| 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 |
| SA00035DE | | Installation of modified engine baffle/cooling louver system. | | Reissued | | 10/16/1998 |
| SA00044LA | | Installation of replacement rudder hinge brackets. | | Reissued | | 2/6/2001 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00063LA | | Installation of Acoustical/Thermal insulation. | | Reissued | | 1/5/2005 |
| SA00066WI | | Installation of global positioning system GPS 150. | | Issued | | 5/24/1993 |
| SA00068SE (PAGE 1) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 |
| SA00068WI | | Installation of a stretcher on the seat rail. | | Issued | | 5/25/1993 |
| SA00070SE | | Fabrication of Model RD-0050replacement wing-tip position light lens covers. | | Issued | | 4/4/1994 |
| 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 |
| SA00080BO | | Installation of BB-145 NAV-COMM antenna. | | Issued | | 1/21/1998 |
| 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 |
| SA00161BO (3 OF 3 | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 0:00 |
| 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 |
| SA00193WI-D | | Installation of Bendix/King KLN 90A Global Positioning System (GPS). For model F33A approved for serial numbers CE-772 and higher. For model A36 serial numbers E-1241 and higher. | | Reissued | | 2/28/2000 |
| 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 |
| SA00203NY | | Installation of .312-inch .375-inch or .500-inch thick replacement windshields. | | Issued | | 7/15/1994 |
| 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 |
| SA00206AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00224SE | | Modification of Beech exhaust stack assemblies. | | Issued | | 8/25/1995 |
| SA00238SE | | Installation of Aviation Development Corporation s sump mounted chip detector | | Issued | | 10/31/1995 |
| SA00242WI-D | | Installation of Bendix/King KLN 90B Global Positioning System (GPS) for IFR enroute and approach operation. For model F33A serial number CE-772 and above model A36 serial number E-1241 and above A36TC and B36TC all serial numbers. | | Reissued | | 11/3/2000 |
| 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 |
| SA00257BO | | S/Ns E-111 E-1241 and up ONLY: Installation of air conditioning system. | | Issued | | 7/20/2007 |
| SA00269BO (3 OF 3) | | Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. | | Reissued | | 4/9/2010 |
| SA00281BO | | Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 | | Amended | | 4/24/2012 |
| SA00290BO ( PAGE 2) | | 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 0:00 |
| SA00304BO | | Installation of Approach Aviation | | Issued | | 12/23/2010 |
| SA00331BO | | Installation of Avidyne Corporation Autopilot | | Issued | | 5/10/2013 |
| SA00352LA | | Installation of Aero Sound Shield Acoustical Firewall Blanket Part No. AS-0500. | | Reissued | | 1/5/2005 |
| SA00353WI | | Installation of a modification kit for cold weather operation. | | Reissued | | 5/29/2007 |
| SA00358DE | | Installation of radio telephone system. | | Issued | | 10/22/1998 |
| SA00368CH | | Installation of cooling air baffles | | Amended | | 3/27/2008 |
| SA00391NY | | Installation of second wind auxiliary vacuum system. | | Reissued | | 6/18/2002 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00423SE | | Installation of stainless steel battery box. | | Reissued | | 10/23/2003 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00462AT | | Replacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47. | | Reissued | | 12/7/1994 |
| SA00469NY | | Installation of Main Landing Gear Auxiliary Landing Lights. | | Reissued | | 2/27/2006 |
| SA00478CH (PAGE 3) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| SA00481AT-D | | Installation and operation of a United Beechcraft Keyless Entry System. | | Reissued | | 4/10/1995 |
| SA00521AT-D | | Installation of replacement fuel cell assemblies | | Reissued | | 4/16/2009 |
| SA00522AT-D | | Installation of replacement fuel cell assemblies | | Reissued | | 5/5/2009 |
| SA00532NY | | Installation of Avcheck Corp. Comcheck 422A Radio Reception Indicator. | | Issued | | 12/10/1996 |
| SA00557AT | | Installation of carbon steel brake discs. | | Reissued | | 1/24/1995 |
| SA00581CH | | Installation of a Bendix/King EFS 40 Two Tube EFIS. | | Issued | | 11/25/1996 |
| 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 |
| SA00639SE | | Installation of Turbine Outlet Temperature Indicator in accordance with Soloy Master Drawing List 887-101 Revision - dated July 30 1998 or later FAA approved revision. This STC is only applicable to aircraft that have been modified in accordance with Soloy STC SA3523NM. | | Reissued | | 12/2/2004 |
| SA00667WI-D | | Installation of Bendix/King KFC 225 Automatic Flight Control System. For model A36 S/N E-1946 E-2104 E-2111 and after. For model B36TC S/N EA-320 EA-389 and after | | Reissued | | 2/28/2000 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00680NY | | Installation of Dorsal Fin. | | Issued | | 8/14/1997 |
| SA00681NY | | Installation of tail cone. | | Issued | | 8/14/1997 |
| SA00690CH | | Installation of Great Lakes Aero Products Pilot Side and Door Windows. | | Amended | | 2/18/1999 |
| SA00696LA | | Installation of Sandel Avionics SN3308 Navigation Display. | | Issued | | 10/20/1998 |
| SA00697LA | | Installation of Avionics Innovations Compact Disc Shuttle Inflight Entertainment System. | | Issued | | 10/20/1998 |
| SA00718CH | | Installation of McCauley Propeller Model 3A36C434/80VEA-0. | | Reissued | | 9/21/2005 |
| SA00718LA | | Installation of a Hartzell PHC-C3YF-1RF/F8468A(B K)-8R constant speed propeller. | | Reissued | | 2/5/1999 |
| SA00719LA | | Installation of a Hartzell PHC-C3YF-1RF/F8468A(B K)-6R constant speed propeller. | | Amended | | 5/25/2005 |
| SA00724WI | | Installation of B&C Specialty products BC410-1 Standby Alternator | | Amended | | 6/26/2000 |
| SA00735LA | | Installation of Teledyne Continental Motors O-470-M engine modified by STC SE00736LA in accordance with Michael Adamson Installation Instructions Beech Model 35-A33 Manual #l Revision N/C dated January 4 1999 or later FAA approved revisions. Michael Adamson Airplane Flight Manual Supplement #1 dated February 23 1999 or later FAA approved revision is required with this installation. (Raytheon 35-A33 Serial Number CD-334) | | Issued | | 3/19/1999 |
| 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 |
| SA00803SE | | Installation of vortex generators on wings and tail surfaces. | | Amended | | 11/7/2008 |
| SA00839WI | | Front spar failsafe strap. | | Amended | | 7/18/2002 |
| SA00849WI | | Installation of a dual Garmin GNS-430 communications transceiver/VOR/ILS receiver/GPS receiver with single Garmin GI-106A course deviation indicator Mid-Continent Instruments MD41-1468 GPS Annunicator Ps Engineering PMA7000M-S Audio Panel Shadin ADC- 200 Fuel/Air Data Computer and BF Goodrich WX-500 Weather Mapping Sensor. | | Reissued | | 3/26/2007 |
| SA00851WI | | Installation of a Dual Garmin GNS-430 Communications Transceiver/VOR/ILS receiver/GLS receiver with Single Garmin GI-106A course deviation indicator. | | Issued | | 2/9/2000 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00874AT-D | | Installation and operation of a United Beechcraft keyless entry system. | | Reissued | | 10/20/2005 |
| SA00899CH | | Installation of pneumatic luggage door strut on those models with an extended luggage door. | | Reissued | | 7/8/1998 |
| SA00901NY | | Installation of a wing tip recognition lights. | | Reissued | | 2/27/2006 |
| SA00902WI | | Replacement of original main landing gear doors with monolithic machined gear doors. | | Amended | | 12/1/2000 |
| SA00911CH | | Installation of rudder fin cap/strobe fairing. | | Issued | | 7/8/1998 |
| SA00954SE (2 OF 2) | | Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. | | Amended | | 8/11/2003 |
| SA00982WI | | Installation of Liese-2xV60 engine exhaust silencer system. This STC is not to be transferred since its issuance was IAW 14 CFR 21.29 and based upon a validation of German LBA EMZ No. 0724/534/534a/627/627a. | | Issued | | 8/20/2001 |
| SA00984WI-D | | Installation of Bendix/King KMH 880 Multi-Hazard Awareness System/KTA 870 Traffic Advisory System and optional Bendix/King KMD 550 Multi-Function Display System. Approved for A36 serial numbers E-1946 E-2104 and E-2111 and for model B36TC serial number EA-320 EA-389 and after. | | Issued | | 7/18/2001 |
| SA01010WI-D | | Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System | | Reissued | | 3/26/2007 |
| SA01033WI | | Replacement of original outboard main landing gear doors with a one-piece monolithic machined metal door. | | Amended | | 1/22/2008 |
| SA01075SE | | Installation of the Precise Flight Inc. SpeedBrake 2000 System. | | Amended | | 7/19/2006 |
| SA01077SE (PAGE 2) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 0:00 |
| 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 |
| SA01091WI | | Increase gross weight of Model N35 and P35 Beech Bonanzas by 100 lbs. | | Issued | | 7/10/2002 |
| 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 |
| SA01110CH | | Installation of wing fuel tank quick valve drains. (Listed models with specific serial number applicability) | | Issued | | 9/27/1999 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01116AT | | Install a freon air conditioning system. | | Issued | | 8/21/1996 |
| SA01120SE | | Installation of Door Steward. | | Amended | | 3/4/2010 |
| SA01126WI | | Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632 | | Issued | | 12/17/2002 |
| SA01136WI | | Installation of the TKS Ice Protection System for flight into known icing conditions. Data Required:
);INSERT INTO stc_table VALUES ( 1) Aerospace Systems & Technologies (AS&T) Drawing List No. 10300DL Revision 3 dated February 25 2003
);INSERT INTO stc_table VALUES ( 2) Supplement to Pilot | | Amended | | 4/4/2011 |
| SA01152CH | | Installation of stainless steel passenger step P/N 002-430076-23 with South Seas Ventures Inc. drawing as listed on AML No. SA01152CH or later FAA approved revision. | | Reissued | | 11/19/2001 |
| SA01154CH | | Install McCauley 3A32C406/82NDB-4 propeller on Beech Model S35 V35 V35A or V35B aircraft equipped with Teledyne Continental Motors Model TSIO-520-D or TSIO-520-DB engines in accordance with D | | Reissued | | 6/17/2011 |
| SA01155AT | | Installation of left hand and right hand auxiliary fuel cell assemblies | | Reissued | | 4/27/2009 |
| SA01156SE | | Installation of a Pratt & Whitney PT6A-21 engine flat rated at 500 HP 2200 RPM and a Hartzell HC-E4N-3N/D8292 propeller and associated hardware. | | Amended | | 7/16/2007 |
| 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 |
| SA01170NY | | Installation of NPX138N-XXX FM Transceiver. | | Amended | | 1/17/2007 |
| SA01204AT | | Installation of left-hand side and right-hand side main fuel tank fuel cell assemblies. | | Reissued | | 4/29/2009 |
| SA01205WI-D (2 OF 2) | | Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.
);INSERT INTO stc_table VALUES ( | | Amended | | 11/20/2007 |
| SA01224AT | | Installation of wheel hub cabs with valve stem access door. | | Amended | | 4/17/1998 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (3 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 |
| 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 |
| SA01330LA (PAGE 2) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
| SA01373NY | | Installation of landing lights IAW Arrow Light Company Adaptation and Installation Instructions and drawing number 2002-A-1 Rev IR dtd 7/10/01. | | Amended | | 4/27/2004 |
| SA01422AT-D | | Installation of lower cabin door stiffener. | | Amended | | 2/10/1999 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01436AT | | Installation of alternator replacement of belt-driven generator in accordance with National AirParts Document Number NAPI-3533 Initial Release dated 12/29/96 or later FAA approved revisions.
);INSERT INTO stc_table VALUES ( | | Reissued | | 6/24/2011 |
| SA01436SE (2 OF 2) | | Cockpit sunvisor retrofit kit. | | Issued | | 8/2/2004 0:00 |
| SA01455WI | | Modification to install a Honeywell KR 87 Automatic Direction Finder (ADF) System and the Honeywell KA 44B ADF Antenna interfaced with the previously installed Garmin 1000 Avionics System. | | Issued | | 10/15/2007 |
| 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 |
| SA01548CH | | Installation of Hartzell Model PHC-(C L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Continental six-cylinder engines in accordance with D | | Reissued | | 6/17/2011 |
| 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 |
| SA01595SE | | Installation of the Garmin G1000 integrated avionics system including GFC700 Automated Flight Control. | | Reissued | | 3/26/2007 |
| SA01595WI-D | | G1000 Integrated Avionics System Update with options | | Reissued | | 5/13/2013 |
| 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 |
| SA01671WI | | Installation of interior configurations | | Amended | | 2/11/2013 |
| 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 |
| SA01698LA | | Installation of interior sidewall/armrest panels per drawing DT1-1-02 Revision B dated December 6 2004 and later FAA approved revisions as listed on AML No. SA01698LA. | | Reissued | | 2/14/2005 |
| SA01711CH | | Installation of Proscan Avionics FSM2000 Flight Systems Monitor. | | Issued | | 10/10/2002 |
| SA01714WI (Page 1) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
| SA01725SE | | Installations of TAWS functionality | | Reissued | | 8/14/2007 |
| SA01727AT | | Installation of archangel avionics cockpit display system. | | Issued | | 12/3/1998 |
| SA01770SE | | ONE-ONLY: Installation of a SAGEM Electronic Displays S/N EA-524 | | Issued | | 6/29/2007 |
| SA01800SE (PG 3) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| 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 |
| SA01880CH | | Installation of a Three Point Torso Restraint System. | | Issued | | 9/5/2003 |
| 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 |
| SA01939CH | | Install Coller on the front landing gear strut. | | Issued | | 1/28/2004 |
| SA01988SE (PAGE 1) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 |
| 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 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 |
| SA02110CH (PAGE 3) | | 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 |
| SA02135CH | | Installation of L-3 Communications Avionics Systems Inc. SkyWatch Traffic Advisory System Model SKY497. | | Reissued | | 3/26/2007 |
| SA02149AK | | Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. | | Reissued | | 5/17/2013 |
| 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 |
| SA02192CH | | Increase of maximum gross weight from 3600/3650 lb. to 4010 lb. for normal category operation. | | Reissued | | 6/17/2011 |
| SA02203AK (PAGE 1) | | 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 |
| SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
| SA02268CH (PAGE 4) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02276AK | | Installation of AMSAFE Aviation Inflatable Restraints | | Amended | | 3/12/2013 |
| SA02279AT | | Installation of a Boom Beam bulb starter and ballast IAW LoPresti Master Drawing List Report No. 43 Rev D dtd 8/25/00 or later FAA approved revision. | | Amended | | 2/14/2003 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| SA02293AK (1 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02314AT-D | | Installation of a stainless steel exhaust system. Required as part of this STC is Atlantic Aero Document 19593010 Instructions for Continued Airworthiness Rev B dtd 3/27/02 or later FAA approved revision. | | Amended | | 5/25/2010 |
| SA02363CH | | Installation of Chuck Ney Enterprises Inc. CNE IO-470-C/N-MOD Model Engine (STC SE02261CH) | | Issued | | 12/18/2006 |
| SA02387AK | | Fabrication and installation of the LSI Exterior LED Lightning Suite | | Reissued | | 3/27/2013 |
| SA02412CH-D | | Installation of Hartzell propeller de-ice components. | | Issued | | 5/7/2007 |
| 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 |
| SA02461CH | | 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 |
| SA02535CH | | Installation of M-T Propeller Inc model MTV-9-D/205-58 or MTV-9-D/210-58 propeller | | Reissued | | 1/1/2009 |
| SA02547AT (PG 1) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 |
| SA02556CH-D | | Installation of a Hartzell PHC-C3YF-1RF/F8068(K) propeller. | | Issued | | 4/18/2008 |
| SA02625CH | | Installation of corrugated aluminum elevator skins in place of corrugated magnesium elevator skins. | | Issued | | 9/24/2008 |
| SA02631AT | | Replace Lord Isolating Mounting Assemblies P/N J-10520-I with Lord Assembly P/N J-23135-1 four each. | | Reissued | | 3/12/2007 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02722CH | | Install D | | Issued | | 7/1/2009 |
| SA02723CH | | Install D | | Reissued | | 9/23/2011 |
| SA02737AT | | Installation of a Hartzell model PHC-C3YF-1RF propeller with F8468AK-8R blades in accordance with Mike Stohler | | Issued | | 10/2/2003 |
| SA02738CH (PAGE 6) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02795AT | | Installation of a PXE7300SR In-Flight Entertainment System | | Issued | | 2/12/2004 |
| SA02930NY | | Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. | | Reissued | | 6/12/2012 |
| SA03122CH | | Increase Maximum Gross weight to 4011 pounds for Normal Category operations | | Issued | | 6/6/2012 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03286CH | | Install an electronic engine ignition system | | Issued | | 1/13/2014 |
| 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 |
| SA08998AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-582 with optional automatic electric trim. | | Amended | | 1/18/2002 |
| SA08999AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-583 with Optional Autotrim System. | | Issued | | 4/27/1995 |
| SA09005SC | | Installation of Trimble 2000 Approach Navigator for nonprecision approach approval. | | Reissued | | 12/21/2001 |
| SA09006AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-584 with Optional Autotrim System. Also eligible on model V35B when modified by STC SA1035WE (turbocharged engine). | | Amended | | 10/9/2001 |
| SA09074SC | | Installation of vortex generators on wing upper surface and vertical stabilizer | | Amended | | 1/23/2013 |
| SA09137AC-D | | Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-611 with Optional Autotrim System. | | Amended | | 4/11/2001 |
| SA09203AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems. | | Amended | | 12/27/2001 |
| SA09206AC-D | | Installation of S-TEC System 30 ALT altitude hold system Model ST-672. | | Issued | | 5/9/1997 |
| SA09254SC | | Increase in maximum takeoff and landing gross weight by 100lbs. when equipped with vortex generators per STC SA09074SC. | | Amended | | 2/21/2013 |
| SA09255SC | | Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E. Inc. STC SA09074SC. | | Reissued | | 6/17/2011 |
| SA09256SC | | Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E. Inc. STC SA09074SC. | | Reissued | | 6/17/2011 |
| SA09311AC-D | | Installation of S-TEC system 30 alt altitude hold system. | | Issued | | 11/21/1997 |
| SA09312AC-D | | Installation of S-TEC System 30 alt altitude hold system. | | Issued | | 11/21/1997 |
| SA09318AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-747-20/30. | | Issued | | 12/29/1997 |
| SA09334SC | | Installation of Magellan Skynav 5000 GPS with Avionics Intl ACF100 and ACF528 cooling fans and AIS80-1 and AIS240-35 switching units | | Reissued | | 1/18/2011 |
| SA09342AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-773-20/30. | | Issued | | 2/20/1998 |
| SA09343AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-774. | | Issued | | 2/24/1998 |
| SA09344AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-749-20/30. | | Issued | | 2/26/1998 |
| SA09361SC | | Installation of Trimble 2000 Approach Plus GPS Navigator. | | Reissued | | 4/5/2002 |
| SA09371AC-D | | Installation of S-TEC System 20/30 Single and Two Axis automatic flight guidance systems Model ST-824-20/30. | | Issued | | 6/10/1998 |
| SA09372AC-D | | Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems Model ST-827-20/30. | | Issued | | 6/11/1998 |
| SA09373AC-D | | Installation of S-TEC System 30 ALT altitude hold system Model ST-828 according to Bulletin No. 928 dated 6/8/98. | | Issued | | 6/12/1998 |
| SA09374AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-825. | | Issued | | 6/18/1998 |
| SA09375AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-833-20/30. | | Amended | | 1/17/2002 |
| SA09376AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-834. | | Issued | | 7/3/1998 |
| SA09410AC-D | | Installation of S-TEC System 50XP Two Axis Automatic Flight Guidance System Model ST-775. | | Issued | | 8/17/1999 |
| SA09416AC-D | | Installation of S-TEC System 40X/50X single and two axis automatic flight guidance systems Model ST-866-40X/50X. | | Issued | | 10/1/1999 |
| SA09418AC-D | | Installation of S-Tec system 40X/50X single and two axis automatic flight guidance systems model ST-778-40X/50X. | | Issued | | 2/22/2000 |
| SA09421AC-D | | Installation of S-TEC system 40X/50X single and two axis automatic flight guidance systems Model ST-780-40X/50X. | | Issued | | 2/21/2000 |
| SA09438AC-D | | Installation of S-Tec system 40X/50X single and two axis automatic flight guidance systems Model ST-784-40X/50X. | | Issued | | 2/23/2000 |
| SA09446AC-D | | Installation of S-TEC GPSS ARINC 429 converter/interface Model ST-901. | | Issued | | 3/30/2000 |
| SA09504AC-D | | Installation of S-TEC Altitude Vertical Speed Selector/Altitude Alerter Model ST-360. | | Issued | | 3/5/2001 |
| SA09528SC | | Installation of a 23-volt 100 ampere alternator. | | Reissued | | 5/17/2013 |
| SA09553SC | | Modification of the ECS s in Bonanza Models F33a A36 and B36TC to convert R12 vapor cycle systems into R134A refrigerant systems. | | Issued | | 6/1/1999 |
| SA09561AC | | Installation of Pilot-side Meggitt EFIS. | | Issued | | 4/22/2002 |
| SA09603SC | | Installation of Teledyne Continental Motors fuel injected engine. | | Amended | | 1/30/2001 |
| SA09619SC | | Installation of Teledyne Continental Motors IIO-550-B engine cooling baffles and propeller. | | Issued | | 8/1/2000 |
| SA09852SC | | Installation of Continental IO-550B engine. | | Amended | | 6/16/2005 |
| 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 | | |
| SA1-354 | | Auxiliary wing tip fuel tanks. | | Reissued | | 2/14/1975 |
| 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 |
| SA1-478 | | 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 |
| SA1-584 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| SA1-587 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| SA1-628 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| SA1-636 | | Install 300 Series dry vacuum pump conversion kits. | | Reissued | | 10/30/1985 |
| SA10004SC | | Installation of Hartzell PHC-C3YF-1RF/F8068 propeller on Raytheon Model S35 V35 V35A V35B 36 A36 35-C33A E33A F33A F33C or G33 with Teledyne Continental Model IO-520-B -BA or | | Reissued | | 3/14/2013 |
| SA1000CE | | Install cabin and engine compart-fire suppression system. | | Reissued | | 12/15/1977 |
| SA10074SC | | Installation of CMI FADEC IOF-550 engine | | Reissued | | 11/6/2013 |
| SA10080SC | | Installation of Hartzell model PHC-C3YF-1RF/F8068 propeller. Aircraft must be equipped with Teledyne Continental Motors IO-520-B IO-550-B or IOF-550-B model engine. | | Issued | | 4/3/2003 |
| 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 |
| SA10135SC | | Installation of Hartzell model PHC-C3YF-1RF/F8068 propeller. Must be equipped with Teledyne Continental Motors IO-520-B IO-520-BA IO-520-BB or IO-550-B model engine. | | Issued | | 4/3/2003 |
| SA10145SC | | Installation of Teledyne Continental Motors Model IO-550-R engine. | | Reissued | | 9/23/2005 |
| SA10145SC-D | | Installation of a Teledyne Continental Motors Model IO-550-R engine | | Amended | | 5/20/2010 |
| SA1022NW | | Installation of a late model instrument panel | | Issued | | 9/12/1980 |
| SA10236SC (4 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1028NW | | Installation of a camera bay in aft cabin (between F.S. 118.5 and 151)and associated systems. | | Amended | | 10/10/1980 |
| SA1033GL | | Installation of Pamco emergency back-up pneumatic system. | | Amended | | 10/12/1989 |
| SA1034GL | | Installation of cooling shroud on engine driven dry air pumps. | | Amended | | 5/1/2007 |
| SA1035WE | | Installation of Continental TSIO-520-D engine in accordance with FAA Sealed AiResearch Drawing No. 101-S35-209. | | Reissued | | 4/25/2011 |
| SA1036EA | | Installation of vertical tail floodlights on upper surfaces of the horizontal stabilizer. | | Reissued | | 2/28/1980 |
| SA10393SC | | Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot | | Amended | | 8/28/2006 |
| 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 |
| SA1069SO | | Installation of Bendix FCS-870automatic flight control system including manual electric pitch trim and optional flight director. | | Issued | | 5/3/1979 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1093CE | | Installation of AP-107 (2 axis)autopilot system and interface with Collins 329A-4V indicator. | | Issued | | 4/1/1975 |
| SA1095CE | | Installation of AP-106 autopilot system and interface with Collins 329A-4V indicator. | | Amended | | 7/1/1975 |
| SA10960SC | | Installation of a built-in oxygen system installed | | Issued | | 11/10/2009 |
| SA1096CE | | Installation of yaw damper system. | | Issued | | 4/1/1975 |
| SA1097CE | | Installation of AP-107 autopilot system and interface with Collins 329A-4V indicator. | | Issued | | 4/1/1975 |
| SA1099GL | | Installation of Pamco emergency backup pneumatic system. (A36TC S/N EA-1 THRU EA-241 EA-243 THRU EA-272 B36TC S/N EA-242 EA-273 THRU EA-439) | | Amended | | 4/11/1989 |
| SA109WE | | M-4 autopilot. | | Issued | | 1/1/1960 |
| SA1103NW | | Installation of a Contental engine Hartzell propeller and associated systems | | Issued | | 11/19/1980 |
| SA1106SO | | Installation of Bendix FCS-870automatic flight control system including manual electric pitch trim and option yaw damper and flight director. | | Issued | | 10/11/1979 |
| SA1112NW | | Installation of a cabin heat boost pump fan | | Reissued | | 11/27/2001 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1113WE | | B-4 flight control system. | | Reissued | | 10/1/1973 |
| SA11151SC | | Installation of an Electromech EM6025 Heat Duct Blower | | Issued | | 9/30/2013 |
| SA1118NW | | Installation of a camera port and an optical port | | Issued | | 12/19/1980 |
| SA112EA | | AF-510A AF-512A or AF-512B autopilots. | | Issued | | 1/1/1960 |
| SA1140CE | | Installation of a 2-axis autopilot system with a King compass and a flight command indicator or an altitude horizon indicator with a mode controller. | | Reissued | | 2/28/2000 |
| SA1145CE | | Installation of King Model KFC-200 2 axis (3 optional) or stand alone yaw damper for Beech Model A36S/N E572 and later autopilot system with a King KI-255(KI-256optional) flight command indicator with the KC-292 mode controller. | | Reissued | | 2/28/2000 |
| SA1150WE | | Gyro sense element relocated to remote position. | | Reissued | | 10/1/1973 |
| SA1154NW | | Approval of a gross weight increase to 3400 pounds | | Issued | | 1/9/1981 |
| SA115CE | | Turbo volt Model Three-Five emergency electrical and vacuum system. | | Issued | | 5/4/1980 |
| SA1163NW | | Installation of a camera port and a view finder hole | | Issued | | 2/2/1981 |
| SA1164CE | | Installation of King KFC-200 two axis autopilot system with King KI-255 (or -256) flight command indicator or King KG-258 altitude horizon indicator with a KC-292mode controller. | | Reissued | | 2/28/2000 |
| SA1166GL | | Installation of McCauley Model 3A32C406/82NDB-2 propeller in accordance with the appropriate installation instruction drawing as determined by Master Eligibility List No. PR0P406 Rev. A dated February 5 1987 or later FAA approved revision. | | Reissued | | 6/17/2011 |
| SA1176SO | | Installation of Aileron and Wing Flap Gap Seals | | Amended | | 1/6/2010 |
| SA1185CE | | Installation of Collins AP-107 (2 axis) autopilot system and interface with Collins FD-112V flight director. | | Issued | | 4/1/1976 |
| SA1186CE | | Installation of Collins AP-107(2 axis) autopilot system and interface with Collins FD-112V flight director. | | Issued | | 4/1/1976 |
| SA11GL | | Installation of Cleveland 6.00-6wheels and brakes conversion kit 199-49. | | Amended | | 9/2/1987 |
| SA1204NW | | Installation of a recalibrated dial face on the United Instruments Fuel Flow Gauge | | Issued | | 3/27/1981 |
| SA1211SO | | Installation of an adjustable trim tab on left aileron. | | Amended | | 11/23/1994 |
| SA1218SW | | Automatic flight system AK306cons. of Century I and optional tracking system. | | Reissued | | 7/9/1984 |
| SA1219NW | | Installation of an extended baggage compartment and hat shelf | | Issued | | 4/30/1981 |
