| SA00046SE | | Installation of American Aviation Inc. redesigned engine exhaust stacks. | | Amended | | 11/1/1998 |
| 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 |
| SA00336AT | | Installation of winglets. | | Reissued | | 2/10/2011 |
| 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 |
| SA00459DE | | Installation of Aircraft Noise Control (ANC) System. | | Amended | | 11/19/2001 |
| SA00473DE | | Installation of cabin entertainment system. | | Reissued | | 7/24/2003 |
| SA00499AT | | Installation of nose gear link. | | Issued | | 5/26/1994 |
| 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 |
| SA00555DE | | Replacement of inboard main landing gear door with an aerodynamic fairing. | | Reissued | | 2/21/2008 |
| SA00560CH | | Install air ambulance conversion. | | Reissued | | 11/18/2008 |
| 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 |
| 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 |
| 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 |
| SA00764SE | | Installation of vortex generators on wing and vertical stabilizer and strakes on inboard and outboard sides of nacelles. | | Reissued | | 11/23/2009 |
| SA00765WI | | One only STC for operation with the forward window emergency exit removed (depressurized operation). (PA-31T2 8166042 only) | | Issued | | 4/28/1999 |
| 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 |
| SA00787AT | | Installation of a flight test instrumentation system. | | Issued | | 6/16/1995 |
| SA00797AT | | Installation of left hand and right hand auxiliary tanks fuel cell assemblies. | | Reissued | | 4/27/2008 |
| SA00798AT | | Installation of left hand and right hand auxiliary tanks fuel cell assemblies. | | Reissued | | 4/29/2009 |
| SA00804SE | | Installation of an engine failure indicator system also referred to as a low Thrust Detector system. | | Amended | | 7/16/2000 |
| SA00823CH | | Installation of various de-icer wire harnesses. | | Reissued | | 10/10/2002 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00863SE | | Installation of two Pratt and Whitney PT6A-135 or -135A engines and two Hartzell HC-B3TN-3B/T10178B-8R propellers or as an option two Hartzell HC-E4N-3N/D8990SK propellers | | Reissued | | 6/7/2007 |
| SA00874SE | | Install two Pratt & Whitney PT6A-34 engines in place of
);INSERT INTO stc_table VALUES ( PT6A-28 engines per Master Document List TFL-PA31T-D01 Revision IR dated November 29 2000
);INSERT INTO stc_table VALUES ( or later FAA approved revision. Inspect and maintain this modification in accordance with Instructions
);INSERT INTO stc_table VALUES ( for Continued Airworthiness Document TFL-PA31T-R34 Revision IR dated November 29 2000 or
);INSERT INTO stc_table VALUES ( later FAA approved revision. | | Issued | | 1/31/2001 |
| 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 |
| SA01005AT | | Installation of left and right hand side fuel cell assemblies. | | Reissued | | 5/1/2009 |
| SA01046CH | | Installation of SMR Technologies engine inlet anti-icer models. | | Amended | | 6/5/2006 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01140AT | | Installation of left hand side and right hand side main tank fuel cell assemblies. (PA-31P S/N 3 THRU 115) | | Reissued | | 5/5/2009 |
| SA01141AT | | Installation of left hand side and right hand side main tank fuel cell assemblies. | | Reissued | | 5/5/2009 |
| 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 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01230NY | | Installation of dual Garmin GPS/NAV/COM Systems (GNS 430 and/or GNS 530). | | Issued | | 7/13/2000 |
| SA01240SE (4 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01248SE | | Installation of two Hartzell HC-E4N-3N/D8990SB propellers. | | Reissued | | 6/7/2007 |
| SA01249AT | | Installation of left hand and right hand nacelle fuel cell assemblies. | | Reissued | | 4/29/2009 |
| SA01269CH | | Install provisions for a camera installation in fuselage floor cut-out. | | Issued | | 7/5/2000 |
| 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 |
| 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 |
| SA01384CH | | Installation of various de-icer harnesses. | | Issued | | 1/30/2001 |
| SA01415CH | | Installation of camera provisions in fuselage floor cut-out. Responsible FAA office is Chicago ACO. | | Amended | | 4/26/2004 |
| 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 |
| 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 |
| SA01510AT | | Installation of AirCell Radiotelephone System. | | Issued | | 11/14/1997 |
| 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 |
| SA01917CH | | Install Air Ambulance Conversion. | | Amended | | 12/22/2009 |
| 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 |
| SA01961CH | | Install OFEK Holding Corporation camera provisions installed pursuant to STC SA01415CH or STC SA01962CH. | | Issued | | 4/19/2004 |
| SA01962CH | | Installation of camera provisions in fuselage floor cut-out. Approved for installation serial number 31T-7820042 ONLY. | | Issued | | 4/19/2004 |
| 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 |
| SA02019SE-D Page 2 | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/19/2012 |
| SA02068AT | | One-time installation to remove the pilot s mechanical ADI and HIS and install the Bendix-King two tube EFIS 40 system. | | Issued | | 2/2/2000 |
| SA02075SE | | Installation of a Mid-Continent MD835( ) Lithium Ion Battery | | Amended | | 2/28/2013 |
| 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 |
| SA02119AK | | Installation of damage protection plates to inboard lower side of flaps. | | Issued | | 6/10/1999 |
| 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 |
| SA02203AK (PAGE 2) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| 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 |
| 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 |
| SA02368NY | | Installation of the Pratt & Whitney Canada PT6A-135A engine modified with dual fuel feed lines | | Reissued | | 10/19/2012 |
| 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 |
| SA02641CH | | Installation of C&D Associates Combustion Heater Kit 30 (P/N CD11003K30) | | Issued | | 10/22/2008 |
| SA02738CH (PAGE 2) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02918AT-D | | Installation of fuel cell modifications | | Reissued | | 4/29/2009 |
| 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 |
| SA02959NY | | Installation of 4-blade propeller MTV-16-1-E-C-F/CFL225-37a in accordance with EASA approved MT Propeller Installation Instruction Doc. No. E-1953 Original Issue dated August 20 2010. The following MT Propeller documents are required with this installation: EASA approved Airplane Flight Manual Supplement Doc. No. E-1952-2 Original Issue dated August 20 2010 and Instructions for Continued Airworthiness Doc. No. E-1954 Revised August 20 2010. | | Issued | | 5/3/2011 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03249NY | | Installation of Model MTV-27-1-E-C-F-R(P)/CFR210-58d 5-bladed full feathering reversible wood composite propellers | | Issued | | 2/13/2013 |
| SA09004AC-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-574. | | Issued | | 5/26/1995 |
| SA09005AC-D | | Installation of S-TEC yaw damper system Model ST-579. | | Issued | | 5/26/1995 |
| SA09020AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-597 with optional autotrim system. | | Amended | | 10/10/2001 |
| SA09021AC-D | | Installation of S-TEC yaw damper system Model ST-602. | | Issued | | 9/21/1995 |
| SA09478SC | | Conversion of existing Piper air conditioning system from R12 to R134a refrigerant. | | Issued | | 5/1/1998 |
| SA09536AC-D | | Installation of S-TEC 01304 Digital FLight Control System. | | Reissued | | 1/3/2008 |
| SA09537AC-D | | Installation of single Meggitt Electronic Flight Instrument System (EFIS). | | Issued | | 8/29/2005 |
| SA09538AC-D | | Installation of Meggitt Engine Instrument Display System (EDIS). | | Issued | | 8/29/2005 |
| SA1000SW | | Nine place seating arrangement. | | Issued | | 1/1/1961 |
| 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 |
| 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 |
| SA10365SC | | Installation of a Benz Airborne Systems Model 800-0021 torque pressure system in accordance with Benz Airborne Systems Master Data List DC104-4021-00 Rev. A dated November 4 2004 or later FAA approved revision. | | Issued | | 12/20/2004 |
| SA1039GL | | Install Eagan Aviation air ambulance stretcher P/N 125 using Installation Kit P/N 800. | | Reissued | | 2/4/2004 |
| SA1053SO | | Installation of FCS-870 automatic flight control system including manual electric trim optional yaw damper system and optional flight director. | | Issued | | 3/13/1979 |
| SA1054SO | | Installation of Bendix NP-2041A area navigation computer programmer. | | Issued | | 3/13/1979 |
| SA1054SW | | Stretcher. | | Reissued | | 11/7/1983 |
| SA1055SW | | Baggage retaining net. | | Issued | | 1/1/1961 |
| SA10594SC | | Modification of the Monroe Automotive Equipment Co. (MAECO) Shimmy Dampener. | | Issued | | 12/7/2006 |
| SA1065SW | | Mitchell flight director and autopilot Model 282-187 with slaved directional gyro and optional autoflite model AK187. | | Reissued | | 7/9/1984 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| 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 |
| SA1155SW | | Installation of three place couch according to Drawing V-00101 dated May 21 1970. | | Reissued | | 6/27/2003 |
| SA1161SW | | Installation of nacelle fuel tanks. | | Reissued | | 3/5/2004 |
| 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 |
| SA1178SO | | Installation of a Bendix FCS-8700 automatic flight control system including optional flight director. | | Amended | | 3/11/1981 |
| SA1187CE | | Installation of King Model KCS 55A pictorial navigation (compass) system with optional KA 52 autopilot adapter. | | Reissued | | 2/28/2000 |
| SA1188CE | | Intallation of King KFC 300 automatic flight control system. | | Reissued | | 2/28/2000 |
| SA1204SW | | Mitchell manual electric trim AK281. | | Reissued | | 7/9/1984 |
| SA1234SW | | Mitchell automatic flight system FD/AP282-273 consisting of flight director /autopilot with optional automatic aileron stabilizer AK273. | | Reissued | | 7/9/1984 |
| SA1265SW | | Mitchell automatic flight system model AK323 cons. of Piper Auto- flite II and Omni tracking system. | | Reissued | | 7/9/1984 |
| SA1272SO | | Installation of Utah Research and Development Co. Model 126BC101 battery charging system. | | Reissued | | 10/31/2002 |
| SA1305SW | | Auxiliary fuel tank for model PA-31 serial numbers 31-2 and up.. | | Reissued | | 3/5/2004 |
| 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 |
| SA1340SW | | Four-place couch. | | Reissued | | 4/1/1973 |
| SA1405CE | | Install King KFC-250 autopilot/flight director. | | Reissued | | 2/28/2000 |
| 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 |
| SA142RM | | Install Hoskins Model CFS-2000 fuel flow meter and related systems. (PA-31 SERIES S/N 31-2 AND UP) | | Reissued | | 1/30/1998 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1522SW | | Mitchell automatic flight system AK394 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/13/1984 |
| SA1523SW | | Mitchell automatic flight system AK395 cons. of Century autopilot w/opt. omni tracker. | | Reissued | | 7/13/1984 |
| SA1529CE-D | | Installation of King KAS 297 altitude selector option (PA-31 SERIES S/N 31-712 AND UP PA-325 and PA-31-350)installed under STC SA1166CE. | | Reissued | | 2/28/2000 |
| SA1558CE-D | | Installation of King KFC-300 automatic flight control system. | | Reissued | | 2/28/2000 |
| SA1566CE-D | | Installation of King KFC 250A two axis (third axis optional) flight control system with 3-inch or 4-inch instruments and optional altitude preselect or manual electric trim only. | | Reissued | | 2/28/2000 |
| SA1569WE | | Installation of windshield wiper system. | | Issued | | 1/1/1960 |
| SA1575GL | | Install air ambulance conversion. | | Reissued | | 12/21/2001 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1581NM | | Installation of a bleed air heat system. | | Amended | | 5/17/1984 |
| SA1593GL | | Installation of McCauley propeller model 4HFR34C766/94LNA-2. | | Reissued | | 10/30/2009 |
| SA1594CE | | Installation of stretcher. | | Reissued | | 8/21/1990 |
| SA1595CE | | Installation of stretcher. | | Amended | | 10/9/1990 |
| SA1611SW | | Mitchell automatic flight system AK413 consisting of altimatic IIIB-1 with optional automatic pitch trim radio coupler and glide slope couplers. | | Reissued | | 7/16/1984 |
| SA1612SW | | Mitchell automatic flight system AK416 consisting of autoflite II with optional tracking system. | | Reissued | | 7/16/1984 |
| SA1617CE | | Installation of cargo pod. | | Issued | | 12/2/1980 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1651WE | | Installation of ski carrying pod under fuselage at wing root. | | Issued | | 1/1/1960 |
| SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
| SA1728SO | | Replace existing nickel-cadmium batteries with Teledyne Battery Products G-6381E and G-6381ES. | | Amended | | 5/4/2001 |
| SA1751CE | | Installation of external baggage pad. | | Issued | | 6/30/1982 |
| SA1773CE-D | | Installation of King KFC 250 3-axis Flight Control System with 3-inch or 4-inch indicators and optional Altitude Preselect. | | Reissued | | 2/28/2000 |
| SA1787NM | | Installation of two Hartzell HC-B3TN-3B/T10178B-10Q propellers on PA-31T PA-31T airplanes equipped with PWC PT6A-28 and PT6A-11 engines. | | Amended | | 2/6/1986 |
| SA1816CE | | Dual stretcher installation. | | Reissued | | 8/21/1990 |
| SA190GL | | Install a J.E.T. DAC-2000 3-D RNAV system. | | Issued | | 8/16/1977 |
| SA191GL | | Installation of microwave landing airborne equipment. | | Reissued | | 1/12/1979 |
| SA1985CE | | Structural provisions for medical provision console installation. | | Reissued | | 8/21/1990 |
| SA1986CE | | Structural provisions for medical provision console installation. | | Reissued | | 8/21/1990 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA213GL | | Installation of storm window in right hand cockpit window dupli- cating storm window now installed in left hand cockpit window. | | Issued | | 2/2/1978 |
| SA2151CE | | Installation of entertainment/ refreshment cabinet. | | Issued | | 11/7/1985 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2309NY | | Install Pratt & Whitney Canada (P&WC) PT6A-135A engines (modified with a dual line start fuel system ) in place of PT6A-135 engine. | | Issued | | 11/1/2006 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2350NM Page 2 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA240CH | | Installation of Aero Crafters exhaust heater system kit. | | Reissued | | 12/27/2006 |
| SA250CE | | Installation of Woodward electronic propeller synchraphaser system. | | Reissued | | 4/30/2007 |
| 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 |
| SA2687NM (PAGE 1) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 |
| SA2693NM (PAGE 2) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 0:00 |
| SA2713NM | | Installation of medical stretcher transport unit including patient restraint oxygen suction electrical service and lighting. | | Issued | | 7/30/1985 |
| SA2756NM | | Installation of medical transport unit. | | Issued | | 8/10/1986 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA284GL | | Install Cleveland conversion kit P/N 199-83. | | Amended | | 4/1/1981 |
| SA289CH | | Installation of Inline Pneumatic Air Filter P/N CV1J4 | | Reissued | | 1/15/2013 |
| SA2948SW | | Addition of Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
| SA2990SW | | Installation of camera pod under left wing | | Reissued | | 7/15/2010 |
| SA2991SW | | Installation of nose radar | | Reissued | | 7/15/2010 |
| SA2992SW | | Installation of 50 gallon fuel tank in nose baggage compartment | | Reissued | | 7/15/2010 |
| SA3008SW-D | | Mitchell automatic flight system AK483 consisting of Piper altimatic IIIC autopilot with optional command/automatic electronic pitch trim radio and glide slope couplers. | | Reissued | | 8/1/1984 |
| SA3009SW-D | | Mitchell automatic flight system AK496 consisting of Century IV autopilot or AK496FD Century IV flight director autopilot with electric elevator pitch trim and optional remote annuciator panel. | | Reissued | | 8/1/1984 |
| SA3010SW-D | | Mitchell automatic flight system YK491 consisting of yaw damper. | | Reissued | | 8/1/1984 |
| SA3012SW-D | | Mitchell automatic flight system AK484 consisting of Piper Altimatic IIIC autopilot with optional command/automatic electronic pitch trim radio coupler and glide slope coupler. | | Reissued | | 8/1/1984 |
| SA3013SW-D | | Mitchell automatic flight system AK492 consisting of a Century IV autopilot or AK492FD consisting of a Century IV flight director optional autopilot with remote annunciator panel. | | Reissued | | 8/6/1984 |
| SA3014SW-D | | Mitchell automatic flight system YK493 consisting of yaw damper. | | Reissued | | 8/1/1984 |
| SA3015SW-D | | Mitchell automatic flight system AK-498 cons. of Piper altimatic IIIC autopilot w/opt command/ automatic electronic pitch trim radio and glide slope coupler. | | Reissued | | 8/1/1984 |
| SA3016SW-D | | Mitchell automatic flight system AK499 cons. of Century IV autopilot or AK499FD consisting of a Century IV flight director autopilot with opt. remote annunciator. | | Reissued | | 8/1/1984 |
| SA3086SW-D | | Mitchell automatic flight system AK560 cons. of Century III autopilot w/opt. radio & glide slope couplers. | | Reissued | | 6/20/1984 |
| SA3130SW-D | | Mitchell automatic flight system AK589 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/5/1984 |
| SA3210SW-D | | Installation of Mitchell automatic flight system Model AK685 consisting of a Piper altimatic X autopilot or Model AK685 FD consisting of a Piper altimatic X flight director autopilot with optional remote annunciator. | | Reissued | | 12/7/1983 |
| SA3212SW-D | | Mitchell automatic flight system Piper altimatic X autopilot AK687 or AK687FD Piper altimatic X flight director autopilot w/opt. Remote annunciator. | | Reissued | | 12/7/1983 |
| SA3213SW-D | | Mitchell automatic flight system Piper altimatic X autopilot AK688 or AK688FD Piper altimatic X flight director autopilot w/opt. remote annunciator. | | Reissued | | 12/7/1983 |
| SA3220NM | | Installation of Hoskins Model CFS-2212 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA323NE | | Remove existing starter generator and install Aircraft Parts Corp. starter-generator APC Model250SG116Q. | | Reissued | | 7/30/2009 |
| SA3305NM | | Installation of monorail sun visor system. | | Reissued | | 3/24/2003 |
| SA3610SW | | Installation of a stretcher in place of two passenger seats. | | Reissued | | 7/15/2010 |
| SA37NE | | Installation of Global navigation GNS-500A series 2 VLF/Omega navigation system and associated components. | | Issued | | 11/17/1980 |
| SA3801NM | | Installation of American Aviation intercooled engines as modified by STC SE3800NM. | | Amended | | 11/1/1998 |
| SA4005NM (PG 4) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4016WE | | Installation of Hoskins model CFS-2002 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA4066SW | | Auto-feather system 1. | | Issued | | 12/4/1979 |
| SA4076NM | | Installation of medical equipment system unit Serial No. 1. | | Amended | | 6/14/1993 |
| SA4143WE | | Installation of Sperry SPZ-200A automatic flight control system. | | Reissued | | 1/15/2009 |
| SA415GL | | Installation of a Collins LRN 70 Omega navigation system. | | Issued | | 6/20/1980 |
| SA4268SW | | Installation of Pratt & Whitney PT6A-135 engines according to Drawing List 50 000L dated 12/11/79 revised 1/23/81 or later FAA approved revision. | | Reissued | | 5/23/2001 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4335SW | | Installation of Pratt and Whitney engines and Hartzell propellers | | Reissued | | 6/6/2011 |
| SA437SO | | Installation of Bendix FCS-810 automatic flight control system including manual electric trim and optional flight director indicator. | | Amended | | 4/4/1979 |
| SA4574SW | | Installation of Texas Instruments Loran C Model TI 9100. | | Issued | | 12/23/1981 |
| SA4723NM | | OPTION 1: Installation of modified ram air engine induction system. OPTION 2: This installation may be installed with the Ice Door Modification only. | | Amended | | 11/1/1998 |
| SA4743NM | | Installation of two Hartzell HC-B3TN-3B/T10178B-10Q propellers on airplanes equipped with P&W PT6A-135 engines. | | Issued | | 7/21/1989 |
| SA4745NM | | Installation of Lifeport Patient Loading and Support System. | | Amended | | 11/23/1993 |
| SA4792SW | | Install Loran C Model TI-91. | | Issued | | 11/2/1982 |
| SA483SO | | Installation of Bendix YD4 yaw damper system. | | Issued | | 12/23/1971 |
| SA4977SW | | J.B. Systems electric motor driven air conditioning compressor. | | Issued | | 3/27/1983 |
| 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 |
| SA529EA | | Installation of kit for radar antenna | | Issued | | 1/1/1960 |
| SA541CE | | Installation of Hoskins Twilighter Mark III Supplemental Light System in accordance with specification sheets Dated November 02 1967. | | Reissued | | 9/30/2011 |
| SA5467SW | | Installation of dual camera port. | | Reissued | | 12/20/2010 |
| SA546EA | | Incorporation of opening in lower surface of fuselage aft of front spar. | | Issued | | 1/1/1960 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA572EA | | Installation of Goodrich Model 5735K deicer kit (P/N 5735 deicer boot P/N D-5735-1 cable P/N 5735H hardware kit). Limited to aircraft which incorporate Goodrich Propeller Deicing Systems equipped with Goodrich Propeller Deicer Boot P/N 4E1185-5 on Hartzell propellers as listed on STC SA572EA eligibility list. | | Reissued | | 5/9/2003 |
| SA578NW | | Install redesigned 7th seat(toilet). | | Issued | | 5/12/1978 |
| SA578SO | | Instl. of a Bendix M-4D automatic flight control system including optional manual electric pitch trim and flight director system. | | Amended | | 10/1/1979 |
| SA5876SW | | Installation of wing/nacelle fairings. | | Reissued | | 7/15/2010 |
| 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 |
| SA5984SW | | Relocation of rear pressure bulkhead. | | Issued | | 7/18/1985 |
| SA599GL | | Installation of Cleveland Wheel & Brake conversion kit No. 199-111. | | Amended | | 5/4/1982 |
| SA613EA | | Installation of nine seats. | | Amended | | 6/6/1969 |
| 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 |
| SA617GL | | Installation of a Shadin Co. 911218 temperature compensated fuel flow indicating system. | | Reissued | | 6/8/2006 |
| SA622EA | | Incorporation of camera hatch and mountings to accommodate Zeiss RMK A15/23 camera. | | Issued | | 1/1/1960 |
| SA629CH | | Limited to installation on PA-31T serial numbers 31T-7620018 31T-7820039 and 31T-7520001 ONLY. Installation of Weather Modification equipment in accordance with Weather Modification conversion instructions Document Control WMI-318MA-972 dtd 3/1/97 (serial number 31T-7620018) or Weather Modification conversion instructions document control WMI-131MP-972 dtd 3/1/97 (serial number 31T-7820039). With flare racks installed aircraft is to be operated in Restricted Category. | | Amended | | 3/10/2003 |
| SA660WE | | Installation of HRD-type fire extinguishing system. (AND STC SA111WE) | | Reissued | | 2/4/1987 |
| SA665NW | | Installation of forward facing white lights (100 watts) clear plastic wing tip tank nose cone and associated systems | | Reissued | | 2/24/1981 |
| SA688NE | | Installation of Safeway Model 6900 deicer boot. | | Amended | | 1/31/1991 |
| SA689NE | | Installation of Safeway Model6901 deicer boot. | | Amended | | 1/31/1991 |
| SA700GL | | Installation of Airborne fuel pump1C54-1 as a replacement for Piper fuel pump P/N 50595-2 50595-4 and 55428-2. | | Amended | | 1/11/1984 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA741EA | | Installation of co-pilot door. | | Amended | | 11/3/1969 |
| SA744EA | | Modification of toilet seat hassock and installation of safety belt. | | Issued | | 4/4/1969 |
| SA764GL | | Installation of a fuel flow meter and totalizer. | | Reissued | | 6/8/2006 |
| SA782CE | | Installation of King Radio H-14 autopilot. | | Issued | | 6/1/1971 |
| 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 |
| SA812NE | | Installation of BF Goodrich Model 6975-1 De-Icer kit or BF Goodrich Model 6975-10 De-Icer kit. | | Reissued and Amended | | 5/26/2000 |
| SA8528SW-D | | Conversion of existing Piper air conditioning system from R12 to R134a refrigerant. | | Issued | | 5/1/1998 |
| SA852EA | | Installation of Grimes 555 Series three light strobe kit P/N 34-0100-1. | | Amended | | 6/4/2007 |
| SA8538SW-D | | Installation of a Century Automatic Flight System Kit No. AK1059. | | Issued | | 8/21/2000 |
| SA8539SW-D | | Installation of a Century yaw damper system kit no. YK1060 consisting of a Century yaw damper. | | Issued | | 8/21/2000 |
| SA862SW | | Installation of Piper automatic flight system model AK187 consisting of altimatic III B-1 autopilot with optional automatic pitch trim automatic aileron stabilizer radio coupler glide slope coupler and optional radio coupler model 1C388-3. | | Reissued | | 6/29/1984 |
| SA865EA | | Installation of radome kit 2031KX. | | Amended | | 5/28/1976 |
| 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 |
| SA8NE | | Installation of Collins AP-1072-axis or 3-axis autopilot including yaw damper system. | | Reissued | | 12/19/1974 |
| SA908SW | | Air conditioner. | | Issued | | 1/1/1960 |
| SA923SO | | Installation of Bendix FCS-870 automatic flight control system. | | Issued | | 2/17/1977 |
| SA924SO | | Installation of Bendix NP-2041A area navigation computer. | | Issued | | 2/17/1977 |
| SA986SW | | Baggage lockers in revised aft nacelle fairings. | | Issued | | 1/1/1960 |
| SP00400SE | | Installation of various propeller electrical de-icer models | | Amended | | 7/25/2006 |
| ST00039WI | | Installation of a Bendix/King electronic flight instrument system EFIS-40. | | Issued | | 2/17/1993 |
| 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 |
| ST01930LA | | Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI) | | Reissued | | 8/4/2009 |
| ST02547AT (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
