| 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 |
| SA00029AT | | Installation of Speed Splitter flap bracket fairings. | | Issued | | 11/20/1992 |
| SA00059AT | | Installation of flap gap seals. | | Issued | | 12/21/1992 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00064AT | | Installation of aileron gap seals. | | Issued | | 12/21/1992 |
| SA00068SE (PAGE 2) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 0:00 |
| SA00072SE | | Cockpit sun visor installation. | | Amended | | 6/2/2005 |
| SA00076WI | | Manufacture and installation of replacement wing tips. (PA-32RT-300T S/N 32R-7787001 and on PA-32-300 S/N 32-7940001 and on PA-32R-300 S/N 7680001 and on PA-32RT-300 S/N 32R-7885001 and on) | | Amended | | 10/29/1993 |
| SA00079BO | | Installation of Meriden GS-22 glide slope antenna. | | Issued | | 1/21/1998 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| 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 |
| SA00190BO | | Installation of Avidyne Corporation Primary Flight Display. | | Issued | | 1/30/2004 |
| SA00191BO | | Installation of Avidyne Corporation Multi-Function Display. | | Issued | | 1/30/2004 |
| SA00193AT | | Installation of carbon steel discs. | | Reissued | | 11/14/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00236DE | | Installation of Oilamatic Preoiler system. | | Issued | | 6/5/1996 |
| 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 |
| SA00261NY | | Installation of Aviation Services Inc. Model 1201 Cockpit Utility Light. | | Reissued | | 12/31/2002 |
| 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 |
| SA00282BO | | Installation of Avidyne Corporation Entegra Integrated Flight Display System | | Amended | | 4/4/2013 |
| 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 |
| SA00332BO | | Installation of non-hazard ice protection system kits | | Issued | | 6/18/2013 |
| SA00387NY | | Installation of replacement windshields. | | Issued | | 1/11/1996 |
| 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 |
| SA00639WI | | Installation of the GARMIN GPS 155SL GPS Receiver. | | Issued | | 3/16/1998 |
| SA00640WI | | Installation of GARMIN GNC 300XL VHF Communication Transceiver/GPS Receiver. | | Issued | | 3/16/1998 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00705WI | | Installation of Garmin GNS 430 VHF Communication Transceiver/VOR/ILS Receiver/GPS Receiver. | | Amended | | 7/25/2002 |
| SA00705WI-D | | Installation of the Garmin GNS 430 or 430A | | Reissued | | 10/17/2007 |
| SA00710WI | | Installation of Garmin GMA 340 audio panel. | | Reissued | | 12/13/2001 |
| SA00762SE | | Installation of Precise Flight Inc. Speedbrake 2000 System | | Amended | | 11/7/2003 |
| SA00769CH | | Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540 AEIO-540 and HIO-540 engines. | | Reissued | | 2/10/2009 |
| SA00780SE (PAGE 1) | | Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. | | Amended | | 5/11/2010 |
| SA00800WI | | Installation of GARMIN GPS 400 with (1) Garmin Dwg No. 005-C0084-00 Rev B dtd 6/17/99 Master Dwg List GPS 400 Installation in Piper PA32 and (2) FAA Approved Flight Manual Supplement (AFMS) for Piper PA32 Garmin GPS 400 Receiver Rev A dtd 7/6/99 or later FAA approved revisions of (1) or (2). | | Reissued | | 5/29/2001 |
| SA00800WI-D | | Installation of the Garmin GPS 400. | | Reissued | | 10/17/2007 |
| SA00801WI | | Installation of GARMIN GNC 420 or GNC 420A. | | Amended | | 7/24/2002 |
| SA00801WI-D | | Installation of the Garmin GNC 420 or GNC 420A | | Issued | | 7/6/1999 |
| SA00812NY | | Installation of Technisonic Industries Limited TFM-138 A and B (does not include TFM-138 s/n 1540 and up TFM-138B s/n 1500 and up). | | Amended | | 9/12/2005 |
| SA00816CH | | Installation of McCauley Propeller Model B3D3C431/80VSA-2 and spinner assembly. | | Reissued | | 9/23/2005 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00864WI | | Installation of GNS 530 or GPS 500 for (1) Installation Data referenced on Sheet 2 and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Sheet 2. | | Amended | | 11/22/2004 |
| SA00864WI-D | | Installation of the Garmin GNS 530 530A or GPS 500 (GNC 500 Series TAWS Option). | | Reissued | | 8/27/2007 |
| SA00870WI | | Installation of GTX 327 transponder. | | Issued | | 4/3/2000 |
| SA00923AT | | Installation of composite propeller spinner. | | Amended | | 10/13/2000 |
| SA00953AT | | Installation of a composite HOWL COWL mod comp engine cowling w/COWL FLAPS full length nosegear close doors belly fairing aft of firewall to streamline forward sec of exposed belly structures strakes and large access doors on both sides of cowling. | | Issued | | 1/26/1996 |
| SA00954AT | | Installation of composite bulkhead. | | Amended | | 3/31/2004 |
| SA00954SE (1 OF 2) | | Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. | | Amended | | 8/11/2003 |
| SA00954WI | | Installation of Concorde RG Series Battiers in Piper Single Engine Airplanes. | | Issued | | 4/2/2001 |
| SA01038AT | | Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28 -28R -32 -32R -34 series MODELS WITH CONSTANT-CHORD WINGS) | | Issued | | 5/13/1996 |
| SA01066WI | | Installation of B&C Specialty Products BC410-1 Standby Alternator System. | | Amended | | 11/6/2006 |
| SA01071LA | | Installation replacement tail cone fairing assembly. | | Issued | | 10/6/2000 |
| SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01105WI-D (2 OF 2) | | Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). | | Amended | | 5/31/2007 |
| SA01107SE | | RMD Aircraft Lighting high intensity discharge wingtip light manufactured | | Amended | | 4/2/2003 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01120SE | | Installation of Door Steward. | | Amended | | 3/4/2010 |
| SA01125WI | | Installation of Garmin GTX 330 Mode S Transponder with Traffic Information System Capability. | | Amended | | 6/22/2005 |
| SA01143WI | | Installation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft. | | Reissued | | 3/12/2003 |
| 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 |
| SA01161SE | | Approval of this change in type design applies to the airplane models listed above only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications including changes in type design will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( If the holder agrees to permit another person to use this certificate to alter the product the holder shall give the other person written evidence of that permission. | | Issued | | 1/8/2003 |
| SA01170NY | | Installation of NPX138N-XXX FM Transceiver. | | Amended | | 1/17/2007 |
| 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 |
| SA01266SE | | Installation of vortex generators on the wings and tail surfaces of the above model aircraft | | Amended | | 11/4/2009 |
| 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 |
| SA01328WI | | Installation of TKS Ice Protection System components with placard stating Intentional Flight into known icing is prohibited. Data Required: (1) AS&T Master Drawing List No. 12700DL Revision 3 dated March 7 2005 or later FAA Approved revision and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) Document 12700-FMS dated May 13 2005 or later FAA Approved revisions to (1) or (2). | | Reissued | | 7/8/2008 |
| SA01330LA (PAGE 2) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
| 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 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| 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 |
| SA01481SE | | Installation of the Garmin G1000 integrated avionics system in accordance with Garmin AT Master Data List 005-C0150-00 Revision B or later FAA approved revision. | | Issued | | 2/20/2008 |
| SA01487SE-D (Page 2) | | Installation of a GDL 69 or GDL 69A XM Satellite Receiver | | Amended | | 5/4/2012 |
| SA01560WI-D | | Installation of the Honeywell KFD 840 Primary Flight Display System.
);INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. | | Amended | | 7/22/2010 |
| SA01582SE | | Installation of battery box. | | Amended | | 5/12/2006 |
| SA01588NY-D | | Installation of a WSI Inflight Weater Briefing System (AV-200). | | Reissued | | 11/26/2003 |
| SA01627WI | | Installation of replacement gas spring door stays on the forward and/or rear cabin doors in accordance with Sioux Center Aviation Drawing List 65DL Revision C dated October 18 2010 or later FAA-approved revisions. | | Issued | | 4/4/2011 |
| SA01643SE | | Installation of BAS Inc. shoulder harness with inertia reel | | Amended | | 12/2/2010 |
| SA01653WI | | Activation of Automatic Speech Recognition (ASR) on a GMA 350/350H Audio Panel | | Issued | | 12/1/2011 |
| SA01660AT | | Installation of composite engine cowling with cowl flap. | | Issued | | 6/25/1998 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01675AT | | Installation of composite wingtips with recognition lights under a lens. | | Issued | | 7/9/1998 |
| 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 |
| SA01831AT-D | | Installation of FFC engineering order P28-2810-001. | | Issued | | 5/12/1999 |
| SA01834CH (1 OF 2) | | Installation of the High Intensity Discharge Light Assembly Kit. | | Amended | | 3/20/2009 |
| SA01834CH (2 OF 2) | | Installation of the High Intensity Discharge Light Assembly Kit. | | Amended | | 3/20/2009 0:00 |
| SA01860NY (2 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 4) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| 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 |
| SA02029CH | | Installation of a Projects Unlimited AVX-5 Interface Computer. | | Issued | | 9/8/2004 |
| 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 |
| SA02093AK | | Installation of hourmeter airspeed switch. | | Issued | | 10/17/1997 |
| SA02097CH | | Installation of a McCauley Propeller Systems B3D32C414/82NDA-2 propeller with optional LORD engine mount isolators. | | Issued | | 3/22/2005 |
| 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 |
| 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 |
| 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 |
| SA02246LA | | Installation of a flap handle extension. | | Amended | | 11/16/2010 |
| SA02249SE | | Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor | | Amended | | 9/18/2013 |
| SA02256CH | | Installation of a Hartzell Propeller model HC-I3Y (scimitar) | | Issued | | 3/10/2006 |
| 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 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| SA02293AK (2 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02384CH | | Installation of Flight Boss LTD SPA-32/34 Series Organizers. | | Issued | | 3/2/2007 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02532AT | | Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. | | Issued | | 6/5/2002 |
| SA02547AT (PG 2) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| SA02579AT | | Installation of a fuel transfer pump incorporating sold state hardware in place of older breaker point hardware. | | Issued | | 11/1/2002 |
| 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 |
| SA02695CH | | Installation of MT-Propeller MTV-9-B/198-52 constant speed propeller in accordance with Professional Pilots Inc. Installation Instructions #SUTN3201MT dated December 22 2006 or later FAA approved revision. | | Issued | | 3/25/2009 |
| 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 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09160AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-640 with optional autotrim system. | | Amended | | 6/28/2001 |
| SA09290AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-733-20/30. | | Issued | | 10/29/1997 |
| SA09294AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-739-20/30. | | Issued | | 11/5/1997 |
| SA09306AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-737-20/30. | | Issued | | 11/12/1997 |
| SA09310AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-738. | | Issued | | 11/17/1997 |
| SA09331AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-734. | | Issued | | 1/22/1998 |
| SA09333AC-D | | Installation of S-TEC system 30 alt altitude hold system. | | Issued | | 1/29/1998 |
| SA09454AC-D | | Installationo f S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-791-40X/50X | | Issued | | 6/5/2000 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA09491SC | | Installation of a low voltage warning system. | | Amended | | 5/3/2001 |
| SA09524SC | | Conversion of existing Piper air conditioning system from R12 to R134a refrigerant. | | Amended | | 3/26/2002 |
| 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 |
| SA1013GL | | Modify the Piper standard nose and main landing gear wheel fairings. (PA-32-300 S/N UP THRU 32-7940020) | | Reissued | | 5/7/1997 |
| SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA10286SC | | Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot. | | Issued | | 9/27/2004 |
| SA10530SC | | Installation of Cargo Net. | | Issued | | 1/10/2007 |
| SA10594SC | | Modification of the Monroe Automotive Equipment Co. (MAECO) Shimmy Dampener. | | Issued | | 12/7/2006 |
| SA1073GL | | Installation of cooling shroud on engine driven dry air pumps. | | Amended | | 5/1/2007 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1105CH | | Installation of a Hartzell HC-C3YR-1RF/F7693F propeller and 835-52(P) or C3535-1(P) spinner | | Issued | | 9/16/1999 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1123EA | | Installation of Devore vertical tail floodlights on upper surface of horizontal stabilator. | | Reissued | | 2/28/1980 |
| SA1154EA | | Installation of radome pod on right wing. | | Reissued | | 2/6/1984 |
| SA1156EA | | Installation of radome pod on right wing. | | Reissued | | 2/6/1984 |
| SA1159EA | | Installation of DeVore Tel-Tail lights on lower surface of horizontal stabilator. | | Reissued | | 10/13/1983 |
| SA1172SW | | Mitchell flight system AK304 cons. of Piper autoflite II with optional auto aileron stabilizer and tracking system. | | Reissued | | 7/9/1984 |
| SA1195GL | | Install fairings over flap hinges. | | Amended | | 3/29/2010 |
| SA1201CE | | Installation of King KFC 200 2 axis flight control system with a King KCS-55 (or -55A) compass and a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller. (PA-32R-300 S/N 32R-7680001 AND UP) | | Reissued | | 2/28/2000 |
| SA1217GL | | Install wing root fairings. | | Amended | | 3/29/2010 |
| SA1226NW | | Installation of a Hoskins C.F.S 1000 computerized fuel system | | Issued | | 5/7/1981 |
| SA1310SW | | Installation of stretcher in lieu of rear seats. | | Amended | | 11/18/1993 |
| SA1362CE | | Chrome-plated brake disc instal- lation. | | Issued | | 8/18/1977 |
| SA1378SW | | Mitchell automatic flight system AK320 cons. of Century I and opt. tracker. | | Reissued | | 7/9/1984 |
| SA1401NW | | Installation of fiberglass wing tips with recognition lights. | | Amended | | 8/14/2008 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1430CE | | Install King KFC-200 automatic flight control system. | | Reissued | | 2/28/2000 |
| SA1439GL | | Installation of Pamco Emergency Backup Pneumatic System. | | Amended | | 4/11/1990 |
| SA1486SO | | Installation of speed enhancement kit. | | Reissued | | 6/22/2000 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1521GL | | Installation of Flap Aileron Flap/Fuselage and Stabilator Gap Seals. | | Amended | | 3/29/2010 |
| SA1522CE-D | | Installation of King KFC 200 Flight Control System (2 axis) with or without Flight Director. | | Reissued | | 2/28/2000 |
| SA1523WE | | Installation of Brittain Model B-4A Flight Control System | | Reissued | | 7/2/2013 |
| SA1557WE | | Installation of turbocharged Lycoming O-540-E4B5 engine | | Reissued | | 6/26/2006 |
| SA1567CE-D | | Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system and optional KAS 297B vertical speed and altitude selector. | | Reissued | | 2/28/2000 |
| SA1568SW | | Wing leading edge cuff flow fences optional wing tips and dorsal fin. | | Reissued | | 9/5/1979 |
| SA1572CE-D | | Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system and optional KAS 297B vertical speed and altitude selector. | | Reissued | | 2/28/2000 |
| SA1572GL | | Installation of rudder fin cap fairing with or without a strobe. | | Amended | | 7/15/1997 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1596GL | | Installation of on-board analyzer system. | | Issued | | 5/8/1991 |
| SA1607SO | | Fabrication and installation of nose wheel fairings. | | Reissued | | 7/17/1989 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1714GL | | Installation of Gear Lobe Fairings. | | Amended | | 7/21/1997 |
| SA1735GL | | Installation of Master Nag warning system. | | Amended | | 3/21/1994 |
| SA1742SO | | Installation of Lycoming IO-540-KIG5D engine. | | Issued | | 2/6/1985 |
| SA1791GL | | Installation of Hartzell HC-C3YR-1( )F/F7663R. | | Issued | | 9/4/1992 |
| SA17PC | | ONE ONLY STC SN 32-7440102: Removal of aft baggage door and installation of overboard dispensing unit. | | Issued | | 11/15/1974 |
| SA1801SO | | Installation of Laminar landing gear fairing additions. | | Reissued | | 6/20/2000 |
| SA1854SO | | Installation of a one-piece windshield. | | Reissued | | 11/16/1996 |
| SA1892SO | | Installation of adjustable trim tab on left aileron. | | Issued | | 2/5/1986 |
| SA2072NM | | Installation of Goodrich de-icing boots on the Hartzell HC-C3YR-1RF/F76663R propeller | | Issued | | 4/8/1983 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2114SO | | Installation of a hand control for the rudder. | | Issued | | 5/14/1987 |
| SA2167NM | | Installation of the Precise Flight stand-by vacuum system (SVS). | | Amended | | 11/7/2003 |
| SA2190NM Page 2 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA21NE | | Installation of Whelen A600-PR and A600-PG anti-collision strobe with forward and tail position light assemblies as replacements for wing tip lights. | | Issued | | 3/1/1978 |
| SA2217WE | | Installation of recontoured wing leading edge raked wing tips fuselage flap wing stall fences drooped ailerons in flaps down mode and dorsal fin (optional). (PA-32S-300 landplane only) | | Reissued | | 9/8/2005 |
| SA2241SO | | Fabrication and installation of main wheel fairings. | | Reissued | | 7/17/1989 |
| SA2253WE | | Installation of Edo Model FD-3500-21 amphibious floats. | | Amended | | 2/15/2001 |
| 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 |
| SA2350NM Page 2 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2356NM | | Installation of R.M.D. Aircraft Lighting Inc. Landing/Recognition Lights Kit. | | Amended | | 3/29/2010 |
| SA2498WE | | Installation of Goodrich de-icing boots on the Hartzell HC-C2YK propeller | | Amended | | 1/10/1979 |
| SA249NE | | Modification of the engine cooling and induction system. | | Issued | | 3/28/1984 |
| SA2556NM | | Installation of rear facing center seats (club seats). | | Issued | | 2/20/1985 |
| 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 |
| SA260GL | | Install a BF Goodrich RNAV 511 area navigation system with 51ASA(Alpha) or 51DSA (Delta) steering adapter or without either adapter. | | Reissued | | 1/31/1992 |
| SA2687NM (PAGE 2) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 0:00 |
| SA2693NM (PAGE 2) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 0:00 |
| SA281AL | | Installation of large nose gear fork and 8.00-6 nose gear tire. | | Reissued | | 4/5/2012 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA2933WE | | Installation of oxygen system. | | Reissued | | 1/26/1984 |
| SA2935NM | | Installation of Turboplus Intercooler System. | | Reissued | | 10/15/2007 |
| SA2941NM | | Installation of Precise Flt Speedbrake system. | | Amended | | 11/7/2003 |
| SA2946SW | | Addition of Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
| SA3011SW-D | | Mitchell automatic flight system AK488 cons. of Piper altimatic IIIC w/opt. command/automatic electronic pitch trim radio coupler and glide slope coupler. | | Reissued | | 8/1/1984 |
| SA3026SW-D | | Mitchell automatic flight system AK463 consisting of Century IIB autopilot with optional radio coupler. | | Amended | | 8/1/1984 |
| SA3052SW-D | | Mitchell automatic flight system AK529 consisting of Piper Altimatic IIIC autopilot with command/automatic electric pitch trim optional radio coupler. | | Reissued | | 6/22/1984 |
| SA3053SW-D | | Installation of Mitchell automatic flight system AK530 cons. of Piper autocontrol IIIB autopilot with opt. radio coupler. | | Reissued | | 6/22/1984 |
| SA3054SW-D | | Mitchell automatic flight system AK531 cons. of Piper autoflite II w/opt. omni tracker. | | Reissued | | 6/22/1984 |
| SA3055SW-D | | Mitchell command/electric trim system Model AK532. | | Reissued | | 6/22/1984 |
| SA308EA (2 OF 2) | | Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) | | Amended | | 11/20/1978 0:00 |
| SA3098SO | | This modification will allow installation of Causey Aviation hinge assembly P/N 62371-108. | | Amended | | 7/2/1992 |
| SA3102SW-D | | Mitchell automatic flight system AK591 consisting of Century IIB autopilot w/opt radio coupler. | | Reissued | | 5/24/1984 |
| SA3103SW-D | | Mitchell automatic flight system model AK592 consisting of Century III autopilot with optional radio coupler and glide slope coupler. | | Reissued | | 5/24/1984 |
| SA3107SW-D | | Installation of Mitchell automatic flight system model AK581 consisting of a Century III autopilot with optional radio coupler and glide slope coupler. | | Reissued | | 5/24/1984 |
| SA311NW | | Installation of full span flaps by removing aileron and changing the deployment route of all flaps. | | Reissued | | 9/8/2005 |
| SA3152SW-D | | Installation of Mitchell automatic flight system model AK621 consisting of Century IV autopilot or AK621FD consisting of Century IV flight director autopilot with optional remove annunciator. | | Reissued | | 6/6/1984 |
| SA3159SO | | Replacement of Piper stabilator trim barrel P/N 63530-000 with Causey Aviation stabilator trim barrel P/N CA-63530-100. | | Issued | | 2/12/1992 |
| SA3167SW-D | | Installation of Mitchell automatic flight system model AK304 consisting of Piper autoflite II autopilot with optional omni tracker system. | | Reissued | | 6/7/1984 |
| SA3173SW-D | | Mitchell automatic flight system AK174 cons. of Piper autocontrol IIIB autopilot w/opt radio coupler. | | Reissued | | 6/18/1984 |
| SA317NE | | Installation of Auto-Vac-2 manifold vacuum system. | | Amended | | 2/2/1990 |
| SA3181NM | | Installation of Hartzell HC-E3YR-1()F/F7673DR-0 three-blade propeller on a Lycoming TIO-540-SIAD engine. | | Reissued | | 6/2/1999 |
| SA3218SO | | Replacement of Piper stabilator trim shaft P/N 65246-000 with Causey Aviation stabilator trim shaft P/N CA65246-100. | | Issued | | 4/29/1992 |
| SA3253SW-D | | Mitchell automatic flight system AK677 consisting of Piper altimatic IIIC autopilot with optional radio and glide slope couplers. | | Reissued | | 3/29/1984 |
| SA3254SO | | Installation of main landing gear fairings. | | Issued | | 6/8/1992 |
| SA3254SW-D | | Mitchell command electric trim system AK 678. | | Reissued | | 3/29/1984 |
| SA3255SW-D | | Mitchell automatic flight system AK 679 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 3/29/1984 |
| SA3273SO | | This modification will allow installation of Causey Aviation cowl plate assembly P/N CA69791-000. | | Issued | | 7/2/1992 |
| SA3287NM | | Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. | | Amended | | 11/14/1986 |
| SA3305SW-D | | Mitchell automatic flight system AK775 consisting of Piper altimatic IIIC autopilot with optional radio and glide slope couplers. | | Reissued | | 9/21/1983 |
| SA3306SW-D | | Mitchell automatic flight system AK776 consisting of Century III autopilot with optional and glide slope couplers. | | Reissued | | 9/21/1983 |
| SA3309SW-D | | Installation of Mitchell automatic flight system consisting of Century IV autopilot or AK771 consisting of flight director autopilot with optional remote annunciator. | | Reissued | | 9/21/1983 |
| SA3334NM | | The Model 706 VHF Communication Radio P/N 430-0054-0 ( )-0( ) is installed on the Piper Model PA-32R-300 airplane in accordance with II Morrow Inc. Installation Report No. 49 dated November 26 1985. | | Reissued | | 12/5/2003 |
| SA3361SW | | Mitchell automatic flight system AK865 consisting of Century 41 autopilot or AK865FD consisting of flight director autopilot. | | Reissued | | 8/24/1983 |
| SA3362SW-D | | Mitchell automatic flight system AK864 consisting of Century 21 autopilot. | | Reissued | | 8/24/1983 |
| SA3370SW-D | | Mitchell automatic flight system AK320 consisting of Century I and optional tracker. | | Issued | | 3/27/1980 |
| SA3374SW-D | | Mitchell automatic flight system AK872 consisting of command electric trim. | | Reissued | | 8/24/1983 |
| SA3380SW-D | | Mitchell automatic flight system AK879 consisting of Century 31 autopilot. | | Reissued | | 8/24/1983 |
| SA3405SW-D | | Edo Avionics automatic flight system AK896 consisting of Century 31 autopilot. | | Reissued | | 8/23/1983 |
| SA3442SW-D | | Installation of Century automatic flight system Model AK947. | | Amended | | 2/28/1997 |
| SA3472SW-D | | Installation of Century Automatic Flight System Model AK979. | | Amended | | 3/13/2013 |
| SA3504NM | | Installation of a Turboplus Inc. instrument sub-panel system | | Reissued | | 10/15/2007 |
| SA3513WE | | Installation of Roto-Master (Rajay) turbocharged Lycoming IO-540-K1G5D engine. | | Reissued | | 7/3/2006 |
| SA364GL | | For T tail configuration - installation of Norton radome kit No. 4229X. For conventional tail configuration - installation of Norton radome kit No. 4229XC. | | Reissued | | 12/5/2000 |
| SA3670WE | | Installation of Silver Instruments Fueltron IG or IP or Fuelgard digital fuel flow indicating system. | | Reissued | | 4/29/1991 |
| SA371EA | | Zeiss aerial camera and intervalometer. | | Issued | | 1/1/1960 |
| SA3736WE | | Installation of an engine oil cooler hose. | | Issued | | 9/22/1978 |
| SA3774WE | | Installation of Hoskins Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA3839WE | | Installation of an air/oil separator. | | Reissued | | 9/28/2001 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA3NW | | Installation of Van s Aircraft Model VA-1 fiberglass wheel fairings. | | Issued | | 8/1/1972 |
| 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 |
| SA409GL | | Installation of a Lycoming IO-540-K1A5 engine Hartzell propeller and associated components. | | Issued | | 5/23/1980 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA4288WE | | Installation of inflatable door seal. | | Amended | | 8/18/1983 |
| SA429GL | | Installation of Edo-Aire Mitchell automatic flight system Model AK771 consisting of a Century IV autopilot. | | Issued | | 8/4/1980 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4327WE | | Installation of rudder brake and flap systems hand controls MFG. | | Amended | | 1/19/1984 |
| SA433CH | | Installation of McCauley Propeller Model B3D36C427/82NGA-2. | | Amended | | 10/30/2006 |
| SA4345WE | | Installation of cooling louvers in the top cowling. | | Issued | | 5/7/1981 |
| SA472SO | | Installation of hand control for rudder pedal operation. rudder pedal operation. | | Amended | | 6/27/1974 |
| SA4745NM | | Installation of Lifeport Patient Loading and Support System. | | Amended | | 11/23/1993 |
| SA4778NM | | Installation of Blackwood Cherokee Mk. I hand control. | | Issued | | 10/12/1989 |
| SA4840SW | | Installation of an Auxiliary Instrument Air System. | | Reissued | | 4/6/2007 |
| SA4994SW | | Install TI 9100 Loran C Navigator. | | Issued | | 4/26/1983 |
| SA4995SW | | TI 9100 Loran C navigator and King Radio KAP autopilot or KFC 200 integrated autopilot flight director system. | | Issued | | 4/27/1983 |
| SA5121SW-D | | S-TEC System 60 two axis flight guidance system ST-098 with optional automatic electric trim system. | | Reissued | | 9/18/1990 |
| SA5122SW-D | | Installation of S-TEC yaw damper system Model ST-134. | | Reissued | | 7/9/1984 |
| SA5123SW-D | | S-TEC System 60 single axis autopilot ST-126 (14 volt). | | Issued | | 12/1/1982 |
| SA5131SW-D | | S-TEC System 60 single axis automatic flight guidance system ST-097. | | Amended | | 9/19/1984 |
| SA5137SW-D | | S-TEC System 60 pitch stabilization system ST-099 with optional autotrim system. | | Issued | | 2/24/1983 |
| SA514GL | | Installation of Norton radome kit No. 4262X. | | Reissued | | 12/5/2000 |
| 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 |
| SA5160SW-D | | S-TEC System 60 two axis automatic flight guidance system Model ST-162 with optional automatic electric trim system. | | Amended | | 6/24/1992 |
| SA5161SW-D | | S-TEC yaw damper system ST-164. | | Issued | | 5/20/1983 |
| SA5163SW-D | | Installation of S-TEC System60 single axis automatic flight guidance system ST-161. | | Amended | | 3/22/1993 |
| SA5164SW-D | | S-TEC System 60 pitch stabilizer system ST-163 with optional automatic electric trim system. | | Amended | | 2/23/1993 |
| SA5255SW-D | | S-TEC System 40/50 single and two axis automatic flight guidance system ST-203-40/50. | | Amended | | 2/10/1993 |
