine. | | Amended | | 9/20/2002 |
| SA2770SW | | Cleveland heavy duty brakes. | | Issued | | 5/9/1978 |
| SA281GL | | Install Cleveland conversion kit P/N 199-72. | | Reissued | | 10/28/1980 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA2844SW | | Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA285SO | | Installation of Lycoming IO-540- A1A5 powerplants and Hartzell HCA3XK-2B/7636D propellers. | | Reissued | | 11/29/1984 |
| SA2862SW | | CFS-2000 electronic fuel flow metering system. | | Reissued | | 1/30/1998 |
| SA2872SW | | Installation of wing nacelle locker tanks. | | Reissued | | 7/5/1990 |
| SA2903 | | Manufacture and installation of 1/4 inch thick plexiglass windshield. | | Reissued | | 5/1/1973 |
| SA2960NM | | Install stay put (seat position locking device). | | Amended | | 3/14/1986 |
| SA3-737 | | M-4 flight control system. | | Issued | | 1/1/1960 |
| 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 |
| SA302CE | | Installation of Hoskins High Intensity Position Light system. A supplemental condenser discharge (strobe) lighting system. Consists of red/green/white wing tip and tail position lights with or without white top and bottom fuselage lights plus a power supply. | | Reissued | | 9/30/2011 |
| SA3043SW-D | | Mitchell automatic flight system AK525 consisting of a Century IV autopilot or model AK525FD consisting of a Century IV flight director autopilot with optional remote annuciator. | | Reissued | | 6/22/1984 |
| SA3044SW-D | | Mitchell automatic flight system YK526 consisting of yaw damper system. | | Reissued | | 6/22/1984 |
| SA306CE | | GUARD System (gear up automatic response device). | | Amended | | 9/6/1966 |
| SA3082SW-D | | Installation of Mitchell automatic flight system AK557 consisting of Century III autopilot with optional radio and glide slope couplers. | | Amended | | 11/8/1984 |
| SA3164SW-D | | Install Mitchell automatic flight system AK485 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/7/1984 |
| SA3231WE | | Installation of recognition light assembly on horizontal stabilizer. | | Reissued | | 2/28/1980 |
| SA3239WE | | Installation of nacelle baggage lockers. | | Issued | | 7/27/1976 |
| SA3242WE | | Installation of pilot s and co- pilot s side vent windows. | | Issued | | 7/30/1976 |
| SA3376NM | | Installation of fowler flaps and a flap activated elevator up spring. | | Reissued | | 9/8/2005 |
| SA338SW | | Automatic pilot AK125. | | Issued | | 1/1/1960 |
| SA3485WE | | Installation of Continental TSIO-520-N or TSIO-520-NB engines and increase takeoff power to 310 h.p. | | Amended | | 4/26/1993 |
| SA3522NM | | Installation of Precise flight series 400 speedbrake system. | | Amended | | 3/10/2005 |
| SA3560NM | | Installation of ARNAV Systems FC-10/FT-10 digital fuel flow indicating system. (340 WITH CONT. TSIO-520-J ENGINES PER STC SA1881SW) | | Issued | | 12/19/1986 |
| SA3610WE | | Installation of Silver Instruments Fueltron IIIG or IIIP fuel flow and totalizer system. | | Reissued | | 4/29/1991 |
| SA362CE | | Description of Type Design Change: Install Hoskins Twilighter | | Reissued | | 9/30/2011 |
| SA3822WE | | Installation of 34-gallon auxiliary fuel tanks in each wing. | | Reissued | | 7/5/1990 |
| SA3850SW | | Install vacuum pump cooling shroud. | | Reissued | | 10/8/2001 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA3871SW | | Installation of camera port provisions. | | Reissued | | 8/15/2009 |
| SA3871WE | | Installation of vapor cycle air conditioning system. | | Issued | | 1/15/1980 |
| SA3923WE | | Installation of Lycoming TIO-540-R2AD engines. (340A S/NS 340A0001 THRU 340A0600) | | Reissued | | 7/5/1990 |
| SA396EA | | Installation of Radome Kit No. 2310X-R. | | Reissued | | 4/15/1976 |
| SA3RM | | Modification of engine exhaust stacks by replacement of expansion joint with slip fit joint. | | Reissued | | 10/1/1973 |
| SA4005NM (PG 2) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4011SW | | Installation of TSIO-520-N or TSIO-520-NB engines. | | Reissued | | 1/8/2001 |
| SA4012SW | | Installation of dual camera port view finder hole camera mount for RMKA8.5/23 and RMKA 15/23 intervalometer and autopilot servo relocation. | | Reissued | | 10/8/2001 |
| SA4024NM | | Replace the standard Cessna oil drain plug with a Bogert Aviation quick drain. | | Amended | | 4/12/1989 |
| SA4056WE | | Installation of 81.6 gallon auxiliary wing fuel tanks | | Reissued | | 11/1/2012 |
| SA409SW | | Automatic pitch trim AK137. | | Issued | | 1/1/1960 |
| SA4158NM | | Option 1: Installation of American Aviation Inc. intercooled engines as modified by Supplemental Type Certificate (STC) SE4159NM in accordance with American Aviation Inc. Top Drawing List TDL 063 dated July 8 2002 or later FAA approved revision. A copy of American Aviation Inc. Approved Flight Manual Supplement (AFMS) dated May 1 2003 or later FAA approved revision must be carried in the modified aircraft. Option 2: This installation may be installed with cowl scoops only in accordance with American Aviation Inc. Top Drawing List TDL 063 dated July 8 2002 or later FAA approved revision. No AFMS is necessary for this option.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( NOTE: This approval includes Cessna 340 series aircraft previously modified per the following STC | | Amended | | 5/1/2003 |
| SA4166NM | | Installation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506. | | Issued | | 1/25/1988 |
| SA4213SW | | Installation of repaired modified exhaust riser assemblies. | | Reissued | | 10/8/2001 |
| SA4222SW | | Mount collision avoidance lights in engine nacelle. | | Issued | | 10/29/1980 |
| SA4241SW | | Installation of Hartzell PHC-C3YF-2UF/FC7663D-2Q or PHC-C3YF-2UF/FC7663DB-2Q propeller. | | Reissued | | 10/8/2001 |
| SA4287WE | | Installation of inflatable door seal. | | Issued | | 12/15/1980 |
| SA42GL | | Install Norton Company radome kit No. 3060X. | | Amended | | 3/28/1978 |
| SA4331SW | | Revised exhaust system. | | Reissued | | 10/8/2001 |
| SA4376NM | | Installation of Spoilers Inc. electric/hydraulic operated wing spoiler system. | | Issued | | 11/4/1988 |
| SA446CE | | Installation of 30 gallon auxiliary fuel tank in baggage compartment. | | Reissued | | 6/23/2006 |
| SA455WE | | Single-piece windshield. | | Issued | | 1/1/1960 |
| SA471EA | | SAGA (Semi-automatic gear actuating) system. | | Issued | | 1/1/1960 |
| SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
| SA474NW | | Replace original split flaps with Fowler flaps. | | Reissued | | 9/8/2005 |
| SA490EA | | Installation of Chamberlain Radome Kit No. 3060K-B for Bendix radar RDR-100 or RDR-110 systems. | | Amended | | 3/28/1978 |
| SA492SW | | Emergency alternate air door actuation. | | Issued | | 1/1/1960 |
| SA4934NM | | Installation of vortex generators on the wing and vertical stabilizer and 5% take off gross weight increase. | | Amended | | 9/28/2004 |
| SA4948NM | | Installation of spoilers. | | Reissued | | 7/9/2013 |
| SA4980NM | | Installation of vortex generators on the wing and vertical stabilizer. (310H S/N 0001-0148) (310G S/N 0001-0156) (310I S/N 0001-0200) (310J S/N 0001-0200) (310Q S/N 0001-0900 0901 AND ON) (T310Q S/N0001-0900 0901 AND ON) | | Amended | | 10/2/1998 |
| SA4GL | | Installation of Bendix FCS-810 autopilot flight director system. | | Issued | | 10/18/1972 |
| SA502SO | | Installation of Bendix FCS-810 automatic flight control system including manual electric trim and optional flight director indicator DH-841. | | Amended | | 6/15/1976 |
| SA5101NM | | Installation of vortex generators on wings and vertical tail. | | Reissued | | 6/14/2012 |
| SA5137NM | | Installation of sun visor. | | Amended | | 2/22/2005 |
| SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
| SA518SO | | Installation of Continental IO-520-E derated engines and McCauley D3AF32C87/82NC-6 or -8 propellers. Modification to be accomplished in accordance with Colemill Enterprises Inc. Drawing AC5800 Rev. A and AC5801 Rev A and Installation Instructions dated 7 July 1972 and revised 21 August 1972. Owner | | Reissued | | 2/10/2011 |
| SA5198NM | | Installation of vortex gnerators on the wing and vertical tail and a5% increase in takeoff weight. | | Amended | | 6/21/1993 |
| SA521SW | | Automatic pilot AK157 and lateral guidance radio coupler AK123. | | Issued | | 1/1/1960 |
| SA537EA | | Installation of Radome Kit No. 3060X-R. | | Amended | | 8/25/1972 |
| SA5423SW | | Modification of engine cooling air louvres on top of cowling. | | Issued | | 10/8/2001 |
| SA544GL | | Installation of a Shadin Company fuel flow indicating system. | | Amended | | 12/11/1985 |
| 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 |
| SA55GL | | Install Airborne wing and tail pneumatic deice kit 710. (340 -0001 AND ON) | | Reissued | | 6/17/1986 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA568EA | | Installation of Grimes Manufacturing Company three light strobe kit P/N 34-0107-1. | | Reissued | | 6/4/2007 |
| SA574NW | | Installation of forward facing white lights (100 Watts) and clear plastic wing tip tank nose cone and associated systems | | Reissued | | 8/26/1991 |
| SA5757NM | | Installation of vortex generator system on wing and vertical stabilizer. | | Amended | | 6/17/1994 |
| SA5796SW-D | | Installation of Alcor Tru-Flow indicating system or SDI Hoskins fuel flow indicating system or Silver Instruments Fueltron fuel flow indicating system. | | Reissued | | 8/27/2008 |
| 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 2) | | 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 |
| SA621SW | | Installation of Mitchell automatic flight system Model AK198 consisting of Century III autopilot with optional automatic pitch trim automatic aileron stabilizer and radio coupler. | | Reissued | | 6/25/1984 |
| SA632WE | | B-4 flight control system including pitch assist PC-1 AH-1 altitude hold and NAV-1 navigation coupler. | | Reissued | | 10/1/1973 |
| SA660WE | | Installation of HRD-type fire extinguishing system. (AND STC SA111WE) | | Reissued | | 2/4/1987 |
| SA662WE | | Hi-Lo sensitivity adaptor BI-400 and autopilot with NAV-1 navigation coupler and heading lock. | | Reissued | | 10/1/1973 |
| SA664GL | | Install Cleveland Conversion Kit P/N 199-76 revision E. | | Issued | | 2/24/1983 |
| SA667SW | | Installation of Mitchell automatic flight system Model AK222 consisting of Century III autopilot optional command/automatic trim system automatic aileron stabilizer radio coupler and glide slope coupler. | | Reissued | | 6/25/1984 |
| 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 |
| SA7148SW-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-405. | | Amended | | 9/28/1992 |
| SA7149SW-D | | Installation of S-TEC yaw damper system Model ST-406. | | Amended | | 9/28/1992 |
| SA7171SW-D | | Installation of S-TEC system 60 two axis automatic flight guidance system Model ST-429 with optional automatic electric trim system. | | Amended | | 9/29/1992 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA722WE | | 30-gallon wing leading edge fuel tanks. | | Amended | | 9/2/1965 |
| SA7365SW-D | | Installation of TCM TSIO-520N or NB engines. Installation of Hartzell PHC-C3YF-2UF/FC7663DB-2Q propellers McCauley 3AF32C93/82NC-6.0 or McCauley 3AF32C505/82NEA-6.0 propellers. | | Reissued | | 8/28/2008 |
| SA7368SW | | Installation of an oil cooler baffle. | | Reissued | | 10/8/2001 |
| SA737SW | | Installation of Mitchell automatic flight system Model AK201 consisting of Century II autopilot with optional automatic aileron stabilizer and radio coupler. | | Reissued | | 6/25/1984 |
| SA7382SW-D | | Installation of TCM TSIO-520N or NB engines (modified by STC SE3714SW). Increase takeoff weight to 6140 pounds landing weight remains at 5975 pounds. Installation of McCauley 3AF32C93/82NC-6.0 or McCauley 3AF32C505/82NEA-6.0 propellers. | | Reissued | | 8/28/2008 |
| SA744SW | | M4B/C autopilot. | | Issued | | 1/1/1960 |
| SA7564SW | | Installation of throttle mixture and propeller control cables. | | Reissued | | 10/8/2001 |
| SA7781SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system model ST-199. | | Issued | | 12/6/1990 |
