| SA00024NY | | Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. | | Amended | | 10/3/2012 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00068SE (PAGE 2) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 0:00 |
| 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 |
| SA00229NY | | Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. (PA-23-250 6 place) | | Amended | | 1/24/1997 |
| 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 |
| 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 ( PAGE3) | | 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 |
| SA00376SE | | Install vortex generators on the wings and vertical tail. | | Amended | | 2/19/1997 |
| SA00393SE | | Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. | | Issued | | 12/6/1996 |
| 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 |
| SA00448DE | | Installation of Oilamatic preoiler system. | | Amended | | 4/14/2003 |
| SA00519AT-D | | Installation of replacement fuel cell assemblies | | Reissued | | 4/16/2009 |
| SA00520AT-D | | Installation of fuel ramp assemblies | | Reissued | | 5/5/2009 |
| SA00621LA | | Installation of an electronic digital engine tachometer horizon model P-1000. | | Amended | | 1/14/2002 |
| SA00674WI-D | | Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation. | | Amended | | 7/23/2012 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00680SE (5 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00695SE | | Replacement of certain Rotomaster and Rayjay scavenge pumps | | Amended | | 2/14/2003 |
| SA00721CH | | Installation of a Hartzell HC-C2YL-2CUF/FC7663-4 propellers and 836-29(P) spinners. | | Issued | | 7/29/1997 |
| 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 |
| SA00733AT | | Installation of composite aft spinner bulkhead and/or composite spinner. | | Amended | | 3/31/2004 |
| SA00734LA | | Installation of modified exhaust system. (PA-23-250 27-2505 and up) | | Issued | | 2/19/1999 |
| SA00743SE | | Installation of vortex generators on the wing leading edge underside of the horizontal stabilizer and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117 Revision IR dated July 14 1999 and Installation Instructions MA2118 Revision IR dated September 21 1999 or later FAA approved revisions to either of these documents.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( NOTE: If more than five vortex generators are damaged or missing the aircraft is not airworthy | | Amended | | 4/27/2004 |
| SA00762AT | | Installation of left hand and right hand fuel cell assemblies. (S/N 7654001 and up) | | Reissued | | 4/27/2009 |
| SA00769CH | | Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540 AEIO-540 and HIO-540 engines. | | Reissued | | 2/10/2009 |
| SA00780SE (PAGE 1) | | Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. | | Amended | | 5/11/2010 |
| SA00800AT | | Installation of left hand and right hand fuel cell assemblies. (PA-23-250 S/N 7554001 AND UP) | | Reissued | | 4/27/2009 |
| SA00804SE | | Installation of an engine failure indicator system also referred to as a low Thrust Detector system. | | Amended | | 7/16/2000 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| 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 |
| SA00971CH | | Remove South Wind 940 series combustion heater and install C&D Asociates TSO-C20 approved heater kit model CD35K or CD45K (310A (USAF U-3A) S/N 35000 trhu 35546 PA-23 S/N 23-1 and up 27-1 thru 27-3049 27-3051 thru 27-3053 PA-30 S/N 30-2 thru 30-401) | | Amended | | 3/29/2004 |
| SA01026SE (PAGE 1) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01057AT | | Installation of Composite skinner. | | Amended | | 10/13/2000 |
| SA01058AT | | Installation of Composite spinner. | | Amended | | 10/13/2000 |
| SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01105WI-D (2 OF 2) | | Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). | | Amended | | 5/31/2007 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01120SE | | Installation of Door Steward. | | Amended | | 3/4/2010 |
| SA01141WI-D | | Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head. | | Amended | | 5/24/2006 |
| SA01147WI | | Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. | | Reissued | | 7/30/2012 |
| 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 |
| SA01237AT | | Installation of fuel cell drain kit. | | Reissued | | 3/6/2000 |
| SA01240SE (4 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01250AT | | Installation of left hand and right hand tip fuel cell assemblies. (PA-23-250 S/N 7654001 AND UP) | | Reissued | | 4/29/2009 |
| SA01263AT | | Installation of Composite Spinner. | | Amended | | 10/13/2000 |
| 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 |
| SA01303AT | | Installation of OCEM AP-3C autopilot. | | Amended | | 11/16/2005 |
| SA01306WI-D | | Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation. | | Amended | | 2/28/2007 |
| SA01330LA (PAGE 2) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
| SA01349NY | | Installation of oil temperature coupler kit P/N ALH-I-005 with Airparts Installation Drawing List as listed on AML No. Sa01349NY. | | Issued | | 5/15/2001 |
| SA01435DE | | Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine. | | Reissued | | 5/25/2011 |
| SA01473SE (4 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 2) | | 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 |
| SA01566CH | | Installation of C&D Associated combustion heater kit P/N CD11005K1 and CD11006K2. | | Amended | | 11/1/2004 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01686SE | | Fabrication and installation of engine control levers. | | Reissued | | 5/7/2009 |
| 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 |
| SA01800SE (PG 3) | | 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 3) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01988SE (PAGE 5) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA02013CH | | Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). | | Amended | | 5/2/2011 |
| SA02015SE-D | | Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. | | Amended | | 2/5/2014 |
| SA02018SE-D (PAGE 2) | | Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D dated January 4 2011 or later FAA approved revision and FAA Approved GPS/XM Antenna STC Master Drawing List Document No.: 005-00638-01 Revision 1 | | Issued | | 1/4/2011 0:00 |
| SA02019SE-D Page 2 | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/19/2012 |
| SA02033AT (PAGE 3) | | 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 |
| SA02096AK | | Installation of hourmeter airspeed switch. (PA-23-250 Navy UO-1) | | Issued | | 12/17/1997 |
| SA02110CH (PAGE 2) | | Installation of a Time Trac Data Recorder | | Reissued | | 1/11/2010 |
| SA02119SE Page 2 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
| 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 |
| SA02203AK (PAGE 1) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02212AK (PG 3) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. | | Amended | | 5/4/2011 |
| 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 |
| SA02243CH | | Install enlarged rear baggage area to accommodate skis. | | Issued | | 3/2/2007 |
| 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 |
| SA02268CH (PAGE 5) | | 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 (1 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02298CH | | Installation of a Three Point Torso Restraint System | | Issued | | 6/15/2006 |
| SA02334NY | | Provide improved access to the engines during the maintenance process. | | Issued | | 1/29/2007 |
| SA02410AT | | Replace existing Auxiliary Electric Standby Fuel Pump with PMA Products Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v) 1A15-s/n 24-3642 24-4000 through 24-4782 24-4784 through 24-4803 2A13-s/n 28-7690001 through 28-7990626 28-8090001 and up(14v) | | Issued | | 10/10/2001 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02532AT | | Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. | | Issued | | 6/5/2002 |
| SA02547AT (PG 2) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| SA02655AT (2 OF 2) | | Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. | | Amended | | 9/1/2004 0:00 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 2) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02795AT | | Installation of a PXE7300SR In-Flight Entertainment System | | Issued | | 2/12/2004 |
| SA02874CH-D | | Installation of Hartzell HC-E2YR-2BTF/FC7693F(B)+1 propellers | | Issued | | 12/14/2010 |
| 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 |
| SA02987CH | | Installation of the Electroair Electronic Ignition System | | Amended | | 7/23/2013 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09119AC-D | | Installation of S-TEC System 65 Two Axis automatic flight guidance system Model ST-601. | | Issued | | 9/20/1995 |
| SA09123AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-607 with Optional Autotrim System. Limited to Piper models PA-23-250 and PA-E23-250 s/n 27-2000 through s/n 27-7554172. Eligible on same models when equipped with approved turbocharged engines (250 hp) and/or wing tip tanks per STC SA1480WE. | | Amended | | 8/29/2007 |
| SA09198AC-D | | Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System Model ST-662. Installation of S-TEC System 55X Two Axis Automatic Flight Guidance System Model ST-662-1. Eligibility limited to Piper models PA-23-250 and PA-E23-250 s/n 27-2000 through 27-7554172. | | Amended | | 4/18/2007 |
| SA09503AC-D | | Installation of S-TEC System 20/30 single and two-axis automatic flight guidance system Model ST-882-20/30. | | Issued | | 10/5/2000 |
| SA1-103 | | Radio-shelf. | | Issued | | |
| SA1-117 | | Propeller anti-icing kit. | | Issued | | |
| SA1-120 | | F-300 automatic pilot. | | Issued | | |
| SA1-137 | | Installation of Tactair T-3 automatic pilot and optional installation of Tactair AH-1 altitude hold device (for use with Tactair T-3 autopilot). | | Reissued | | 8/7/1972 |
| SA1-169 | | Reinforcement of floor structure between fuselage station 91-1/2 and 123-3/4 and provision for tie-down facilities. | | Issued | | |
| SA1-177 | | Lightweight reservoir type pneumatic deicing system. | | Reissued | | 3/1/1996 |
| SA1-28 | | Radio rack limited to 30 pounds of radio equipment. | | Issued | | |
| SA1-383 | | Lube oil filter PB 55-1. | | Issued | | |
| SA1-484 | | Electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
| SA1-485 | | Install electrothermal propeller deicing system. (PA-23-250 5 OR 6 PCLM) | | Reissued | | 3/1/1996 |
| SA1-5 | | Unfeathering system change to HC-82XL-2/7636D-4 or HC-A2XL-2/7636D-4 propellers. | | Amended | | |
| SA1-53 | | Conversion to Goodyear 6.50-8 wheels (9531319) and brakes(9531779). | | Amended | | 1/1/1960 |
| SA1-534 | | Installation of BFGoodrich lightweight reservoir type deicing system. | | Reissued | | 3/1/1996 |
| SA1-548 | | SP-3 autopilot EB2597034. | | Amended | | 1/1/1960 |
| SA1-586 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| SA1-6 | | Unfeathering system change to HC-82XG-2/7636D-4 propellers. | | Amended | | 1/1/1960 |
| SA1004GL | | Install a FLIR 2000A pod and a miniature CCD camera or a color TV camera. | | Reissued and Amended | | 9/28/1987 |
| SA1007NW | | Installation of a low thrust detector system. | | Reissued | | 3/6/1998 |
| SA100SW | | Automatic pilot AK114. | | Issued | | 1/1/1961 |
| SA10126SC (2 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 |
| SA1022CE | | Installation of King Model KGS-55 pictorial navigation system(compass) with optional KA-52 autopilot adapter. | | Reissued | | 2/28/2000 |
| SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1027CE | | Installation of KCS-55 pictorial navigation system (compass) with optional KA-57 autopilot adapter. | | Reissued | | 2/28/2000 |
| SA1054SW | | Stretcher. | | Reissued | | 11/7/1983 |
| SA1063CE | | Installation of two Hartzell HC-E3YR-2AF/FC7663-2R propellers and C-3269A or 82D3273P spinners. (PA-23-250 LANDPLANES S/N S 27-2505 THRU 27-74-05471) | | Reissued | | 2/3/1983 |
| SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
| SA1076CE | | Installation of Halon 1301 cabin fire extinguishing system and engine nacelle fire extinguishant distribution system. | | Reissued | | 12/15/1977 |
| 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 |
| SA1091SW | | Mitchell automatic flight system FD/AP 282-184 consisting of flight director/autopilot with optional automatic electric pitch trim and automatic aileron stabilizer. | | Reissued | | 7/9/1984 |
| SA1102CE | | Installation of AP-107 2-axis autopilot system and interface with Collins 329A-4V indicator. | | Issued | | 4/1/1975 |
| SA1103CE | | Installation of AP-107 autopilot system and interface with Collins329A-4V indicator. | | Issued | | 4/1/1975 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1124EA | | Installation of enlarged cargo door in accordance | | Reissued | | 4/11/2013 |
| SA1126EA | | Installation of DeVore vertical tail floodlights on upper surface of stabilator. (PA-23-250 S/N 271 THRU 27-7554172 PA-E23-250 S/N 27-2505 THRU 27-7554172) | | Reissued | | 9/28/1978 |
| SA1162EA | | Installation of Silver Instruments fueltron IIIG or IIIP digital fuel flow and totalizer system | | Reissued | | 4/29/1991 |
| SA1162GL | | Install a BF Goodrich LRN500 or LRN500(501) or F4 or F4(F14) long range navigation system. | | Reissued | | 1/31/1992 |
| SA1163CE | | Installation of KFC-200 automatic flight control system (2 axis) with or without flight command indicator. | | Reissued | | 2/28/2000 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA11NE | | Installation of laser sensor system. | | Issued | | 10/31/1975 |
| SA1202WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1205SW | | Installation of Mitchell command electric trim model AK268. | | Reissued | | 7/9/1984 |
| SA1260WE | | Installation of turbocharged Lycoming O-360-A1A or A1D engines. | | Reissued | | 6/26/2006 |
| SA1262SW | | Mitchell automatic flight system FD282-242 consisting of flight director/autopilot and automatic pitch trim. | | Reissued | | 7/9/1984 |
| SA1276SW | | Mitchell automatic flight system AK332 consisting of Piper Autoflite II and omni tracker system. | | Reissued | | 7/9/1984 |
| SA1294SW | | Installation of fiberglass tail cone. | | Reissued | | 10/10/1997 |
| SA1306SW | | Installation of Lycoming IO-360-C1C engines with Hartzell HC-C2YK-2/C7666A-4 propellers with gross weight increase. | | Reissued | | 12/27/1999 |
| SA1314SW | | Installation of Fiberglass extended nose. | | Reissued | | 12/27/1999 |
| SA1315SW | | Installation of fiberglass dorsal fin. | | Reissued | | 12/27/1999 |
| 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 |
| SA1348WE | | B-4 flight control system. | | Reissued | | 10/20/1972 |
| SA1349GL | | Install combustion heater. | | Issued | | 2/8/1989 |
| SA1350GL | | Replace existing combustion heater. | | Issued | | 2/8/1989 |
| SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
| SA1361CE | | Chrome plated brake disc installation. | | Issued | | 3/6/1978 |
| SA136EA | | Installation of Monitair angle of attack system Model AA-2. | | Reissued | | 2/14/1972 |
| SA1377SW | | Mitchell automatic flight system AK340 consisting of Century I and optional tracker. | | Reissued | | 7/10/1984 |
| SA1390CE | | Install 1/4-inch plywood flooring over existing floor remove 4 passenger seats install reinforce- ment tubing. | | Amended | | 8/6/1979 |
| SA1391CE | | Cutting and reattaching the left and right lower engine cowling with AN 2700-4 cam locks. | | Amended | | 8/6/1979 |
| SA140SW | | Cabin window addition. | | Reissued | | 7/15/2010 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1444WE | | Installation of Edo Model 679-4930 floats and addition of left-hand passenger entry door. (PA-23-250 S/N 27-2505 AND UP) | | Reissued | | 5/20/1982 |
| SA1448GL | | Replace existing combustion heater with C&D Airmotive combustion heater P/N 1059. | | Issued | | 2/6/1990 |
| SA1449GL | | Install combustion heater P/N 1059. | | Issued | | 2/6/1990 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| SA1480WE | | Installation of an integral 24 gallon auxiliary fuel tank in each wing tip. | | Amended | | 6/14/2002 |
| SA1486WE | | Installation of Brittain Industries Inc. Model B2C Flight Control System | | Reissued | | 1/29/2013 |
| SA148SW | | Replacement of right front seat with stretcher. | | Reissued | | 8/21/1987 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1524SW | | Mitchell automatic flight system AK371 consisting of altimatic IIIB-1 autopilot with optional radio and glide slope couplers. | | Reissued | | 7/13/1984 |
| SA1527SO | | Installation of seat tracks and seats. | | Amended | | 3/7/1984 |
| SA1532GL | | Installation of on-board engine analyzer system. | | Issued | | 11/14/1990 |
| SA1554CE-D | | Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director installed under STC SA1163CE. | | Reissued | | 2/28/2000 |
| SA155EA | | Install B.F. Goodrich pneumatic de-icing system. | | Reissued | | 3/1/1996 |
| SA1571SW | | Mitchell automatic flight system AK382 consisting of Piper auto- control IIIB with optional radio coupler. | | Reissued | | 7/13/1984 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1585SO | | Installation of engine fire detection system. | | Reissued | | 9/24/1984 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA162SW | | Installation of cabin emergency exit window and sixth seat. | | Reissued | | 10/10/1997 |
| SA164CE | | Installation of Hartzell HC-A3XK-2B/7636D-4 Propellers and C-2513-2P spinners. Data required: Doyn Dwg. 2100 dated August 5 1963.
);INSERT INTO stc_table VALUES ( | | Reissued | | 7/14/2011 |
| SA1653SW | | Mitchell automatic flight system AK372 consisting of AutoFlite II with optional tracking system. | | Reissued | | 7/16/1984 |
| SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
| SA172EA | | Reinforcement of rearmost seat and installation of additional safety belt. (PA23-250 s/n 27-2000 and up) (N2T-1 S/N 27-2000 AND UP) | | Issued | | 1/1/1960 |
| SA1798CE | | Installation of fire extinguishing system in cabin and/or fire extinguishant system in engine compartments. | | Reissued | | 2/1/1993 |
| SA179CE | | Installation of the following: Engines: Lycoming IO-540-A1A5 or Lycoming IO-540-G1A5 Propellers: Hartzell HC-A3XK-2C/8433-10 or HC | | Reissued | | 7/14/2011 |
| SA1810WE | | Installation of left-hand passenger entry door. | | Reissued | | 5/20/1982 |
| SA1845WE | |
);INSERT INTO stc_table VALUES ( Installation of Vibration Isolation Products (VIP) engine mount P/N VIP-50804-20 on various aircraft as shown on FAA Approved Model List (AML) No. SA1845WE. | | Amended | | 10/17/2002 |
| SA1847WE | | Installation of Brittain Up-Command Signal Adapter Kit. | | Reissued | | 10/20/1972 |
| SA188SO | | Flight control wheel. | | Issued | | 1/1/1960 |
| SA195EA | | Installation of Goodrich Electro- thermal propeller de-icing system kit 77-170. (PA-E23-250 S/Ns 27-2505 and up) | | Reissued | | 3/1/1996 |
| SA2-1533 | | Installation of windshield wiper. | | Reissued | | 1/31/1997 |
| SA2-17 | | Installation of a 17-1/4 inch diameter camera mount ring. Approved for serial number 23-118 ONLY. | | Reissued | | 12/1/1999 |
| SA2-21 | | Installation of landing lights in outer wing leading edge. | | Reissued | | 6/26/2001 |
| SA2020CE | | Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. | | Issued | | 8/10/1984 |
| SA202SO | | Fyr-Fyter 23-4 2 1/2 lb. dry chemical fire extinguisher. | | Issued | | 1/1/1960 |
| SA2051NM | | Installation of a ARNAV Systems AVA-1000 Loran C Navigation System | | Amended | | 6/24/1983 |
| SA205GL | | Installation of Aerosonic totalize fuel flow indication system in lieu of fuel pressure gages. | | Issued | | 12/19/1977 |
| 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 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA219EA | | Installation of Katz integrated flight indicator Model KIFI-2 or KIFI-2A. | | Amended | | 5/21/1969 |
| SA230CE | | Airspeed indicator landing gear warning system. | | 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 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2357CE | | Installation of LH and RH main fuel tank bladder cells P/N s DF054-320 and DF054-321 as replacements for original bladders. | | Reissued | | 7/31/2002 |
| SA236CE | | Installation of Hoskins Supplemental Model B High intensity wing tip lights Model C tail lights with or without Model 2 high intensity fuselage lights. | | Reissued | | 9/30/2011 |
| SA242SO | | Two-place couch. | | Issued | | 1/1/1960 |
| SA243EA | | 13-quart propeller anti-icing kit WAP-102. | | Issued | | 1/1/1960 |
| SA2442WE | | Installation of dual hydraulic pump. | | Reissued | | 9/8/2005 |
| SA2445WE | | Installation of recontoured inboard wing leading edge stall fences drooped ailerons in flaps down mode rudder anti-servo tab system. | | Reissued | | 9/8/2005 |
| SA244SO | | PA-23-250 wing root and nacelle fairings. | | Issued | | 1/1/1960 |
| SA250WE | | Dorsal fin. | | Issued | | 1/1/1960 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA2586NM (PAGE 4) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2598CE | | Operation of airplane on unleaded and leaded automotive gasoline 91 minimum antiknock index(RON+MON)/2per ASTM Specification D-439. Inter-mixing with aviation gasoline also approved. | | Issued | | 3/30/1990 |
| SA25GL | | Installation of propeller unfeathering accumulator kit number 213632. | | Reissued | | 3/20/1992 |
| SA266SO | | Modification of fuel cap 16097-00 by making a new cover and enlarging the lower vent hole. Rework fuel cell filler neck door 19049-06 by putting a spring loading vent in the door to be used as auxiliary vent during icing conditions. | | Issued | | 1/1/1960 |
| SA2687NM (PAGE 1) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 |
| SA268WE | | Sixth seat and emergency exit. | | Issued | | 1/1/1960 |
| SA2693NM (PAGE 2) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 0:00 |
| SA2720SW | | Installation of wing root fairings. | | Reissued | | 4/16/1999 |
| SA272CE | | Installation of Lycoming IO-360-B1A engines and Hartzell HC-C2YK-2RA/7666A-2 propellers. Gross weight increase to 4000 lbs. Data required: Eight photographs for Doyn 180 HP Piper Apache | | Reissued | | 7/14/2011 |
| SA2793SW | | Installation of rubber hinge reinforcing bracket. | | Reissued | | 10/10/1997 |
| SA280SW | | Forward fuselage section and long nose 30542-02. | | Issued | | 1/1/1960 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA285CE | | Installation of Lycoming IO-360-B1B engines and Hartzell HC-C2YR-2RA/7666A-2 propellers. Gross weight increase to 3684 lbs on PA-23 and 4000 lbs on PA-23-160. Data required: PA-23: Doyn dwg 1500 Rev. C except for Hartzell HC-922K-2B/8447-12A props. Doyn dwg 1507 Rev. C PA-23-160: Doyn dwg. 1800 Rev. C except for Hartzell HC-922K-2B/8447-12A props. Dwg. 1807 Rev. C. | | Reissued | | 7/14/2011 |
| SA2914WE | | Installation of improved rudder trim tab actuating rod. | | Reissued | | 4/25/2001 |
| SA2950SW | | Addition of Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
| SA29CE | | Lycoming O-360-A1D engine with Hartzell HC-92ZK-2B/8447-12A or HC-C2YK-2R/7666-4 propellers. | | Reissued | | 3/9/1979 |
| SA2CE | | Installation of Doyn Model 1600 Dorsal Fin per Doyn Drawing No. 1600 Revision A dated January 5 1962. | | Reissued | | 8/16/2011 |
| SA2WE | | Installation of fuel pressure warning lights | | Reissued | | 5/3/2006 |
| SA3-158 | | Radio power pack on bulkhead forward of instrument panel. | | Issued | | 1/1/1960 |
| SA3-334 | | Installation of aerial camera provisions. Limited to Restricted Category with camera installed. | | Reissued | | 6/26/2001 |
| SA3-397 | | Petch Manufacturing Company right or left-handy hydrotrim aileron trim device. | | Issued | | 1/1/1960 |
| SA3-509 | | L-2B autopilot with or without altitude control and approach coupler. | | Issued | | 1/1/1960 |
| SA3-564 | | This approval provides for the installation of a Woodward Governor propeller unfeathering accumulator kit number 210313. | | Reissued | | 3/20/1992 |
| SA3-641 | | Corporation cabin air temperature control system. | | Reissued | | 2/9/1982 |
| SA3-644 | | Adams Rite 2302 rev. C-2 handle on inside of cabin door. | | Issued | | 1/1/1960 |
| SA3-728 | | Lycoming O-360-AID engines with Hartzell HC-92ZK-2B/8447-12A or HC-C2YK-2R/7666-4 propellers and increase gross weight to 3 684 lbs. | | Issued | | 1/1/1960 |
| SA3-94 | | Narco 1016 antenna and/or remote compass transmitter equipment shelf oxygen bottle mounting. | | Issued | | 1/1/1960 |
| SA3002SW-D | | Mitchell automatic flight system AK479 consisting of Piper Altimatic IIIC autopilot with optional command/automatic electronic pitch trim system radio coupler and glide slope coupler. | | Reissued | | 8/1/1984 |
| SA3003SW-D | | Mitchell automatic flight system AK477 consisting of Century IV autopilot or AK477FD consisting of a Century IV flight director with optional remote annunciator. | | Reissued | | 8/1/1984 |
| SA3005SW-D | | Installation of Mitchell automatic flight system model AK508 consisting of Piper autocontrol IIIB autopilot with optional radio coupler. | | Reissued | | 6/20/1984 |
| SA3006SW-D | | Mitchell automatic flight system AK494 consisting of Century IV autopilot or AK494FD consisting of a Century IV flight director with optional remote annunciator. | | Reissued | | 8/1/1984 |
| SA3007SW-D | | Installation of Mitchell automatic flight system model AK504 consisting of Piper altimatic IIIC autopilot with optional command/automatic electronic pitch trim radio coupler and glide slope coupler. | | Issued | | 6/20/1984 |
| 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 |
| SA3022SW-D | | Installation of Mitchell automatic flight system model AK517 consisting of Autocontrol IIIB autopilot with optional radio coupler. | | Reissued | | 6/20/1984 |
| SA3027SW-D | | Mitchell command/electric trim system Model AK440. | | Reissued | | 8/1/1984 |
| SA308EA (2 OF 2) | | Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) | | Amended | | 11/20/1978 0:00 |
| SA3099SW-D | | Mitchell automatic flight system AK587 consisting of Century I auto-pilot with optional omni tracker. | | Reissued | | 6/20/1984 |
| SA309WE | | Installation of non-icing fuel tank vents. | | Reissued | | 4/26/1991 |
| SA3100SW-D | | Mitchell automatic flight system AK588 consisting of Century III autopilot with optional radio coupler and glide slope coupler. | | Reissued | | 5/24/1984 |
| SA3101SW-D | | Mitchell automatic flight system AK586 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 5/24/1984 |
| SA3104SW-D | | Mitchell automatic flight system AK583 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 5/24/1984 |
| SA311SW | | Alternate static source. | | Issued | | 1/1/1960 |
| SA3133SW-D | | Mitchell automatic flight system AK599 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/5/1984 |
| SA3137SW-D | | Mitchell automatic flight system AK611 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/5/1984 |
| SA3155SW-D | | Installation of Mitchell automatic flight system model AK626 consisting of Century III autopilot with optional radio coupler and glide slope coupler. | | Reissued | | 6/6/1984 |
| SA3156SW-D | | Installation of Mitchell automatic flight system model AK627 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/6/1984 |
| SA316SO | | Carburetor ice detector. | | Amended | | 10/5/1966 |
| SA317EA | | Radome kit No. 2025K-B for Bendix RDR-100 or RDR-110 series radar systems with 12-inch antenna per Chamberlain installation. | | Reissued | | 3/21/1974 |
| SA319EA | | Install electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
| SA3209SW-D | | Mitchell automatic flight system Piper altimatic X autopilot AK684 or AK684FD Piper altimatic X flight director autopilot with remote annunciator. | | Reissued | | 12/7/1983 |
| SA3285NM | | Installation of ARNAV Systems FC-10/FT 10 digital fuel flow indicating system. | | Issued | | 11/24/1986 |
| SA3290WE | | Installation of Pathfinder auto- pilot systems and/or pitch trim systems. | | Reissued | | 9/30/1998 |
| SA334SW | | Installation of InterAv Alternator. | | Reissued | | 7/20/1981 |
| SA335CE | | Installation of Honeywell H-14 YG-391 autopilot. | | Amended | | 9/9/1966 |
| SA337EA | | Conversion of aircraft electrical system to 24 volt. (PA-23-250 SN 27-2505 and up) | | Issued | | 1/1/1960 |
| SA339SW | | Electrical hydraulic pump. | | Reissued | | 9/20/1977 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3581NM | | Installation of electric heater and auxiliary alternator. (PA-23-250 SN 27-7654001 & up) | | Issued | | 3/17/1987 |
| SA362SW | | Installation of rear baggage compartment. | | Reissued | | 10/10/1997 |
| SA363SW | | Pitch trim system AK128. | | Issued | | 1/1/1960 |
| SA371SW | | Installation of fiberglass nose cone. | | Reissued | | 10/10/1997 |
| SA376WE | | Left and right third window. | | Issued | | 1/1/1960 |
| SA3823WE | | Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA3843SW | | Installation of electrical propeller deicing boots. | | Reissued | | 10/10/1997 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA387WE | | Sixth seat and escape hatch. | | Issued | | 1/1/1960 |
| SA394WE | | Replacement engine nose cowls. | | Issued | | 1/1/1960 |
| SA395WE | | Lycoming O-360-A1A engines and Hartzell HC-C2YK-2R/7666-2 propellers. | | Issued | | 1/1/1960 |
| SA398CE | | Install Hoskins Twilighter MK III Supplemental Lighting System consisting of Model F Wing Lights with Model P or K (dual) Tail Light. | | Reissued | | 9/30/2011 |
| SA39RM | | Installation of freon air-conditioner | | Reissued | | 5/17/2013 |
| SA4-1016 | | Installation of Lycoming 160 hp O-340-A1A engines and Hartzell HCB2XG-2B/8433-12 propellers | | Reissued | | 4/8/1991 |
| SA4-1131 | | SP-3 autopilot less altitude and navigation hold features. | | Issued | | 1/1/1960 |
| SA4-1166 | | Installation of Firestone Model DFA-180 wheel. | | Reissued | | 6/25/2003 |
| SA4-1501 | | AB-6562 and AB-6563 brake blocks. | | Issued | | 1/1/1960 |
| SA4-1602 | | Dorsal fin. | | Issued | | 1/1/1960 |
| SA4-1637 | | Installation of Turbocharged Lycoming 0-320-A or | | Reissued | | 7/3/2006 |
| SA4-299 | | Windows at station 144. | | Issued | | 1/1/1960 |
| SA4-345 | | B Arcon. | | Issued | | 1/1/1960 |
| SA4-522 | | Autopilot. | | Reissued | | 10/1/1973 |
| SA4-652 | | Full flow aerofilter kit 3-1A101. | | Issued | | 1/1/1960 |
