| SA00013SE | | Installation of vortex generators stall fences and strakes. | | Reissued | | 11/23/2009 |
| SA00014AT | | Installation of Lycoming model L/TIO-540-J2B engines in accordance with Colemill Enterprises Inc. Installation Instructions for Modification of Piper Navajo Model PA-31-350 | | Reissued | | 2/10/2011 |
| 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 |
| SA00037SE | | Vortex generators manufactured and installed. | | Reissued | | 11/23/2009 |
| SA00038SE | | Vortex generators manufactured and installed. | | Reissued | | 11/23/2009 |
| SA00039SE | | Vortex generators manufactured and installed. (T-1020) | | Issued | | 11/23/2009 |
| SA00047SE | | Vortex generators manufactured and installed. | | Amended | | 5/30/2013 |
| SA00048SE | | : Vortex generators manufactured and installed. | | Amended | | 5/30/2013 |
| SA00057WI | | Installation of single place composite commuter seats on the seat rail. This STC approves only the installation of the parts contained in the Description of Type Design Change section. The requirements for the aisle width passenger oxygen system seats and safety belts and upholstery coverings require a separate FAA approval. | | Amended | | 10/22/2003 |
| 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 |
| SA00126SE | | Installation of strakes to sides of engines nacelles and vortex generators to the wing upper surface the vertical tail and the lower surface of the horizontal tail | | Reissued | | 5/15/1997 |
| 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 |
| SA00192SE | | Vortex generators manufactured and installation of the Super Chieftain I takeoff weight increase kit | | Amended | | 5/30/2013 |
| SA00202SE | | Installation of landing weight increase kit. | | Reissued | | 11/23/2009 |
| 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 |
| SA00307AT | | Install an Aero Support engineering propeller bulkhead assembly. | | Issued | | 8/12/1993 |
| SA00336AT | | Installation of winglets. | | Reissued | | 2/10/2011 |
| SA00347NY | | Installation of shoulder harness. | | Issued | | 7/10/1995 |
| SA00360NY | | Installation of Janitrol Heater Models C39D59 or 45D70-1. | | Amended | | 2/5/1998 |
| SA00378SE | | Boundary Layer Research Inc Wing Rib Reinforcement Modification. (and T-1020) | | Reissued | | 11/23/2009 |
| SA00422SE | | Installation of Lycoming TIO-540-J2B(left side) or LTIO-540-J2B (right side). | | Issued | | 3/28/1997 |
| 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 |
| SA00505SE | | Installation of SMR technologies pneumatic de-icers. | | Amended | | 6/22/2009 |
| SA00528SE | | Installation of emergency medical stretcher and base oxygen and electrical systems. | | Amended | | 7/27/2004 |
| SA00554AT | | Installation of composite aft spinner bulkhead and/or composite spinner. | | Amended | | 10/13/2000 |
| SA00555DE | | Replacement of inboard main landing gear door with an aerodynamic fairing. | | Reissued | | 2/21/2008 |
| SA00608NY | | Installation of tail stinger elevator modification equipment rack and video camera. (PA-31 S/N 31-639) | | Issued | | 4/23/1997 |
| SA00632AT | | Installation of Dayton-Granger dischargers. | | Reissued | | 4/13/1995 |
| 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 |
| SA00681WI-D | | Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I 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 | | Reissued | | 1/25/2011 |
| SA00694NY | | Installation of geophysical tail boom. | | Issued | | 10/17/1997 |
| 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 |
| SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
| SA00775NY | | Install equipment rack. | | Issued | | 12/15/1997 |
| 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 |
| SA00801AT | | Installation of left hand and right hand fuel cell assemblies. | | Reissued | | 7/29/2002 |
| SA00804SE | | Installation of an engine failure indicator system also referred to as a low Thrust Detector system. | | Amended | | 7/16/2000 |
| SA00857CH | | Installation of McCauley Propeller Model B3DF36C526/80HJA-0 and B3DF36C527/L80HJA-0 spinner assembly and optional de-icer. | | Reissued | | 9/23/2005 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00940AT | | Installation of an ADF antenna system. | | Issued | | 1/5/1996 |
| 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 |
| SA00961WI | | Stretcher installation per Aviation Fabricators STC Drawing List AF-204 Rev A dtd 7/7/97 stamped FAA Approved with an approval date of 4/13/01 or later FAA approved revision. | | Amended | | 2/1/2010 |
| SA00963WI | | Installation of a heated windshield panel using Aviation Fabricators STC Data Package AF-295 Rev (-) dated 11/17/98 stamped Faa Approved with an approval date of 4/24/01 or later FAA approved revision. | | Issued | | 4/24/2001 |
| SA01005AT | | Installation of left and right hand side fuel cell assemblies. | | Reissued | | 5/1/2009 |
| SA01035AT | | Installation of an HF antenna system. | | Issued | | 5/10/1996 |
| 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 |
| SA01143AT | | Installation of left hand side and right hand side main tank fuel cell assemblies. (PA-31-350 S/N 5 THRU 7300923) | | Reissued | | 5/5/2009 |
| SA01147WI | | Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. | | Reissued | | 7/30/2012 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01161WI-D | | Installation of the Bendix/King KFC 225 Flight Control System. | | Issued | | 4/4/2003 |
| 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 |
| SA01229NY | | Installation of SLFMR Microwave Radiometer Pod. | | Reissued | | 5/28/2001 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (4 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01280CH | | Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) | | Issued | | 8/29/2000 |
| SA01330LA (PAGE 2) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
| SA01384CH | | Installation of various de-icer harnesses. | | Issued | | 1/30/2001 |
| 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 |
| SA01438SE | | Installation of a crew door. | | Reissued | | 2/9/2009 |
| SA01452CH | | Installation of an air ambulance conversion kit. | | Amended | | 3/27/2013 |
| 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 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01692SE (Page 1 OF 2) | | Installation of a Garmin GMX 200 Multi-Function Display | | Reissued | | 10/3/2012 |
| SA01695SE (4 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
| SA01751CH | | Installation of C&D Associates auxiliary rear combustion heater Model CD35K heater kit P/N CD12031K9. | | Issued | | 1/2/2003 |
| 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 |
| SA01861SE (PAGE 3) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01917CH | | Install Air Ambulance Conversion. | | Amended | | 12/22/2009 |
| SA01924CH | | Installation of provisions for a belly mounted camera. | | Amended | | 7/3/2012 |
| SA01933LA-D Page 2 | | 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 |
| SA01988SE (PAGE 6) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA02002AK | | Installation of cowl latch kit No. NC-100. | | Issued | | 7/15/1993 |
| SA02004NY | | Installation of SMR Technologies pneumatic deicer models. | | Issued | | 10/6/2004 |
| SA02013CH | | Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). | | Amended | | 5/2/2011 |
| 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 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 |
| SA02033AT (PAGE 6) | | 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 |
| 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 |
| SA02118AK | | Installation of damage protection plates to the inboard lower side of the flaps. | | Issued | | 6/30/1998 |
| SA02119SE Page 2 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
| SA02142AK-D | | Fabrication and Installation of Aero Twin Inc. Main Landing Gear Inboard Door Hinge Kit No. DH31-100-1. | | Issued | | 6/21/1999 |
| SA02146AK-D | | Fabrication and installation of Aero Twin Inc. main landing gear outboard door hinge kit No. DH31-200-1. | | Issued | | 10/5/1999 |
| SA02149AK | | Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. | | Reissued | | 5/17/2013 |
| SA02153LA-D (Page 2) | | 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 |
| SA02193AK | | Installation of a secondary flap interconnected landing gear warning system (Kit No. WAV-LGWS-001). | | Issued | | 4/25/2002 |
| SA02205AK | | Removal of Piper PA-31 series main landing gear inboard doors | | Reissued | | 2/19/2013 |
| 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 |
| 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 |
| SA02331AK | | Installation of a Secondary Forward Baggage Door Latch | | Reissued | | 10/24/2011 |
| 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 |
| 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 |
| SA02918AT-D | | Installation of fuel cell modifications | | Reissued | | 4/29/2009 |
| SA02973CH | | Installation of C&D Associates Distribution Modification Kit P/N CD29151 in accordance with C&D Associates Installation Instructions IN29151 Rev. - dated February 16 2011 or later FAA approved revision. | | Issued | | 5/31/2011 |
| SA03148NY (PAGE 2 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09066SC | | Install LORI Oil Cooler P/N L8535311. | | Reissued | | 11/14/2012 |
| SA09265AC-D | | Installation of S-TEC Manual Electric Trim System Model ST-705. | | Issued | | 8/15/1997 |
| SA09285AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-727-20/30 according to Bulletin No. 827 Revision 6 dated 1-21-11 and Master Drawing List No. 921029 Revision F dated 1-21-11 or later FAA Approved revisions of the above data (28 Volt System). | | Reissued | | 2/24/2011 |
| SA09286AC-D | | Installation of S-TEC system 30 alt altitude hold system. | | Issued | | 11/26/1997 |
| SA09298AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-751 with Optional Autotrim system. | | Amended | | 3/12/2001 |
| SA09397AC-D | | Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System Model ST-849 with Autotrim. | | Amended | | 7/1/2003 |
| SA1007NW | | Installation of a low thrust detector system. | | Reissued | | 3/6/1998 |
| SA1008EA | | Installation of single lamp logo light in horizontal tail. | | Reissued | | 2/28/1980 |
| SA1010NW | | Installation of a single or dual camera ports optional camera door package and associated components. | | Reissued | | 10/22/2003 |
| 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 |
| SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1032NE | | Installation of (1) propeller spinner assemblies P/N s 43934-01 (LH or RH) and CA 43934-02 (RH) and(2) propeller spinner backplate assemblies P/N s CA 43933-07 (RH) and CA 43933-08 (LH or RH). | | Amended | | 7/14/1994 |
| SA1035GL | | Install Egan Aviation Air Ambulance Stretcher P/N 125 using Installation Kit P/N 800. | | Amended | | 2/10/2004 |
| SA10594SC | | Modification of the Monroe Automotive Equipment Co. (MAECO) Shimmy Dampener. | | Issued | | 12/7/2006 |
| SA1085CE-D | | Installation of Collins Radio Group AP-106 3-axis autopilot system. | | Amended | | 6/25/1975 |
| SA1086CE-D | | Installation of Collins Radio Group AP-107 3-axis autopilot system. | | Amended | | 6/26/1975 |
| SA1087CE-D | | Installation of Collins Radio Group AP-107 2-axis autopilot system. | | Amended | | 6/26/1975 |
| SA1088CE-D | | Installation of Collins Radio Group yaw damper system. | | Amended | | 4/25/1975 |
| SA1104GL | | Installation of South Wind (Div. of Stewart Warner Corp.) Model 8259L heater into the rear baggage compartment. | | Amended | | 9/14/1987 |
| SA1119SO | | Installation of twin cameras and two camera aperatures on starboard side of the lower fuselage. | | Issued | | 1/8/1980 |
| SA1120SO | | Installation of single camera and camera aperature on starboard side of the lower fuselage. | | Issued | | 1/8/1980 |
| SA1121SO | | Installation of supply dropping aperature and sliding shutter and antenna fairing. | | Issued | | 1/8/1980 |
| SA1122SO | | Installation of single camera and camera aperature on the starboard side of the lower fuselage. | | Issued | | 1/8/1980 |
| SA1123SO | | Installation of navigation sight and transparent plastic dome on the lower fuselage station 128. | | Issued | | 1/8/1980 |
| SA1124SO | | Installation of a single camera and camera aperature and antenna fairing on the starboard side of the lower fuselage. | | Issued | | 1/8/1980 |
| SA1125SO | | Installation of twin cameras and two camera aperatures plus camera sights on starboard side of lower fuselage. | | Issued | | 1/8/1980 |
| SA1130SW | | Installation of side facing seats in accordance with (1) Custom Aircraft Conversions Inc. Drawing List 7057 Revision B dated 3/20/70 and E.O. No. 2 dated 11/6/71 or (2) Aviation Fabricators Inc. STC Drawing List AF-206 Rev. (D) dated 5/5/98 or later FAA approved revision. | | Amended | | 12/12/2003 |
| SA1136CE | | Installation of Fiquench cabin fire extinguisher and engine fire extin- guishant distribution system. | | Reissued | | 12/15/1977 |
| SA1151SO | | Installation of Hartzell HC-C4YR-2L/-2/FJC7663D-6Q/FC7663D-6Q Propellers cowling changes and winglets or wing tip extension per Colemill Enterprises Inc. drawing 72000 Revision E August 10 1983 and Installation Instruction for modification of Piper Navajo Model PA-31-350 revised August 10 1983. Colemill Enterprises Inc. Process Spectification for Drawings 64000 and 66000 dated August 31 1977. Colemill Enterprises Inc. Process Specifications #500 for Piper Wing Caps and Winglets dated September 1 1981. Later FAA approved revisions to the above data are acceptable. | | Reissued | | 2/10/2011 |
| SA1164SO | | Installation of a Bendix FCS-870 automatic flight control system. | | Issued | | 7/2/1980 |
| SA1166CE | | Installation of King KFC-200 2 axis (3 optional) flight control system autopilot only or autopilot with flight director. (PA-31 series S/N 31-712 AND UP) | | Reissued | | 2/28/2000 |
| SA1187CE | | Installation of King Model KCS 55A pictorial navigation (compass) system with optional KA 52 autopilot adapter. | | Reissued | | 2/28/2000 |
| SA1255SW | | Mitchell automatic flight system Model AK324 consisting of Piper autoflite II and tracking system. | | Reissued | | 7/9/1984 |
| SA1306SO | | Installation of a 2-place couch in accordance with Drawing Number CA2001 Revision C dated November 19 1981 or later FAA approved Revisions. | | Reissued | | 6/27/2003 |
| SA1318CE | | Chrome-plated brake disc installation. | | Issued | | 5/1/1977 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1421SO | | Installation of 40:1 gear ratio wing flap transmissions and related changes in accordance with Colemill Enterprises Inc. Installation Instructions dated February 16 1983 or later FAA approved revision. This modification provides and equivalent means of compliance with paragraphs (a)1 (a)2 and (a)4 of AD 82-27-13 and restores the 40 | | Reissued | | 2/10/2011 |
| SA1423GL | | Install air ambulance conversion. | | Reissued | | 12/21/2001 |
| SA1522SW | | Mitchell automatic flight system AK394 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/13/1984 |
| SA1595CE | | Installation of stretcher. | | Amended | | 10/9/1990 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA162EA | | Modification of Navion retract link assembly 145-34106. | | Issued | | 1/1/1960 |
| SA1666GL | | Install air ambulance conversion. | | Reissued | | 8/6/2007 |
| SA1744SO | | Installation of two nacelle locker(left side and right side) metal fuel tanks (22.6 gallons each). | | Reissued | | 11/12/1988 |
| SA1774SO | | Installation of a TIO-540-J2B or TIO-540-J2BD Lycoming engine on the left side and LTIO-540-J2B or LTIO-540-J2BD Lycoming engine on the right side. | | Issued | | 4/12/1985 |
| SA1807SW | | AP106 2-axis or 3-axis autopilot including yaw damper and FD-108 flight director. | | Reissued | | 4/24/2000 |
| SA1818CE | | Install fire extinguishing system in cabin and/or fire extinguishant system in engine compartments. | | Reissued | | 2/1/1993 |
| SA184GL | | Installation of microwave landing system airborne equipment. | | Reissued | | 1/12/1979 |
| SA1986CE | | Structural provisions for medical provision console installation. | | Reissued | | 8/21/1990 |
| SA2037CE | | Installation of auxiliary wing fuel transfer tanks of 30.75 gallon capacity. | | Reissued | | 7/5/1990 |
| SA2124WE | | Installation of air conditioning system. | | Reissued | | 5/17/2013 |
| SA2151CE | | Installation of entertainment/ refreshment cabinet. | | Issued | | 11/7/1985 |
| SA2384CE | | This change installs an equipment console two observation windows a modified landing/taxi light system relocation of pitot tubes and provisions for the installation of a (FLIR) Forward Looking Infrared. | | Issued | | 7/11/1988 |
| SA240CH | | Installation of Aero Crafters exhaust heater system kit. | | Reissued | | 12/27/2006 |
| SA2440SW | | Installation of airstair door saver. | | Reissued | | 3/5/2012 |
| SA2504NM | | Installation of power brake valve. | | Issued | | 9/11/1984 |
| SA2586NM (PAGE 4) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA289CH | | Installation of Inline Pneumatic Air Filter P/N CV1J4 | | Reissued | | 1/15/2013 |
| SA295GL | | Install Cleveland conversion kit P/N 199-83. | | Amended | | 4/1/1981 |
| SA2998SO | | Installation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-10 February 15 1991. | | Reissued | | 2/10/2011 |
| 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 |
| SA3017SW-D | | Mitchell automatic flight system AK485 consisting of Piper altimatic IIIC autopilot with optional command/ automatic electronic pitch trim system radio and glide slope couplers. | | Reissued | | 8/1/1984 |
| SA3021SW-D | | Mitchell automatic flight system AK500 and AK500FD consisting of Century IV autopilot and Century IV flight director autopilot with optional remote annuciator panel. | | Amended | | 8/1/1984 |
| SA3129SW-D | | Mitchell automatic flight system AK590 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/5/1984 |
| SA3176NM | | Installation of Machen intercooled engines as modified by STC SE3177NM. | | Amended | | 11/1/1998 |
| SA3197SO | | Installation of replacement of the nose gear scissors link with a link that may be disconnected for ground handling. | | Issued | | 3/24/1992 |
| SA3211SW-D | | Mitchell automatic flight system AK686 or AK686FD Piper altimatic X flight director autopilot with optional remote annunciator. | | Reissued | | 12/7/1983 |
| SA3282NM | | Installation of ARNAV systems FC-10/FT-10 digital fuel flow indicating system. (PA-31-325 SN 31-7405479 and up) (PA-31-350 SN 31-5001-7405478 when modified) | | Issued | | 9/26/1986 |
| SA3355SW | | Mitchell automatic flight system AK846/FD consisting of Century IV/flight autopilot with optional remote annunciator. | | Reissued | | 8/24/1983 |
| SA3388SW-D | | Installation of Mitchell automatic flight system Model YK849 consisting of a yaw damper system. | | Reissued | | 8/15/1983 |
| SA3389SW-D | | Mitchell automatic flight system AK847 consisting of Century 41 autopilot or AK847FD consisting of Century 41 flight director. | | Reissued | | 8/24/1983 |
| SA3401WE | | Installation of single piece windshield. | | Reissued | | 10/31/2001 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3610SW | | Installation of a stretcher in place of two passenger seats. | | Reissued | | 7/15/2010 |
| SA3612NM | | Installation of SAFT type 2376 nickel-cadmium battery. | | Amended | | 1/23/1987 |
| SA3642NM | | Installation of Hartzell HC-E3YR-2ATF/FC8468( )-8Q (left engine) and HC-E3YR-2ALTF/FJC8468( )-8Q (right engine) propeller assemblies. PA-31-350 (T-1020) and PA-31-350 (Chieftain). Serial numbers 31-7405218 238 485 490 31-7552043 076 and 31-7652144 are ineligible for this installation. | | Amended | | 2/9/1990 |
| SA367GL | | Installation of Norton radome kit No. 2032X | | Amended | | 10/24/1980 |
| SA3747SW | | Installation of a camera port and view port. | | Reissued | | 7/12/2005 |
| SA3768WE | | Installation of Fueltron digital fuel flow and totalizer system. | | Reissued | | 4/29/1991 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA4005NM (PG 4) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4037WE | | Installation of Silver Instruments fueltron IIIG or IIIP digital fuel and totalizer system | | Reissued | | 4/29/1991 |
| SA4096WE | | Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. (PA-31-350 SN 31-7405479 and up 31-5001 thru 7405478 when modified per Piper SL 722) | | Reissued | | 1/30/1998 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA418NE | | Installation of Sperry Model MLZ-900 microwave landing system. | | Amended | | 7/27/1989 |
| SA4226WE | | Installation of DTL-1000 -1001 and/or -1002/3 autopilot adapters for the Edo-Aire Mitchell Century III autopilot. | | Issued | | 9/15/1980 |
| SA4385WP | | Installation of inflatable door seal. | | Issued | | 12/4/1981 |
| SA4483NM | | Installation of FC/FT-10 digital fuel flow indicating system. | | Issued | | 6/20/1988 |
| SA454GL | | Installation of Shadin Co. fuel flow indicating system. | | Amended | | 6/8/2006 |
| SA4574SW | | Installation of Texas Instruments Loran C Model TI 9100. | | Issued | | 12/23/1981 |
| SA4678SW | | Installation of Pratt & Whitney AC L PT6A-20 -27 engine and airplane modifications to increase the maximum takeoff gross weight to8 000 pounds. | | Reissued | | 8/9/1988 |
| SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
| SA4745NM | | Installation of Lifeport Patient Loading and Support System. | | Amended | | 11/23/1993 |
| SA4791SW | | Installation of a motorized cover and bottom fuselage hole. | | Amended | | 3/16/1994 |
| SA4792SW | | Install Loran C Model TI-91. | | Issued | | 11/2/1982 |
| SA49CH | | Installation of exhaust heater system kit. | | Issued | | 4/1/1993 |
| SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
| SA5156NM (PG 2) | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 7/29/2010 0:00 |
| SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
| SA563GL | | Installation of Cleveland conversion kit P/N 199-100. | | Issued | | 9/29/1981 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5790NM | | Vortex generators manufactured | | Reissued | | 11/23/2009 |
| SA5796NM | | Vortex generators IAW Document AA1113. | | Reissued | | 11/23/2009 |
| SA5921NM | | Vortex generators manufactured IAW Boundry Layer Research Document AA1126 and installed.. | | Reissued | | 11/23/2009 |
| SA5924NM | | Installation of RPM instrument. | | Amended | | 11/24/1997 |
| SA5925NM | | Installation of oil pressure/temperature instrument. | | Amended | | 12/8/1997 |
| SA5926NM | | Installation of manifold pressure instrument. | | Amended | | 8/15/1993 |
| SA593CH (3 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
| SA5954NM | | Vortex generators manufactured | | Reissued | | 11/23/2009 |
| SA5967NM | | Vortex generators manufactured and installed. | | Reissued | | 11/23/2009 |
| SA5968NM | | Vortex generators manufactured and installed. | | Reissued | | 11/23/2009 |
| SA603EA | | Addition of a 32 inch high door on L.H. side of fuselage between fuselage stations 244 - 261 in accordance with drawings and instructions listed in:
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( 1. Reading Aviation Service Incorporated Drawing List No. 2276 Revision | | Reissued | | 6/27/2003 |
| SA615EA (PAGE 2) | | Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. | | Reissued | | 7/6/2010 |
| SA689NE | | Installation of Safeway Model6901 deicer boot. | | Amended | | 1/31/1991 |
| SA693CE | | Replace existing engine induction air filter with AC Spark Plug filter. | | Reissued | | 6/20/2000 |
| SA721GL | | Install Parker Hannifin Wheels & Brakes Conversion Kit 199-119. (PA-31-350 modified by STC SA4678SW) | | Issued | | 1/10/1984 |
| SA729NW | | Installation of a left wing rear spar to fuselage attach repair procedure | | Issued | | 3/2/1979 |
| SA7584SW | | Modification to the nose wheel steering system. | | Reissued | | 1/22/1990 |
| SA7811SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-467 with optional autotrim system. | | Amended | | 7/24/1996 |
| SA7812SW-D | | Installation of S-TEC Yaw Damper System Model ST-468. | | Amended | | 1/12/1999 |
| SA800EA (PAGE 2) | | Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. | | Amended | | 7/6/2010 |
| SA825NW | | Installationo f a Pilot s Door | | Issued | | 8/23/1979 |
| SA8383SW-D | | Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-525-40/50. | | Amended | | 2/11/1998 |
| SA8705SW | | Installation of R25V0N Alternator Control Unit or R2510N Alternator Control Unit or V2510A Over Voltage Sensor. | | Amended | | 6/21/1996 |
| SA8922SW | | Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) | | Issued | | 7/21/1994 |
| SA935NW | | Relocation of the aircraft battery to a position 4 inches aft of the original location | | Issued | | 5/8/1980 |
| SA967GL | | Installation of Norton Radome Kit No. 2032B. | | Issued | | 10/31/1985 |
| SA970SO | | Installation of Lycoming TIO-540-J2BD or TIO-540-J2B engines and Hartzell propellers HC-C4YR-2/FC7663D-4R or HC-C4YR-2/FC7663D-6Q additional fuel pump and related cowling changes.Modification Drawing Piper Navajo PA-31 Navajo-Panther-Drawing 68000 Revision D Dated 5/17/82.
);INSERT INTO stc_table VALUES ( Installation Instructions for Modification of Piper Navajo Model PA-31 and PA-31-325 Drawing 68000 change D | | Reissued | | 2/10/2011 |
| SA999NE | | Installation of Cleveland wheels and brakes nose-gear shimmy damper P/N 15-16. | | Issued | | 8/21/1992 |
| SP00400SE | | Installation of various propeller electrical de-icer models | | Amended | | 7/25/2006 |
| ST00276WI | | Installation of Kedeg Company 21BC11e Coaleser Assemly. | | Amended | | 7/15/1996 |
| ST00961LA | | Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29 2000 or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1 Slug Thrower Cartridges Master Drawing List | | Reissued | | 7/13/2011 |
| ST01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| ST01468CH | | Installation of various SMR Technologies electrical propeller deicer models. | | Amended | | 7/25/2006 |
| ST01494LA (PG 2) | | Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. | | Reissued | | 8/30/2011 |
| ST02547AT (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
| ST09524SC | | Piper conversion of air conditioning systems from using R12 to R134a refrigerant on aircraft models listed. For PA-31-300 s/n 31-660 31-712 thru 31-900 31-7300901& up. For PA-31-325 sns 31-7400990 & up. PA-31-350 sns 31-5001& 31-5003 31-7305005 up | | Amended | | 3/28/2000 |
