| SA00022WI | | Installation of seals on lower surface between the wing ailerons and flaps. S/N 24-2844 AND UP | | Amended | | 5/24/1993 |
| 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 |
| SA00027SE | | Installation of CAPCO Auxiliary Nacelle Fuel Tanks | | Reissued | | 9/9/2003 |
| 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 |
| SA00160SE | | Installation of modified instrument panel. | | Issued | | 12/12/1994 |
| 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 |
| SA00187DE | | Installation of Oilamatic Preoiler system. | | Issued | | 10/5/1995 |
| SA00193AT | | Installation of carbon steel discs. | | Reissued | | 11/14/1994 |
| SA00229NY | | Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. (PA-23-250 6 place) | | Amended | | 1/24/1997 |
| SA00233SE | | Installation of the Precise Flight Series 100 Speedbrake System | | Amended | | 3/10/2005 |
| 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 |
| SA00356WI | | Installation of a 10.2 gallon auxiliary fuel tank in each wing nacelle and associated changes. | | Reissued | | 9/8/1995 |
| 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 |
| SA00449AT | | Installation of flap gap seals. | | Issued | | 3/31/1994 |
| SA00484WI | | Installation of shoulder harness for two front seats. | | Reissued | | 3/25/2009 |
| SA00563AT | | Installation of Appalachian Accessories carbon steel brake discs P/N AA-22. | | Reissued | | 1/24/1995 |
| SA00670AT | | Installation of an OCEM AP-2C or AP-3C autopilot system in accordance with Automatic Flight Systems OCEM AP-2C AP-3C Installation Manual for Aircraft Piper Models PA-30 and PA-39 | | Reissued | | 4/6/2004 |
| SA00676CH | | Replace existing spinner with either Hartzell spinner P/N D-5749L or D-5749LP. | | Issued | | 5/20/1997 |
| 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 |
| SA00726CH | | Replace lower cabin door sill. | | Issued | | 8/5/1997 |
| 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 |
| SA00735AT | | Installation of composite aft spinner bulkhead and/or composite spinner. | | Amended | | 10/13/2000 |
| SA00746WI | | Installation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901) | | Reissued | | 3/25/2009 |
| SA00763SE | | Installation of vortex generators on the wing leading edge and vertical fin surfaces. | | Issued | | 12/21/1999 |
| 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 |
| SA00786SE | | Installation of Aviation Innovations fuel pump motor modification in accordance with Aviation Innovations Drawing List DLPA30 Revision G dated August 1 2002 or later FAA approved revision. | | Amended | | 10/10/2002 |
| 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 |
| SA00906AT | | Installation of replacement fuel cell assemblies for left-hand and right-hand auxiliary tank. | | Reissued | | 4/27/2009 |
| 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 |
| 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 |
| 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 |
| SA01205WI-D (2 OF 2) | | Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.
);INSERT INTO stc_table VALUES ( | | Amended | | 11/20/2007 |
| SA01224AT | | Installation of wheel hub cabs with valve stem access door. | | Amended | | 4/17/1998 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (4 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01252SE | | Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30 dated September 24 1999 (PA-30 PA-39) or DLPA30T dated August 28 1999 (Turbocharged PA-30 PA-39) or later FAA approved revisions to either document. | | Reissued | | 1/20/2004 |
| 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 |
| 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 |
| 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 |
| SA01516AT | | Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. | | Amended | | 10/24/2008 |
| 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 |
| SA01571CH | | Installation of modified nose cone. | | Issued | | 11/16/2001 |
| 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 |
| 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 |
| SA01834CH (1 OF 2) | | Installation of the High Intensity Discharge Light Assembly Kit. | | Amended | | 3/20/2009 |
| 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 |
| 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 |
| 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 |
| SA02146AT | | Replace alternators solid state voltage regulations and wiring harness with Electrosystems equipment. | | Reissued | | 3/9/2009 |
| 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 |
| 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 |
| SA02268CH (PAGE 5) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02276AK | | Installation of AMSAFE Aviation Inflatable Restraints | | Amended | | 3/12/2013 |
| SA02293AK (2 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02297AK | | Installation of a fixed mounted Max-Vis Enhanced Vision System (EVS) Model 1000 to include a nose mounted conformal fairing and associated sub structural mount a forward nose compartment mounted power supply an aft avionics rack installed 12 to 24 VDC power converter and a dash mounted dedicated display monitor. | | Issued | | 9/9/2007 |
| SA02492CH | | Installation of a Three Point Torso Restraint System. | | Issued | | 10/29/2007 |
| 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 |
| 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 |
| 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 |
| SA03708AT | | Replacement of the Main Landing Gear Housing | | Issued | | 6/2/2009 |
| SA04019AT | | Installation of The Aeronautical Design Service (ADS) part number 1008020828 Stabilator Horn | | Reissued | | 9/12/2013 |
| SA09359AC-D | | Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems Model ST-816-20/30. | | Amended | | 7/15/2008 |
| SA09363AC-D | | Installation of S-TEC system 30 alt altitude hold system. | | Issued | | 5/8/1998 |
| SA1007NW | | Installation of a low thrust detector system. | | Reissued | | 3/6/1998 |
| 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 |
| SA1022NE | | Installation of single pane increased thickness side windows. | | Amended | | 4/2/1997 |
| SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1027SW | | Mitchell manual electric pitch trim AK267. | | Reissued | | 7/9/1984 |
| SA10594SC | | Modification of the Monroe Automotive Equipment Co. (MAECO) Shimmy Dampener. | | Issued | | 12/7/2006 |
| SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1111SW | | Outer wing integral auxiliary fuel tanks and increase gross weight of180 pounds. | | Amended | | 3/14/1983 |
| SA1112SW | | Dorsal fin. | | Amended | | 3/14/1983 |
| SA1113SW | | Extended nose with baggage compartment. | | Amended | | 3/14/1983 |
| SA1114SW | | Nacelle baggage compartments. | | Amended | | 3/14/1983 |
| SA1115SW | | Dual brakes. | | Reissued | | 11/22/1998 |
| SA1151SW | | Lycoming IO-360-C1C engines(200 hp) with Hartzell HC-C2YK-2/ C7666A-4 propeller. | | Amended | | 3/14/1983 |
| SA1152SW | | One-piece windshield. | | Reissued | | 3/14/1983 |
| SA1153SW | | Square wing tips with dual navigation lights. | | Amended | | 9/7/1999 |
| SA1154SW | | Rudder and aileron interconnect system. | | Reissued | | 3/14/1983 |
| SA1202WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1239SW | | Turbosupercharged Lycoming IO-360-C1C engines. | | Reissued | | 3/14/1983 |
| SA1254SW | | Installation of electrothermal propeller de-icing system. Aircraft must be placarded: WARNING. THIS AIRPLANE NOT APPROVED FOR FLIGHT INTO KNOWN ICING CONDITIONS. | | Reissued | | 11/22/1998 |
| 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 |
| SA1320CE | | Chrome-plated brake disc installation. | | Amended | | 6/20/1977 |
| SA1337SW | | Pneumatic de-icing system. | | Reissued | | 11/22/1998 |
| SA1341SW | | Nose taxi light. | | Reissued | | 3/14/1983 |
| SA1342SW | | Mitchell automatic flight system AK296 cons. of Piper altimatic IIIB-1 autopilot w/opt. Automatic pitch trim radio and glide slope couplers. | | Reissued | | 7/9/1984 |
| SA1343SW | | Mitchell automatic flight system AK325 cons. of Piper autoflite II w/opt. tracking system. | | Reissued | | 7/9/1984 |
| SA1344SW | | Mitchell command electric trim AK267. | | Issued | | 7/20/1971 |
| SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
| SA1386SW | | Mitchell automatic flight system model AK339 cons. of Piper auto-control III autopilot with optional radio coupler. | | Reissued | | 7/10/1984 |
| SA1401CE | | Install King Model KNS 80 digital area navigation system. | | Reissued | | 2/28/2000 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1431NM | | Installation of a Shadin 910502 or 910514 Digiflo digital fuel flow indicator system and optional removal of the fuel pressure indicating system on Piper PA-30 and PA-39 airplanes equipped with Lycoming Model IO-320-B1A and LIO-320-B1A or IO-320-C1A and LIO-320-ClA engines. | | Reissued | | 3/1/1988 |
| SA1446NM-S | | Installation of 15x6.00-6 tire on original equipment nose wheel | | Issued | | 1/20/1982 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| 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 |
| SA1512WE (2 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 0:00 |
| SA1530GL | | Install PA-30 or PA-39 lower cowl oil drain access panel with relief for quick drain. | | Amended | | 3/1/1991 |
| SA1533GL | | Installation of on-board engine analyzer system. | | Issued | | 11/30/1990 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1588WE | | Installation of supplemental exterior flashing lights. | | Issued | | 1/30/1968 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1638SW | | Mitchell automatic flight system AK355 consisting of Century I with omni tracker. | | Reissued | | 7/16/1984 |
| SA1662GL | | Installation of rudder fin cap fairing with or without a strobe. | | Reissued | | 5/7/1997 |
| SA1675NM | | Installation of a third seat belt in the center of the rear bench seat | | Issued | | 7/15/1982 |
| SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
| SA1689SO | | Installation of shoulder harness. | | Issued | | 10/19/1984 |
| SA1696NM | | Installation of Shadin 910502 Digiflo fuel flow indicator system and removal of fuel pressure indicating system. | | Reissued | | 3/17/1988 |
| SA1712GL | | Installation of Gear Lobe fairings. | | Reissued | | 5/7/1997 |
| SA1753NM | | Removal of the factory equipped vertical fin mounted rotating beach and installation of a vertical fin mounted Whelen strobe light assembly | | Issued | | 10/13/1982 |
| SA1754NM | | Installation of a Shadin 910502 or 910514 Digiflo digital fuel flow indicator system and removal of the pressure indicating system on PA-30 and PA-39 airplanes equipped with Lycoming IO-320-B1A and LIO-320-B1A engines. | | Amended | | 2/7/1983 |
| SA1756NM | | Installation of positive flap retraction system. | | Reissued | | 9/8/2005 |
| SA1806SO | | Installation of nose landing gear tire. | | Issued | | 7/10/1985 |
| SA184EA | | Installation of 13-quart alcohol propeller anti-icing kit utilizing either a Weldon pump (P/N 100B-6) or a Bendix pump (P/N 478360). | | Amended | | 10/15/1971 |
| SA1870NM | | Installation of Aileron Gap Fairings | | Issued | | 4/18/1983 |
| SA188SO | | Flight control wheel. | | Issued | | 1/1/1960 |
| SA18CH | | Installation of windshield cowler fairing. | | Reissued | | 5/7/1997 |
| SA1935WE | | Installation of Brittain Industries Inc. Model B5 B2C or NAV-2B Flight Control System | | Reissued | | 2/6/2013 |
| SA209GL | | Installation of one piece windshield. | | Reissued | | 1/31/2007 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA214CH | | Installation of Hartzell HC-E2YL-2BSF/F7663D-4 or HC-E2YL-2BLSF/ FJ7663D-4 model propellers. | | Reissued | | 5/7/1997 |
| SA215CH | | Installation of an induction system. | | Reissued | | 5/7/1997 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA225EA | | Installation of Monitair angle of attack and stall warning system. | | Reissued | | 2/14/1972 |
| SA2273NM | | Installation of fiberglass window mouldings. (PA-30 SN 30-1 thru 30-901) | | Issued | | 4/16/1984 |
| SA2312WE | | Installation of leading edge cuffs stall fences stall strips drooped ailerons flap actuated stabilator trim system raked wing tips(optional) and dorsal fin. | | Reissued | | 9/8/2005 |
| SA2337SO | | Replacement of Cleveland brake discs P/N 164-22A and/or 164-23 or 164-123 with Appalachian Accessories stainless steel brake discs P/N 75-23. | | Issued | | 5/17/1988 |
| SA233EA | | Reservoir-type pneumatic wing and tail deicing system. | | Amended | | 10/7/1970 |
| SA2350NM Page 2 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2484CE | | Installation of side windows with an increase of thickness from 1/8 inch to 1/4 inch. | | Issued | | 4/14/1989 |
| SA2550CE | | Installation of a Webco door latch kit per Webco Aircraft Drawing List2430-101. | | Issued | | 10/27/1989 |
| 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 |
| SA2647CE | | Installation of flap actuated gear warning system. | | Reissued | | 5/7/1997 |
| SA2652CE | | Installation of main fuel cell bladders as replacements for original bladders. | | Reissued | | 7/31/2002 |
| 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 |
| SA271GL | | Installation of Great Lakes forward windows P/N s W- W/T- W/G-2058-187 or -250 and W- W/G-20599-187 or -250. | | Reissued | | 11/26/2008 |
| SA282CE | | GUART System (Gear-up automatic response device). | | 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 |
| SA2849WE | | Installation of oxygen system. | | Reissued | | 1/26/1984 |
| SA2949SW | | Addition of Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
| SA3028SW-D | | Mitchell auto. Flight system AK481 consisting of Piper altimatic IIIC autopilot with command automatic electronic pitch trim system optional radio and glide slope couplers. | | Reissued | | 8/16/1984 |
| SA3036SW-D | | Mitchell automatic flight system AK506 consisting of Piper Autocontrol IIIB autopilot with optional radio coupler. | | Reissued | | 6/21/1984 |
| SA3045SW-D | | Mitchell automatic flight system consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/22/1984 |
| SA308CH | | Replace baggage door holdup bracket with air strut bracket. | | Reissued | | 5/7/1997 |
| SA3105SO | | Installation of speed spats main landing gear fairings. | | Issued | | 12/18/1991 |
| SA3128SW-D | | Mitchell automatic flight system AK598 consisting of Century III autopilot with optional command automatic trim radio and glide slope couplers. | | Reissued | | 6/5/1984 |
| SA313SW | | Pitch trim system AK124. | | Issued | | 1/1/1960 |
| SA3205NM | | Installation of fiberglass wing tips. | | Issued | | 12/6/1985 |
| SA3282SO | | Installation of flap bracket fairings. | | Issued | | 7/13/1992 |
| SA3302SO | | Installation of fiberglass nose bowl. | | Amended | | 3/4/1993 |
| SA331SO | | External power supply plug. | | Issued | | 1/1/1960 |
| SA3336WE | | Installation of single piece windshield. | | Reissued | | 4/8/1999 |
| SA334SW | | Installation of InterAv Alternator. | | Reissued | | 7/20/1981 |
| SA3395SW-D | | Installation of Mitchell automatic system AK893 consisting of Century IIB autopilot. | | Reissued | | 8/24/1983 |
| SA343SW | | Automatic pilot AK127 AK127E or AK127E-3 and lateral guidance radio coupler AK123. | | Issued | | 1/1/1960 |
| SA3468SW-D | | Installation of Century automatic flight system Modedl AK974 consisting of a Century 2010/2030/2031/2050/2051 autopilot. | | Amended | | 10/21/1992 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3563NM | | Installation of ARNAV Systems FC-10/FT-10 digital fuel flow indicating systems. | | Issued | | 9/14/1987 |
| SA3707WE | | Installation of single piece windshield. | | Reissued | | 6/25/2001 |
| SA370CH | | Installation of wing fillet. | | Reissued | | 5/7/1997 |
| SA3729WE | | Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA394CH | | Installation of cowl nose bowl. | | Reissued | | 5/7/1997 |
| SA4005NM (PG 4) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4008NM | | Installation of removable panels on the battery box slides. | | Reissued | | 9/30/2005 |
| SA4066WE | | Installation of Silver Instruments Fueltron IIIG or IIIP digital fuel flow and totalizer system. | | Reissued | | 4/29/1991 |
| SA4189WE | | Installation of DTL-1000 -1001 and/or -1002/3 autopilot adapters for the Edo-Aire Mitchell Centrury III autopilot. | | Issued | | 7/29/1980 |
| SA4238WE | | Installation of inflatable door seal. | | Issued | | 9/25/1980 |
| SA426CH | | Installation of electronic tachometer fuel flow manifold pressure and fuel totalizer instruments. (PA-30 SN 30-147) | | Issued | | 10/18/1995 |
| SA428NE | | Installation of William C. Roberts brake discs P/N 202-22SS in lieu of Piper brake discs P/N 754-554. | | Amended | | 12/15/2003 |
| SA4295SW | | Propeller synchrophaser system. | | Issued | | 3/6/1981 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA466SW | | Pitch trim system AK147. | | Issued | | 1/1/1960 |
| SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
| SA475SW | | Pitch trim system AK152. | | Issued | | 1/1/1960 |
| SA477EA | | SAGA (semi-automatic gear actuating) system. | | Issued | | 1/1/1960 |
| SA4852NM | | Installation of electrical heater including engine driven alternators and controls. | | Issued | | 4/4/1990 |
| SA5112SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-127 with optional autotrim system. | | Amended | | 1/23/1997 |
| SA5138SW-D | | Install S-TEC System 60 pitch stabilization system Model ST-128 with optional autotrim system. | | Amended | | 3/19/1997 |
| 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 |
| SA516GL | | Installation of aileron flap flap to fuselage rudder gap seals wing root fairings dorsal fin and engine nacelle fairing. | | Reissued | | 1/21/1999 |
| SA520SO | | Installation of Bendix FCS-810(Piper Altimatic V/F/D) automatic flight control including manual electric trim and optional flight director indicator. | | Amended | | 8/13/1976 |
| SA5227SW-D | | Install S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-205-40/50. | | Amended | | 3/28/1997 |
| SA524SW | | Pitch trim system AK164. | | Issued | | 1/1/1960 |
| SA525SW | | Piper autocontrol III Mitchell AK161 autopilot. | | Issued | | 1/1/1960 |
| SA531SW | | Fifth seat. | | Issued | | 1/1/1960 |
| SA533NW | | Installation of aileron trim. | | Issued | | 10/19/1977 |
| SA534EA | | Replacement of existing stall warning detector Safe Flight P/N C-52207 with pre-stall warning and speed control transducer Safe Flight P/N 792 and speed control indicator P/N 571. | | Issued | | 1/2/1990 |
| SA551CH | | Modify the fuselage nose cover. | | Issued | | 9/12/1996 |
| SA557GL | | Installation of Hartzell Propeller Models HC-E2YL-2BSF/F7663-6Q and HC-E2YL-2BLSF/FJ7663-6Q and Hartzell D-5749(P) or D-5749(P) spinners. | | Amended | | 6/22/1999 |
| SA559WE | | B-4 flight control system including autopilot PC-1 pitch assist AH-1 altitude hold and NAV-1 navigation coupler. | | Reissued | | 10/1/1973 |
| SA563CH | | Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. | | Reissued | | 2/10/2009 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA576SW | | Installation of Mitchell automatic flight system model AK186 consisting of Piper altimatic IIIB autopilot radio coupler and automatic aileron stabilizer model AK179. | | Reissued | | 6/25/1984 |
| SA581SW | | Installation of Mitchell automatic aileron stabilizer model AK179. | | Reissued | | 6/25/1984 |
| SA5841NM | | Installation of an engine electronic digital tachometer. | | Reissued | | 1/14/2002 |
| SA589WE | | Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. | | Reissued | | 10/5/1976 |
| SA591CE | | Install Alco XW20101-PA-30-L windshield wiper system. | | Issued | | 1/1/1960 |
| 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 |
| SA5983NM | | Cockpit sun visor installation. | | Reissued | | 3/24/2003 |
| SA6058SW-D | | Installation of S-TEC manual electric trim system Model ST-355. | | Issued | | 3/19/1986 |
| 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 |
| SA630WE | | Installation of oil filter assemblies. (NAVION A AND B with optional engine) | | Reissued | | 8/29/1974 |
| SA634NE | | Installation of Cleveland Wheel & Brakes (Parker Hannifin). | | Issued | | 2/21/1989 |
| SA662SW | | Installation of Mitchell automatic flight system model AK220 consisting of Century III autopilot with option automatic pitch trim automatic aileron stabilizer and radio coupler. | | Issued | | 6/25/1984 |
| SA662WE | | Hi-Lo sensitivity adaptor BI-400 and autopilot with NAV-1 navigation coupler and heading lock. | | Reissued | | 10/1/1973 |
| SA673EA | | Installation of radome kit 3058X. | | Amended | | 5/26/1976 |
| SA676EA | | Installation of Norton Company radome kit 3058-B. | | Amended | | 3/24/1971 |
| SA693CE | | Replace existing engine induction air filter with AC Spark Plug filter. | | Reissued | | 6/20/2000 |
| SA7063NM | | Installation of acrylic window liners in accordance with FAA approved Drawing Lists. Drawing lists are listed on FAA approved Model List Number SA7063NM or later FAA approved revision. | | Reissued | | 10/17/2008 |
| SA7151SW-D | | Installation of S-TEC System 65 two axis automatic flight guidiance system Model ST-414. | | Amended | | 3/31/1997 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA727WE | | Installation of Brittain Industries Model TT-5 wing tip fuel tanks. | | Reissued | | 9/17/1987 |
| SA72RM | | Installation of camera wells. | | Amended | | 12/9/1976 |
| SA738CE | | Install King Radio KNC 610 area navigation computer. | | Reissued | | 2/28/2000 |
| SA756SW | | Installation of Mitchell automatic flight system model AK236 consisting of Century II autopilot with optional radio coupler. | | Reissued | | 6/25/1984 |
| SA766WE | | Plastic wing tips replaced with Speedplates SP51463. | | Issued | | 6/6/1965 |
| SA767WE | | Modification to include three pair of seat belts on rear seat to accommodate three passengers. | | Issued | | 1/1/1960 |
| SA776CE | | Installation of King Radio KN-74 area navigation computer. | | Reissued | | 2/28/2000 |
| SA787WE | | Installation of turbosupercharged Lycoming IO-320-B1A IO-320-C1A LIO-320-B1A or LIO-320-C1A engines in accordance with FAA sealed Rajay Drawing List No. RJ0600. | | Reissued | | 6/26/2006 |
| SA789CE | | Install Woodward propeller unfeathering accumulator kit number 213630. | | Reissued | | 3/20/1992 |
| 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 |
| SA808NW | | Installation of an Edo-Aire Mitchell Century IIB autopilot (approved for installation on a Piper PA-30 by STC SA3045SW) on a Robertson modified PA-30 (STC 2312WE) | | Issued | | 7/26/1979 |
| SA808SW | | Installation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW. | | Reissued | | 6/29/1984 |
| SA816EA | | Installation of 13 quart alcohol propeller anti-icing kit WAP-500B. | | Amended | | 10/15/1971 |
| SA838SW | | Installation of Mitchell glide slope coupler Model 1C493. | | Reissued | | 6/29/1984 |
| SA8430SW | | Installation of an EQ1500 paralleling relay. | | Issued | | 8/26/1992 |
| SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
| SA848EA | | Installation of pneumatic pump operated wing and tail de-icing boot system. | | Issued | | 10/22/1970 |
| SA8513SW-D | | Installation of a Century Automatic Flight System Model AK1017 consisting of a Century 2110/2130/2131/2150/2151 autopilot. | | Issued | | 2/19/1996 |
| SA871WE | | Installation of fiberglass wing tips. | | Amended | | 9/23/1996 |
| SA875GL | | Install speed sweep windshield. | | Reissued | | 5/7/1997 |
| SA8891SW-D | | Install S-TEC System 55 2 axis automatic flight guidance system Model ST-562 with optional autotrim system. | | Amended | | 4/18/2001 |
| SA890EA | | Installation of Grimes three light strobe kit P/N 34-0101-2 as supplemental lighting. | | Reissued | | 6/4/2007 |
| SA891SO | | Remove existing windshield and install single piece windshield. | | Reissued | | 8/16/2011 |
| 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 |
| SA917EA | | Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). | | Reissued | | 6/4/2007 |
| ST01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| 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 |
