| 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 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00143LA | | Installation of control yoke retainer lock. | | Issued | | 8/2/1996 |
| SA00176SE | | Installation of FLD-100C self contained hydraulic propeller pitch change system. | | Amended | | 1/2/2001 |
| SA00195AT | | Installation of carbon steel brake discs. | | Reissued | | 11/14/1994 |
| SA00199SE | | Modification of Beech 35-950116and/or 35-950118 exhaust stack assemblies by adding a slip joint to the middle riser of each exhaust stack assembly. | | Amended | | 10/19/1995 |
| SA00204NY | | Installation of .250 inch .312 inch or .375 inch thick one piece windshields (two piece windshield to one piece windshield conversion). | | Reissued | | 5/7/1997 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00243BO (4 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 |
| SA00245SE | | Installation of the Aviation Research Systems Inc. Locking Fuel Caps | | Reissued | | 10/23/2003 |
| SA00246SE | | Installation of the Aviation Research Systems Inc. Locking Fuel Caps | | Reissued | | 10/23/2003 |
| 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 |
| SA00460SE | | Installation of stainless steel battery box. | | Issued | | 8/8/1997 |
| SA00478CH (PAGE 3) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| SA00557AT | | Installation of carbon steel brake discs. | | Reissued | | 1/24/1995 |
| SA00609DE | | Installation of a nose whell shimmy damper | | Issued | | 12/3/2007 |
| SA00625LA | | Installation of a Concorde Battery Model no RG-35 or RG-35XC. | | Issued | | 4/27/1998 |
| SA00638WI | | Installation of Concorde Battery Corporation (vrsla) Valve Regulated Sealed Acid Battery. | | Amended | | 8/10/2012 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00706LA | | Installation of a starter engaged light. | | Issued | | 11/25/1998 |
| SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
| 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 |
| SA00785SE | | Installation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package MA2125 Revision IR dated January 18 2000 and Installation Manual MA2126 Revision IR dated January 21 2000 or later FAA approved revisions. | | Issued | | 2/29/2000 |
| SA00789LA | | Installation of Clear View Sunvisor. | | Amended | | 11/2/2001 |
| SA00839WI | | Front spar failsafe strap. | | Amended | | 7/18/2002 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00901NY | | Installation of a wing tip recognition lights. | | Reissued | | 2/27/2006 |
| SA00954SE (1 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 |
| SA01075SE | | Installation of the Precise Flight Inc. SpeedBrake 2000 System. | | Amended | | 7/19/2006 |
| SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
| SA01078NY | | Installation of Left and Right Side Windows. | | Issued | | 8/25/1999 |
| SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
| SA01085SE | | Installation of BAS Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE dated May 13 2002 or later FAA approved revision. | | Amended | | 12/2/2010 |
| SA01110CH | | Installation of wing fuel tank quick valve drains. (Listed models with specific serial number applicability) | | Issued | | 9/27/1999 |
| SA01120SE | | Installation of Door Steward. | | Amended | | 3/4/2010 |
| SA01155AT | | Installation of left hand and right hand auxiliary fuel cell assemblies | | Reissued | | 4/27/2009 |
| 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 (2 OF 2) | | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | Amended | | 3/29/2005 1:00 |
| SA01165CH | | Install cooling air baffle on Raytheon (Beech) aircraft Model H35 J35 K35 M35 N35 and P35 or aircraft Model A35 B35 C35 D35 E35 F35 G35 H35 J35 K35 M35 35-33 35-A33 35-B33 35-C33 E33 and F33 which are modified by STC SA2660SW SA5635SW SA5527SW SA238GL SA893WE or SA2361SW to use Teledyne Continental Motors engine Models IO-470-C or IO-470-N in accordance with Castlegar Trust L. L. C. Installation manual as listed on AML No. SA01165CH or later FAA Approved revisions. | | Reissued | | 6/7/2011 |
| SA01168SE | | Installation of Teledyne Continental E225-8 engine modified. | | Amended | | 10/16/2007 |
| 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 |
| SA01330LA (PAGE 2) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01436SE (2 OF 2) | | Cockpit sunvisor retrofit kit. | | Issued | | 8/2/2004 0:00 |
| SA01473SE (5 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 |
| SA01561CH | | Installation of Hartzell Model PHC-(C L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental Motors six-cylinder engines in accordance with D | | Reissued | | 6/17/2011 |
| SA01639NY | | Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B. | | Amended | | 6/1/2004 |
| SA01655LA | | Installation of ignition switch. | | Reissued | | 4/1/2008 |
| SA01668CH | | Installation of Hartzell Model PHC-(C L)3YF-1RF/F8068 three bladed propeller in accordance with D | | Reissued | | 3/21/2011 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01683NY | | Installation of .250 .312 .375 or .500 thick windshield. | | Issued | | 6/17/2003 |
| SA01692SE (Page 1 OF 2) | | Installation of a Garmin GMX 200 Multi-Function Display | | Reissued | | 10/3/2012 |
| SA01695SE (4 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 |
| SA01807AT | | Installation of a Basic Type BAE 14/28 Model 2025 Air Driven Alternator. | | Issued | | 1/14/1999 |
| SA01834CH (1 OF 2) | | Installation of the High Intensity Discharge Light Assembly Kit. | | Amended | | 3/20/2009 |
| SA01860NY (1 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 4) | | 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 (4 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
| SA01944CH (1 OF 2) | | Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. | | Issued | | 3/5/2004 |
| SA01988SE (PAGE 2) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| 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 4) | | Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) | | Amended | | 7/25/2008 0:00 |
| 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 2) | | Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. | | Amended | | 1/12/2005 0:00 |
| SA02168AK (PG 1) | | Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. | | Issued | | 3/23/2001 |
| SA02203AK (PAGE 2) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02217AK (4 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 |
| SA02268CH (PAGE 4) | | 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 |
| SA02424AT-D | | Installation of replacement fuel cell assemblies | | Reissued | | 4/16/2009 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02460CH | | Install Genesis Aero LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanks | | Reissued | | 11/19/2012 |
| 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 1) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02722CH | | Install D | | Issued | | 7/1/2009 |
| SA02738CH (PAGE 6) | | 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 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03913AT | | Installation of the Astronics LED Replacement Lighting Bulbs in accordance with Chippewa Aerospace Master Drawing List (MDL) No. P23-3340-01-0001 Rev. 1 Dated November 01 2010 or later FAA approved revision. | | Issued | | 3/21/2011 |
| SA09141AC-D | | Installation of S-TEC System 55two axis automatic flight guidance system Model ST-613 with optional autotrim system. | | Amended | | 10/24/2001 |
| SA09143AC-D | | Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System Model ST-614. | | Amended | | 9/21/2002 |
| SA09145SC | | Installation of vortex generators on wing upper surfaces in accordance with J.V.E. Inc. Drawing List JVE-501 Revision IR dated 01/05/96 and Installation Manual JVE-0596 Revision IR dated 01/05/96 or later FAA approved revisions. | | Reissued | | 6/17/2011 |
| SA09313AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-757-20/30. | | Issued | | 12/5/1997 |
| SA09337SC | | An increase gross weight of 100lbs for Beech models A35 B35 C35 D35 E35 F35 G35 and 35R when equipped with Vortex Generators per J.V.E. Inc. STC SA09145SC. | | Reissued | | 9/28/2011 |
| SA09345AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-758. | | Issued | | 2/25/1998 |
| SA09441AC-D | | Installation of S-TEC System 40X/50X Single and Two-Axis Automatic Flight Guidance Systems Model ST-787-40X/50X. | | Issued | | 3/8/2000 |
| SA09603SC | | Installation of Teledyne Continental Motors fuel injected engine. | | Amended | | 1/30/2001 |
| SA1-27 | | Installation of Tactair T-3 auto-matic pilot and optional installation of Tactair AH-1 altitude hold device (for use with Tactair T-3autopilot). | | Reissued | | 8/7/1972 |
| SA1-303 | | Auxiliary wing tip fuel tanks. | | Reissued | | 2/14/1975 |
| SA1-341 | | Oil-free vacuum pump PA-201. | | Issued | | |
| SA1-343 | | Oil-free vacuum pump. | | Issued | | |
| SA1-368 | | Installation of auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company | | Reissued | | 8/16/2011 |
| SA1-377 | | Replacement of d.c. belt- driven generator and regulator with Leece-Neville belt-driven alternator with built-in silicon rectifier. | | Issued | | |
| SA1-379 | | Lube oil filter PB55-1 on aircraft with Continental E-185-1 through -11 engines. | | Amended | | 9/11/1967 |
| SA1-381 | | Installation of Fram oil filter Model PB55-1. | | Amended | | 9/11/1967 |
| SA1-460 | | : Installation of auxiliary wing tip fuel tanks in accordance with Drawing Number RB1-001B and Installation Instructions number RB-1 Revision of April 1 1960.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( This wing tip tank installation is acceptable with either the baggage auxiliary tanks or the wing auxiliary tanks. However it is not acceptable with both auxiliary installations incorporated simultaneously. | | Reissued | | 8/16/2011 |
| SA1-478 | | Griswold lateralizer. | | Amended | | |
| SA1-491 | | Flare rack modification to include radio equipment mount. | | Amended | | |
| SA1-55 | | Federal F-200 automatic pilot. | | Amended | | 1/1/1960 |
| SA1-569 | | Installation of Continental IO-470-J engine (fuel injection) and Hartzell BHC-92ZF-lDl / 8447 propeller in accordance with Stauffer drawing No. 7 dated May 2 1961 and Stauffer Flight Manual Supplement No. 7 FAA approved May 5 1961. | | Reissued | | 6/17/2011 |
| SA1-570 | | Installation of propeller equipped with 8433 or 8833-4 or V8433 V8834-4 blades respectively. | | Amended | | 6/29/1979 |
| SA1-628 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| SA1000CE | | Install cabin and engine compart-fire suppression system. | | Reissued | | 12/15/1977 |
| 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 (4 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA10558SC | | Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot. | | Issued | | 7/27/2006 |
| SA1056WE | | BSA-2 stability augmentation system and optional rudder add-on kit. | | Reissued | | 10/1/1973 |
| SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA10921SC | | Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators | | Issued | | 11/10/2008 |
| SA109WE | | M-4 autopilot. | | Issued | | 1/1/1960 |
| SA1113WE | | B-4 flight control system. | | Reissued | | 10/1/1973 |
| SA1150WE | | Gyro sense element relocated to remote position. | | Reissued | | 10/1/1973 |
| SA115CE | | Turbo volt Model Three-Five emergency electrical and vacuum system. | | Issued | | 5/4/1980 |
| SA1176SO | | Installation of Aileron and Wing Flap Gap Seals | | Amended | | 1/6/2010 |
| SA11GL | | Installation of Cleveland 6.00-6wheels and brakes conversion kit 199-49. | | Amended | | 9/2/1987 |
| SA1211NW | | Installation of an improved instrument panel | | Issued | | 7/24/1981 |
| SA1215NW | | Installation of a Contintental engine Hartzell propeller | | Issued | | 4/20/1981 |
| SA1254NW | | Installation of Beech Model E35 front and rear wing spar center section carry-through members and Beech Model G35 wing panels | | Issued | | 6/9/1981 |
| SA1258NW | | Installation of a modified Aviation Enterprises instrument panel | | Issued | | 6/18/1981 |
| SA1262WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1270SW | | Installation of Mitchell automatic flight system Model AK328 consisting of Century I autopilot with omni tracking system. | | Reissued | | 7/9/1984 |
| SA1285NW | | Installation of a Tactair T3 autopilot | | Issued | | 8/11/1981 |
| SA1290NW | | Installation of a McCauley 3A32C76S-M/S82NB-2 propeller on a Continental IO-520-BA engine | | Issued | | 8/14/1981 |
| SA130EA | | AF-510A AF-512A or AF-512B autopilots. | | 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 |
| SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
| SA1369WE | | Installation of Brittain Industries Inc. Model BSA-3 stability augmentation system. | | Reissued | | 10/20/1972 |
| SA136WE | | Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. | | Reissued | | 10/1/1973 |
| SA1375WE | | Installation of Dukes Astronautics Model 4140-00-39 Auxiliary Fuel Pump into fuel system | | Amended | | 2/4/1976 |
| SA137WE | | Beech wing tip kit 35-660. | | Issued | | 1/1/1960 |
| SA1387WE | | Installation of Brittain Industries Model NAV-2A Flight Control System. | | Reissued | | 10/1/1973 |
| SA1405NM | | Installation of a fuel transfer system | | Issued | | 1/29/1982 |
| SA1417NM | | Installation of a Franklin 6AS-350-A or 6AS-350-A1 engine with an AiResearch TE-0657turbosupercharger and Hartzell HC-C2YF-1BF/F8459A-4 to -8 or Hartzell HC-C2YF-1BF/8459A-4Q or -8Q propeller. | | Reissued | | 4/9/1999 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1423WE | | Wing truss reinforcement front spar and change of hinge points for landing gear idler arm. | | Amended | | 6/14/1976 |
| SA144EA | | Approval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG RBI-IDOL) Fiberglass wing Solenoid Fuel System (ref STC SAl-303 dated February 20 1959). No wing or baggage compartment auxiliary tanks are permitted with this system. This STC also places the above aircraft in the Normal and Utility categories using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders Inc. Installation Manual FEI-35 (4A) Rev. D dated February 15 1964 is required. | | Reissued | | 8/16/2011 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| SA1476WE | | Installation of Brittain Industries Inc. Model B2C Flight Control System | | Reissued | | 1/23/2013 |
| SA1477WE | | Installation of Brittain Model B2C Flight Control System. | | Reissued | | 10/20/1972 |
| SA147CE | | Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. | | Issued | | 1/1/1960 |
| SA1493WE | | Installation of Brittain Industries Inc. Model B2C Flight Control System | | Reissued | | 2/1/2013 |
| SA1499NM | | Installation of a General Electric flap indicator | | Issued | | 4/19/1982 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA152CE | | Federal F-200 autopilot. | | Issued | | 1/1/1960 |
| SA152NW | | Installation of deck and glare shield (with or without instrument lights). | | Amended | | 5/21/1981 |
| SA1531WE | | Installation of Brittain Model BSA-4 Stability Augmentation System. | | Reissued | | 10/20/1972 |
| SA153EA | | Install Beryl D | | Amended | | 1/30/2013 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1584CE | | Installation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005 stamped FAA Approved | | Reissued | | 9/28/2011 |
| SA1584GL | | Install Aero Fabricators shoulder harness and seat belt assembly. | | Issued | | 7/1/1991 |
| SA1644SW | | Installation of Mitchell automatic flight system Model AK415 consisting of Century IIB autopilot with optional radio coupler. (S35 S/N 7841 AND BELOW) | | Reissued | | 7/16/1984 |
| SA1650CE | | Installation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8 1981 or later. | | Reissued | | 9/28/2011 |
| SA165SW | | Automatic pilot AK121. | | Issued | | 1/1/1960 |
| SA1703CE | | Installation of flap and aileron fairings and seals. | | Reissued | | 1/26/1993 |
| SA1722WE | | Installation of Fiberglass tail fairing. | | Amended | | 8/28/2006 |
| SA1736WE | | Installation of Brittain Industries B-5 Flight Control System. | | Reissued | | 10/20/1972 |
| SA173GL | | Installation of Dukes fuel pump P/N 4140-00-39. | | Reissued | | 5/22/1989 |
| SA1775NM | | Installation of a Teledyne/Continental engine a Beechcraft propeller a Dukes fuel pump a Woodward propeller governor and associated changes | | Issued | | 7/12/1983 |
| SA1776NM | | Installation of standard late model long sloping windshield. (35-33 S/N CD-1 THR E 33 S/N CD118) (C35 S/N D2681 THRU V35 S/N 8598) | | Issued | | 7/19/1983 |
| SA177EA | | Installation of Monitair angle of attach system Model AA-2. | | Reissued | | 2/14/1972 |
| SA1782NM | | Installation of Precise speedbrake system. | | Amended | | 11/7/2003 |
| SA1803CE | | Installation of fire extinguishing system in cabin and/or fire extinguishant system in engine compartment. | | Reissued | | 2/1/1993 |
| SA1811NM | | Installation of Safe Flight Model SC-150 lift detector system. | | Reissued | | 10/31/1984 |
| SA181EA | | Approval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG RBI-IDOL) Fiberglass wing tip fuel tanks (ref STC SA3OEA Configuration 2 or 3) and Type II or III Kit transfer fuel system. This system eligible with Beech 20 gal wing aux. tanks or baggage compartment tanks but not both. This STC also places the above aircraft in the Normal and Utility categories using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders Inc. Installation Manual FEI-35 (4A) Rev. C dated February 15 1964 is required. | | Reissued | | 8/16/2011 |
| SA184NE | | Installation of a landing gear protective switch cover. | | Issued | | 10/6/1983 |
| SA1850SO | | Installation of revised instrument panel. | | Issued | | 10/16/1985 |
| SA1883WE | | Installation of Brittain Industries NAV-2B flight control system. | | Reissued | | 10/20/1972 |
| SA1902SW | | Installation of Mitchell automatic flight system Model AK348consisting of Century I autopilot with optional omni tracker. | | Reissued | | 8/1/1984 |
| SA197NW | | Installation of Clark three- light gear position indicator system. | | Reissued | | 6/17/2011 |
| SA19GL | | Install Cleveland 7.00-8 wheels and brakes. | | Amended | | 7/24/1987 |
| SA2-1533 | | Installation of windshield wiper. | | Reissued | | 1/31/1997 |
| SA2000SW | | Dual control wheel. | | Issued | | 1/1/1960 |
| SA2029WE | | Installation of Delta Sigmatronix Emergency Electric Fuel Pump Kit PK-2 in lieu of Beech hand pump P/N 35-924230 (on aircraft equipped with Beech P/N 35-921171 or P/N 35-924065 fuel unit). (C35 S/N D1 THRU D2900) | | Issued | | 1/1/1960 |
| SA2045CE | | Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index(RON +MON)/2. | | Amended | | 5/10/2004 |
| SA2065NM | | Installation of a Dukes Model 4140-00-39 fuel boost pump under the cabin floor | | Issued | | 3/18/1983 |
| SA2081WE | | Installation of Madras Air Service P/N MAS 102 wing tips. | | Amended | | 12/7/1987 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2131WE | | Installation of Delta Sigmatronix emergency electric fuel pump P/N 29000 in above models equipped with Beech P/N 35-924230 fuel unit. | | Issued | | 1/1/1960 |
| SA2144WE | | Installation of Madras Air Service Part No. MAS 102 wing tips. | | Issued | | 1/1/1960 |
| SA2145SO | | Installation of Appalacian Accessories stainless steel brake discs P/N s 75-25A or75-25B. | | Reissued | | 9/29/1995 |
| SA2160NM | | Installation of the Precise Flight stand-by vacuum system (SVS). | | Amended | | 11/7/2003 |
| SA2198NM | | Installation of a winch and fairlead system for deployment of a trailing drogue (cone). | | Issued | | 2/13/1984 |
| SA219EA | | Installation of Katz integrated flight indicator Model KIFI-2 or KIFI-2A. | | Amended | | 5/21/1969 |
| SA2200SW | | Installation of Teledyne Continental IO-520-B -BA - BB or IO-550-B engine and applicable McCauley Propeller only as listed on STC. | | Reissued | | 3/23/2009 |
| SA2201SW | | Ventral fin. | | Issued | | 6/23/1975 |
| SA2208WE | | Installation of Red-Q-Mark Signet A-MK-100 or A-MK-110 marker assembly. | | Amended | | 8/7/1970 |
| SA2219WE | | Installation of Filtrator Company Engine Crankcase Breather and Vacuum Pump Air-Oil Separator in accordance with the applicable FAA sealed drawing listed on the attached Master Eligibility List Number SA2219WE.Installation of Filtrator Company engine crankcase breather and vacuum pump air-oil separator. | | Reissued | | 7/14/2011 |
| SA222CE | | Reinforce front lower carry- through section & wing attach fittings. | | Amended | | 6/2/1980 |
| SA2271WE | | Installation of long fiberglass tailcone to replace the short factory installed tailcone. | | Reissued | | 4/3/1975 |
| SA2286NM | | Installation of tail stabilizer support. | | Reissued | | 3/26/2007 |
| SA22SW | | AK087 AK087E or AK087R automatic pilot. | | Issued | | 1/1/1960 |
| SA232EA | | Installation of Tactair omni lock model OL-1 and optional installation of Tactair localizer adapter model LA-1 (for use with Tactair model omni lock model OL-1). | | Reissued | | 8/7/1972 |
| SA2361SW | | Installation of Continental IO-470-N engine and McCauley 2A36C23/84B-0 or 2A37C223/90RB-6 or Beech 278-100-11/278-214-82 or 278-100-13/278-214-82 or Flottorp F12A-3/8400-2 propeller | | Amended | | 3/7/2013 |
| SA236GL | | Installation of a Continental O-470-G engine and McCauley propeller. | | Issued | | 5/4/1978 |
| SA2375CE | | Installation of B&D Instruments & Avionics Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics Inc. Installation Manual Part No. 0535-003-011 Rev. B or later FAA Approved | | Reissued | | 11/3/2011 |
| SA23CE | | 210419 governor. | | Issued | | 1/1/1960 |
| SA23EA | | Installation of Third Cabin Window on both sides of Fuselage in accordance with Glenn Floyd Stauffer Drawing Nos. 42601 Revision A dated 31 May 1962 and 42602 Revision A dated 13 June 1962. | | Reissued | | 8/16/2011 |
| SA2470WE | | Installation of anticollision lighting system. | | Issued | | 2/8/1972 |
| SA2546WE | | Installation of Pathfinder Engineering Corp. Model P1-( )autopilot system. | | Reissued | | 9/30/1998 |
| SA2547WE | | Installation of Pathfinder Engineering Corporation Model P2-( ) autopilot system. | | Reissued | | 2/20/1974 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA2619WE | | Installation of Pathfinder Model P1-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2633WE | | Installation of enlarged window and baggage compartment. | | Reissued | | 11/19/2012 |
| SA2653SW | | Installation of Instrument Panel in accordance with 1998-54 Installation Manual and Drawings 1998A200 1998A300 1998A400 and 1999 all dated July 1 1977 Battery Box Kit per 1998-84 Installation Manual and Drawing 2000 dated July 1 1977 Radio Cooling Kit per 1998-86 Installation Manual and Drawing 2002 each dated July 1 1977. | | Reissued | | 8/16/2011 |
| SA2653WE | | Installation of Beryl D | | Reissued | | 7/14/2011 |
| SA2654WE | | Installation of Pathfinder Model P2A( ) autopilot. | | Amended | | 7/3/1979 |
| SA265SO | | Extension addition to nose landing gear doors. | | Issued | | 1/1/1960 |
| SA269WE | | Pneumatic pitch assist PC-1 and optional installation altitude hold AH-1. | | Reissued | | 10/1/1973 |
| SA2700WE | | Installation of Airborne Electronics solid state automatic propeller control Model 350A. | | Amended | | 3/28/1977 |
| SA2753CE | | Installation of flap actuated landing gear warning system. | | Reissued | | 5/7/1997 |
| SA2771WE | | Installation of Long Fiberglass tailcone to replace the short factory installed tailcone in accordance with FAA Sealed N.E. Coote Tool and Machine Drawing List Report No. 1 dated September 2 1970. | | Reissued | | 8/16/2011 |
| SA283EA | | Installation of Flight Extender Inc. Alternate Fiberglass Fuel Tip Tanks (P/N RB4-100 15 Gal.) on the above aircraft when equipped with 15 gal. or 12 gal. tip fuel systems in accordance with the following STC | | Reissued | | 2/6/1975 |
| SA2858WE | | Installation of right and/or left hand cockpit side windows in accordance with FAA sealed Beryl D | | Reissued | | 6/17/2011 |
| SA28EA | | Installation of 12-gallon fiberglass wing tip fuel tanks. | | Reissued | | 8/16/2011 |
| SA292WE | | Alternator A-14-0 or A-14-5 and voltage regulator A-20. | | Issued | | 1/1/1960 |
| SA293CE | | GUARD System (Gear Up Automatic Response Device). | | Amended | | 9/6/1966 |
| SA2941SW | | Addition to Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
| SA294CE | | GUARD System (Gear Up Automatic Response Device). | | Amended | | 9/6/1966 |
| SA3-196 | | Lear ADF-12C kit complete and LTRA-5 with scope complete. | | Issued | | 1/1/1960 |
| SA3-241 | | Electric motor-driven AN4100 fuel pump. | | Issued | | 1/1/1960 |
| SA3-264 | | Radio rack aft of baggage compartment. | | Issued | | 1/1/1960 |
| SA3-276 | | Scott 8800 oxygen console. | | Issued | | 1/1/1960 |
| SA3-298 | | Electric motor-driven fuel booster pump. | | Issued | | 1/1/1961 |
| SA3-3 | | BC Chinook cabin heater. | | Issued | | 1/1/1960 |
| SA3-317 | | Baggage compartment windows. | | Issued | | 1/1/1960 |
| SA3-56 | | Oxygen equipment Purtain Type E bottles and Scott#8800 console. | | Issued | | 1/1/1960 |
| SA3-58 | | Grimes D-7080-2-12 rotating beacon. | | Issued | | 1/1/1960 |
| SA3-673 | | L-2B autopilot with or without altitude control and/or approach coupler. | | Issued | | 1/1/1960 |
| SA3-8 | | L-2B automatic pilot including approach coupler and altitude control. | | Issued | | 1/1/1960 |
| SA3020WE | | Installation of exhaust silencers in accordance with Top Banana Installation Instructions dated March 12 1975 Revision of October 22 1975.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( Silencer is manufactured in accordance with Top Banana Drawing No. 2-12-A35 G | | Reissued | | 7/14/2011 |
| SA30EA | | Installation of 13.5 gallon fiber-glass wing tip tank assembly. | | Reissued | | 8/16/2011 |
| SA3113SW-D | | Mitchell automatic flight system AK415 cons. Of Century IIB autopilot with optional radio coupler. | | Reissued | | 8/16/1984 |
| SA3116SW-D | | Installation of Mitchell automatic flight system AK325 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 6/5/1984 |
| SA312WE | | Beech pneumatic pitch assist PC-1and optional altitude hold AH-1. | | Reissued | | 10/1/1973 |
| SA3191WE | | Installation of wing tip fences. (A35 B35 C35 D35 E35 F35 G35 UTILITY CATEGORY) (35 NORMAL OR UTILITY CATEGORY) | | Issued | | 5/11/1976 |
| SA319NW | | Installation of a Continental IO-520-BA engine Hartzell HC-C3YF-1RF/8468A-8R propeller and associated systems | | Amended | | 9/17/1976 |
| SA321SO | | Tank type wing tip plates. | | Issued | | 1/1/1960 |
| SA321WE | | Beech pneumatic pitch assist PC-1and optional altitude hold AH-1. | | Reissued | | 10/1/1973 |
| SA322WE | | Pneumatic pitch assist PC-1 and optional altitude hold AH-1. | | Reissued | | 10/1/1973 |
| SA323WE | | Beech pneumatic pitch assist PC-1and optional altitude hold AH-1. | | Reissued | | 10/1/1973 |
| SA3260WE | | Installation of electric driven fuel pump. | | Issued | | 9/8/1976 |
| SA3267SW-D | | Mitchell automatic flight system AK727 consisting of Century III autopilot with optional and glide slope couplers. | | Reissued | | 3/29/1984 |
| SA3268SW-D | | Mitchell automatic flight system AK728 consisting of Century IV autopilot or AK728FD consisting of Century IV flight director autopilot with optional remote annunciator. | | Reissued | | 3/29/1984 |
| SA3271SW-D | | Mitchell yaw damper system YK631. | | Reissued | | 3/29/1984 |
| SA3286SW-D | | Mitchell automatic flight system AK732 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 3/29/1984 |
| SA332EA | | Electronic voltage alarm. | | Amended | | 1/1/1960 |
| SA3337WE | | Installation of ventral air skeg. | | Amended | | 4/2/1979 |
| SA334SW | | Installation of InterAv Alternator. | | Reissued | | 7/20/1981 |
| SA3365NM | | Install a Continental IO-470-K Engine McCauley 2A36C23/84B-0 Propeller and an M35 Bonanaza nose section structure | | Issued | | 4/28/1986 |
| SA33SW | | Beech T-24 ailerons 45-135050-3with servo attach fittings 45-115090. | | Issued | | 1/1/1960 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3584NM | | Installation of aileron and flap gap seals. | | Reissued | | 10/23/2003 |
| SA358GL | | Carburetor air filter (dry type). | | Issued | | 1/1/1960 |
| SA358WE | | One-piece windshield. | | Reissued | | 6/25/2001 |
| SA359WE | | Supercharged Continental engine E225-8. | | Issued | | 1/1/1960 |
| SA361EA | | A. Installation of monitair angle of attack and stall warning kit number 92-107 and B. Installation of Monitair angle of attack and stall warning kit number 92-105. | | Reissued | | 2/14/1972 |
| SA3650NM | | Cockpit sun visor installation. | | Amended | | 7/7/2004 |
| SA3678WE | | Installation of air/oil separator. | | Reissued | | 9/28/2001 |
| SA374SW | | Automatic pilot AK131 AK131E and AK131E-3 pitch trim system AK132 and federal lateral guidance radio AK123. | | Issued | | 1/1/1960 |
| SA380SW | | A-C generator. | | Issued | | 1/1/1960 |
| SA384WE | | Installation of adjustable pilot and co-pilot seat | | Amended | | 6/27/2012 |
| SA387SO | | Installation of Aviation Elec. Omni bearing tester Model OBT-X in accordance with AET Drawing Nos. 1001 1002 1003. | | Issued | | 1/1/1960 |
| SA4-1146 | | Hartzell HC-12X20-7C/8433-0propeller. | | Issued | | 1/1/1960 |
| SA4-1239 | | Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. | | Reissued | | 10/1/1973 |
| SA4-1245 | | Installed Flightcraft ski bag compartment. | | Reissued | | 1/31/1986 |
| SA4-1260 | | Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. | | Reissued | | 10/1/1973 |
| SA4-1305 | | Hartzell HC-12X20-7E/8433-0propeller. | | Issued | | 1/1/1960 |
| SA4-133 | | Automatic rudder control. | | Issued | | 1/1/1960 |
| SA4-1437 | | Leece-Neville alternator A001-2002AA and regulator A001-3533RA. | | Issued | | 1/1/1960 |
| SA4-1538 | | Oil-air separator. | | Issued | | 1/1/1960 |
| SA4-1611 | | Anticollision beacon Roto- Lite X5000 either 12 or 24- volt on the top or bottom of fuselage. | | Issued | | 1/1/1960 |
| SA4-1629 | | Installation of wing tip fuel tanks. | | Reissued | | 9/29/2009 |
| SA4-190 | | Automatic rudder control. | | Issued | | 1/1/1960 |
| SA4-191 | | L-2 automatic pilot. | | Issued | | 1/1/1960 |
| SA4-238 | | Thompson TF 2800 engine- driven fuel pump installation on Continental O-470-G engine. | | Issued | | 1/1/1960 |
| SA4-280 | | Ceco CE-9136 AN-4100 or AN-4101 electric fuel pump. | | Issued | | 1/1/1960 |
| SA4-282 | | Tactair T-3 automatic pilot. | | Issued | | 1/1/1960 |
| SA4-344 | | B arcon system. | | Issued | | 1/1/1960 |
| SA4-393 | | Fiberglas reinforced plastic wing tips incorporating positions. | | Issued | | 1/1/1960 |
| SA4-435 | | Automatic rudder control Model B. | | Issued | | 1/1/1960 |
| SA4-436 | | L-2 autopilot. | | Issued | | 1/1/1960 |
| SA4-489 | | Automatic rudder control. | | Issued | | 1/1/1960 |
| SA4-550 | | Standard Beech A-35 Fuel System modified. | | Reissued | | 3/5/1998 |
| SA4-559 | | 20-gallon auxiliary fuel tank. | | Issued | | 1/1/1960 |
| SA4-562 | | Federal F-200 autopilot. | | Issued | | 1/1/1960 |
