| SA00009SE | | Fiberglass wing tips and wing tip landing lights. | | Reissued | | 12/23/2011 |
| SA00024NY | | Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. | | Amended | | 10/3/2012 |
| SA00028AT | | Installation of speed splitter flap bracket fairings. | | Issued | | 11/20/1992 |
| SA00043AT | | Removal of existing aluminum battery and starter cables and replacement of cables with copper cables. | | Issued | | 12/21/1992 |
| SA00047NY | | Installation of replacement windows. | | Amended | | 7/21/1997 |
| SA00060AT | | Installation of flap gap seals. | | Issued | | 12/21/1992 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00063AT | | 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 |
| SA00070BO | | Installation of P/N 9725 carburetor heat shroud. | | Issued | | 6/26/1997 |
| SA00072SE | | Cockpit sun visor installation. | | Amended | | 6/2/2005 |
| SA00079NY | | Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. | | Amended | | 10/31/2012 |
| 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 |
| SA00176AT | | Installation of composite spinner assemblies. | | Issued | | 4/5/1993 |
| SA00178AT | | Installation of composite spinner and/or spinner bulkheads. | | Amended | | 10/13/2000 |
| SA00191AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00193AT | | Installation of carbon steel discs. | | Reissued | | 11/14/1994 |
| SA00198AT | | Installation of carbon steel brake discs. | | Reissued | | 11/14/1994 |
| SA00206AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00238SE | | Installation of Aviation Development Corporation s sump mounted chip detector | | Issued | | 10/31/1995 |
| 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 |
| 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 |
| SA00379NY | | Increase in maximum gross weight to 2440 pounds. | | Reissued | | 8/8/2006 |
| SA00393SE | | Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. | | Issued | | 12/6/1996 |
| SA00395NY | | Installation of .250 in. thick replacement windshields. | | Issued | | 2/1/1996 |
| SA00397NY | | Increase in maximum gross weight to 2440 pounds. | | Issued | | 2/14/1996 |
| 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 |
| SA00444WI-D | | Installation of Bendix/King KAP 140 Automatic Flight Control System with optional KCS 55A Compass System. For model PA-28-181 serial numbers 2890206 thru 2890231 and 2843001 and after | | Reissued | | 2/28/2000 |
| SA00477DE | | Installation of engine cowling baffle exhaust and oil cooler. Limited to installation on PA-28-140 serial number 28-7325528 ONLY. | | Issued | | 7/12/2002 |
| SA00507AT | | Modification of battery box. | | Issued | | 6/8/1994 |
| SA00633LA | | Installation of an electric constant speed propeller MTV-18B/180-7 and control unit P-120-U. | | Issued | | 5/15/1998 |
| 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 |
| SA00720CH | | Installation of McCauley Propeller Model B3D36C431/80VSA-1. | | Reissued | | 9/21/2005 |
| SA00744DE | | Installation of Automatic Dependent Surveillance | | Amended | | 3/28/2013 |
| SA00760SE | | Installation of glare shield. | | Reissued | | 5/20/2010 |
| 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 |
| 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 |
| SA00849SE | | Installation of vortex generators on wings and tail surfaces. | | Issued | | 10/27/2000 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00915CH | | Installation of McCauley Propeller Model D3A36C436/74SA-0 and spinner assembly. | | Reissued | | 9/23/2005 |
| SA00927AT | | Installation of composite propeller spinner. | | Amended | | 5/20/2004 |
| SA00945AT | | Installation of composite forward bulkhead. | | Amended | | 10/13/2000 |
| 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 |
| SA00955AT | | Installation of composite bulkhead. | | Amended | | 10/13/2000 |
| SA01024CH | | Installation of a Hartzell PHC-C3YF-1RF/F7663-4T propeller and C-3570(P) spinner in accordance with Hartzell installation instructions HP2834 dated February 3 1999 or later FAA approved revision. | | Issued | | 4/6/1998 |
| SA01026SE (PAGE 1) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| 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 |
| SA01042AT | | Installation of Composite Spinner. | | Amended | | 10/13/2000 |
| 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 |
| SA01100AT | | Installation of Composite Spinner. | | Amended | | 3/31/2004 |
| 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 |
| SA01121AT-D | | Installation of FFC engineering order P28-2810-001. | | Issued | | 5/12/1999 |
| 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 |
| SA01170NY | | Installation of NPX138N-XXX FM Transceiver. | | Amended | | 1/17/2007 |
| SA01174LA | | Installation of supplemental baggage compartment below existing rear baggage compartment. | | Issued | | 2/28/2002 |
| SA01190LA | | Installation of Hartzell HC-C3YR-1RF/F7693F propeller and Hartzell C-3535-1(P) spinner. | | Issued | | 8/15/2001 |
| SA01191LA | | Installation of Hartzell HC-F3YR-1ARF/F7693F propeller and Hartzell C-3570(P) spinner. Responsible ACO is Los Angeles NM-L. | | Issued | | 8/15/2001 |
| 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 |
| 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 |
| SA01319AT | | Installation of new composite engine cowling with cowl flap and large inspection access doors on both sides of cowling. | | Amended | | 5/20/1997 |
| 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 |
| SA01482AT | | Manufacture of sun visor. | | Issued | | 10/20/1997 |
| 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 |
| 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 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01690AT | | Installation of Archangel Avionics Cockpit Display System. | | Issued | | 8/21/1998 |
| 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 |
| SA01786SE | | Fabrication and installation of wing tips | | Issued | | 9/7/2007 |
| SA01787SE | | Fabrication and installation of wing tips | | Issued | | 9/7/2007 |
| SA01800SE (PG 3) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01807SE | | Installation of vortex generators on the wings and horizontal and vertical tail surfaces of the above model aircraft | | Issued | | 12/4/2007 |
| 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 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 |
| SA01944CH (2 OF 2) | | Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. | | Issued | | 3/5/2004 0:00 |
| SA01982AT | | Installation of new composite wingtip with recognition light. | | Amended | | 9/23/1999 |
| SA01988SE (PAGE 5) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA02013CH | | Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). | | Amended | | 5/2/2011 |
| SA02015CH | | Installation of Three-Point Torso Restraint System. | | Issued | | 7/30/2004 |
| 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 |
| SA02022CH | | Installation of Pneumatic Luggage Door Strut Kit. | | Issued | | 8/16/2004 |
| 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 |
| SA02093AK | | Installation of hourmeter airspeed switch. | | Issued | | 10/17/1997 |
| 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 |
| SA02149AK | | Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. | | Reissued | | 5/17/2013 |
| 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 |
| SA02168AT | | Modification of engine exhaust system for improved engine performance by installation of a Laminar Flow System Extractor Exhaust System. | | Amended | | 2/28/2003 |
| SA02203AK (PAGE 1) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02212AK (PG 3) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. | | Amended | | 5/4/2011 |
| SA02217AK (4 OF 5) | | Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision. | | Amended | | 12/1/2004 0:00 |
| 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 |
| 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 (1 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02410AT | | Replace existing Auxiliary Electric Standby Fuel Pump with PMA Products Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v) 1A15-s/n 24-3642 24-4000 through 24-4782 24-4784 through 24-4803 2A13-s/n 28-7690001 through 28-7990626 28-8090001 and up(14v) | | Issued | | 10/10/2001 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02454AT | | Installation of a shoulder harness restraint system. | | Issued | | 5/7/2002 |
| 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 |
| SA02555CH | | Installation of Hartzell HC-C2YR-1BFP/F7497 constant speed propeller. | | Issued | | 4/17/2008 |
| SA02572AT | | Installation of a PXE7300 In-Flight Entertainment System. | | Amended | | 2/13/2003 |
| SA02579AT | | Installation of a fuel transfer pump incorporating sold state hardware in place of older breaker point hardware. | | Issued | | 11/1/2002 |
| SA0258AT | | Install MT-Propeller Model MTV-12-D/188-30d Propeller and Spinner Assembly on Piper Models PA-28R-201T and PA-28RT-201T aircraft per MT-Propeller Operation and Installation Manual E-124 Issue 26 dated November 29 2001 or later FAA approved revision. Airplane Flight Manual Supplement (AFMS) E-677-E dated December 19 2000 or later FAA approved revision is a required part of this STC. | | Issued | | 1/8/2003 |
| SA02707AT | | Installation of a PAV80 In-Flight Entertainment Audio-Video System on a Piper PA-28-181 Archer III aircraft | | Issued | | 9/3/2003 |
| 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 |
| SA02770AT | | Installation of Aeronautical Electronics Corporation Electronic Checklist Models AEC-ECTO AEC-ECTS or AEC-APWS. | | Issued | | 12/18/2003 |
| SA02777CH | | Installation of a Hartzell PHC-C3YF-1RF/F7663-2R Model Propeller | | Issued | | 11/6/2009 |
| 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 |
| SA03207AT | | Installation of Gomolzig Quietflight Low Noise Silencer P/N PA28-606500. | | Issued | | 1/20/2006 |
| SA03208AT | | Installation of Gomolzig Quietflight low noise silencer. | | Issued | | 1/20/2006 |
| SA03209AT | | Installation of Gomolzig Quietflight low noise silencer P/N PA-28-606503. | | Issued | | 1/20/2006 |
| SA03210AT | | Installation of Gomolzig Quietflight low noise silencer P/N PA-28-606504 | | Issued | | 1/20/2006 |
| SA03303AT | | Installation of Thielert Aircraft Engines (TAE) Aircraft Diesel Engine model TAE 125-01 and MT-Propeller model MTV-6-A-187/129 propeller and other minor modifications. | | Issued | | 7/24/2006 |
| SA03470AT | | Installation of a replacement cowling for Piper Turbo Arrow models. | | Issued | | 8/13/2007 |
| SA09129AC-D | | Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-610 with optional autotrim system. | | Amended | | 11/20/2000 |
| SA09155AC-D | | Installation of S-TEC System 60 Pitch Stabilization System Model ST-630 with Optional Autotrim System. | | Issued | | 5/20/1996 |
| SA09159AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-635 with Optional Autotrim System. Eligibility limited to Piper model PA-28-235 serial number 28-7310001 and up. | | Amended | | 5/25/2001 |
| SA09166AC-D | | Installation of S-TEC System 55 Two Axis autoomatic flight guidance system Model ST-642 with Optional Autotrim System. Eligibility limited to Piper PA-28-235 s/n 28-10003 through 28-11393 and s/n 28-7110001 through s/n 28-7210023. | | Amended | | 8/1/2002 |
| SA09222AC-D | | Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-683-2/30. | | Issued | | 5/19/1997 |
| SA09233AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-684. | | Issued | | 6/3/1997 |
| SA09251AC-D | | Installation of S-Tec System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-703-20/30. | | Issued | | 6/26/1997 |
| SA09252AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-704. | | Issued | | 6/30/1997 |
| SA09254AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-711-20/30. | | Issued | | 7/7/1997 |
| SA09257AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-712. | | Issued | | 7/11/1997 |
| SA09287AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance System Model ST-729-20/30. | | Issued | | 10/13/1997 |
| SA09292AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-730. | | Issued | | 10/24/1997 |
| SA09328AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-764-20/30. | | Issued | | 1/19/1998 |
| SA09346AC-D | | Installation of S-TEC system 30 alt altitude hold system. | | Issued | | 3/3/1998 |
| SA09414AC-D | | Installation of S-TEC System 40X/50X single and two axis automatic flight guidance systems model ST-867-40X/50X. | | Issued | | 2/17/2000 |
| SA09415AC-D | | Installation of S-TEC system 50XP two axis automatic flight guidance system Model ST-779. | | Issued | | 10/13/1999 |
| SA09444AC-D | | Installation of S-TEC GPSS ARINC 429 converter/interface Model ST-901. Eligibility limited to model PA-28-140 serial number 28-21392. | | Amended | | 12/10/2001 |
| 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 |
| SA09623AC | | Installation of Century Flight Systems Model AK1069 Triden autopilot. Eligible on Piper PA-28-180 serial number 28-4378 and after. | | Issued | | 3/21/2003 |
| SA09666AC | | Installation of a Global Positioning Steering System (GPSS) consisting of a GPSS Adapter Controller 1C975-0 and a GPSS Annunciator/Switch 1C977-0 or 1C977-1 | | Issued | | 3/21/2006 |
| SA1-468 | | Six or 13 quart propeller anti- icing kit WAP-101A revision 2. | | Amended | | |
| SA1-649 | | Lube oil filter PB55-1. | | Issued | | 1/1/1960 |
| SA100EA | | AF-510 AF-512A or AF-512B autopilots. | | Issued | | 1/1/1961 |
| SA10126SC (2 OF 2) | | Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision. | | Amended | | 10/23/2003 |
| SA1012GL | | Modify the Piper standard nose and main landing gear wheel fairings. (PA-28-151 ALL S/N S PA-28-161 S/N S UP THRU 28-7916228 PA-28-181 S/N S UP THRU 28-7990242) | | Amended | | 8/5/1998 |
| SA10207SC | | Limited to installation on PA-28-140 serial number 28-20983 ONLY. | | Issued | | 1/30/2004 |
| SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA10281SC | | Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot. | | Reissued | | 9/28/2006 |
| SA1043NW | | Installation of a ski compartment | | Issued | | 10/27/1980 |
| SA1046SO | | Installation of an adjustable trim tab on left aileron. | | Amended | | 4/26/1996 |
| SA1053GL | | Install hand controller to actuate rudder pedals. | | Amended | | 8/3/1988 |
| 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 |
| SA1072CE | | Installation of wing leading edge cuffs and droop tips dorsal fin and vertical stabilizer vortex generator. | | Amended | | 11/6/1984 |
| SA1072GL | | Installation of cooling shroud on engine driven dry air pumps. | | Amended | | 5/1/2007 |
| SA1075SO | | Wing-Ding door stop to be installed using existing screws(Piper P/N 415 309 MS27039-0809) on leading edge of right wing at inboard side of fuel cell(W.S. 57.00). | | Issued | | 5/18/1979 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1093GL | | Installation of Airborne Auxiliary Dry Air Pump Kit No. 374-2 or 374-3. | | Reissued | | 1/27/1987 |
| SA110SO | | Electric pitch trim system. | | Issued | | 1/1/1996 |
| 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 |
| SA1131EA | | Installation of a radome pod on right wing. | | Reissued | | 2/6/1984 |
| SA1156EA | | Installation of radome pod on right wing. | | Reissued | | 2/6/1984 |
| SA1157SW | | Mitchell flight system AK295 con- sisting of Piper AutoFlite II auto- matic aileron stabilizer and optional tracking system. | | Reissued | | 7/9/1984 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA1183CE | | Installation of King Model KFC 2002 axis flight control system with a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon indicator with a KC-292 mode controller. (PA-28R-200 S/N 28R-7235001 AND UP PA-28R-201 S/N 28R-7737002 and up | | Reissued | | 2/28/2000 |
| SA1189SW | | Air circulator. | | Issued | | 9/15/1970 |
| SA1191WE | | Removal of baggage door for aerial photography operations. | | Issued | | 1/1/1960 |
| SA1192EA | | Installation of Safe Flight (SFIC) SC-150 speed control system. | | Issued | | 4/15/1980 |
| SA1194GL | | Install fairings over flap hinges. | | Amended | | 7/15/1997 |
| SA1202WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1214GL | | Installation of Pamco emergency backup pneumatic system. (PA-28-181 S/N 28-7690001 THRU 28-7990626) | | Amended | | 4/27/1988 |
| SA1216GL | | Install wing root fairings. | | Amended | | 7/15/1997 |
| SA1216SO | | Installation of an adjustable trim lab on the left aileron. | | Amended | | 11/4/1981 |
| SA1227CE | | Installation of dorsal fin. | | Amended | | 7/10/1991 |
| SA1228CE | | Installation of wing tip extension. | | Amended | | 6/1/1974 |
| SA1237SW | | Mitchell automatic flight system Model AK314 consisting of altimatic IIIB-1 with optional automatic pitch trim and radio coupler and glide slope coupler. | | Amended | | 8/3/1988 |
| SA1258EA | | Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584) | | Amended | | 4/11/1983 |
| SA1272SW | | Mitchell automatic flight system AK307 consisting of Century I and omni tracker. | | Reissued | | 7/9/1984 |
| SA129CH | | Installation of propeller model B3D36C424/74SA. | | Reissued | | 7/19/2006 |
| 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 |
| SA1317CE | | Chrome-plated brake disc installation. | | Amended | | 3/1/1978 |
| SA1331CE | | Installation of 160 hp Lycoming engine and repitched Sensenich propeller. | | Amended | | 1/25/1996 |
| SA1354WE | | PAS-1 stability augmentation system. | | Reissued | | 10/20/1972 |
| SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
| SA1373CE | | Install third window. (PA-28-180 S/N 28-1 THRU 28-4377 PA-28-235 S/N 28-10003 THRU 28-11039) | | Amended | | 11/17/1977 |
| SA1383CE | | Installation of Edo-Aire propeller governor Model 34-828-014-12. | | Reissued | | 9/17/1990 |
| SA1401NW | | Installation of fiberglass wing tips with recognition lights. | | Amended | | 8/14/2008 |
| SA1406SW | | Mitchell automatic flight system Model AK269 consisting of Piper Autocontrol III autopilot with optional radio coupler. | | Reissued | | 7/10/1984 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1437NM | | Installation of a rear cabin shelf and closeout panel. | | Reissued | | 12/3/1996 |
| SA1463SO | | Installation of Speed Enhancement Kit. | | Issued | | 6/2/1983 |
| SA1469WE | | Installation of Brittain Model B2C Flight Control System | | Reissued | | 7/2/2013 |
| SA1470WE | | Installation of Brittain Model PAS-1 stability augmentation system. | | Reissued | | 10/20/1972 |
| SA1484WE | | Installation of Brittain Industries Inc. Model B2C Flight Control System | | Reissued | | 1/29/2013 |
| SA1485NM | | Installation of a Lycoming IO-360-A1B6 and a Hartzell HC-M2YR-1B/7666A-2 propeller and associated baffling changes | | Issued | | 3/15/1982 |
| SA1487SO | | Installation of speed enhancement kit. | | Reissued | | 6/21/2000 |
| SA148RM | | Install Hoskins Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA148SW | | Replacement of right front seat with stretcher. | | Reissued | | 8/21/1987 |
| SA1498CE | | Installation of King KFC 200 automatic flight control system two axis with or without flight director | | Reissued | | 2/28/2000 |
| SA1499GL | | Installation of on-board engine analyzer system. | | Issued | | 7/12/1990 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1563CE-D | | Install 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 |
| SA1565CE-D | | Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system. | | Reissued | | 2/28/2000 |
| SA1571GL | | Installation of rudder fin cap fairing with or without a strobe. | | Amended | | 7/21/1997 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1580SO | | Installation of speed enhancement kit. | | Reissued | | 6/20/2000 |
| SA1588WE | | Installation of supplemental exterior flashing lights. | | Issued | | 1/30/1968 |
| SA1607SO | | Fabrication and installation of nose wheel fairings. | | Reissued | | 7/17/1989 |
| SA1616NM | | Installation of a Hartzell propeller on a Continental engine | | Issued | | 4/14/1982 |
| SA1623GL | | Installation of McCauley governor model C290D3(x)/T39. | | Reissued | | 7/19/2006 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA164SW | | Automatic pilot AK092E. | | Issued | | 1/1/1960 |
| SA1692GL | | Installation of Pamco emergency backup pneumatic system. (PA-28-236 s/n 28-7911001 thru 28-8111018) | | Issued | | 1/22/1992 |
| SA1696SO | | Installation of one-piece windshield. | | Amended | | 6/1/1994 |
| SA1713GL | | Installation of gear lobe fairings. | | Amended | | 7/15/1997 |
| SA1716SW | | Mitchell automatic flight system AK430 consisting of AutoFlite II with optional omni tracker. | | Reissued | | 7/16/1984 |
| SA1717SW | | Mitchell automatic flight system AK431 consisting of auto-control III or IIIB with optional radio coupler. | | Reissued | | 7/16/1984 |
| SA1735GL | | Installation of Master Nag warning system. | | Amended | | 3/21/1994 |
| SA1741WE | | Installation of hand control for the rudder system. | | Reissued | | 5/5/1997 |
| SA1745SO | | Installation of Appalachian Access. stainless steel brake rotors P/N 75-20. | | Reissued | | 2/6/1995 |
| SA1762NM | | Installation of a pressurized magneto system on the Continental turbocharged TSIO-360-C F and FB engines. | | Reissued | | 3/14/2006 |
| SA1764GL | | Installation of Vortex generators. | | Amended | | 6/25/2001 |
| SA1766NM | | Installation of rudder hand control for paraplegic | | Issued | | 12/3/1982 |
| SA1789WE | | Installation of Brittain lateral stability augmentation system and super venturi. | | Reissued | | 10/1/1973 |
| SA178WE | | Full flow aerofilter 30409A with element 1A0235. | | Issued | | 1/1/1960 |
| SA1792WE | | Installation of Morse protection system. | | Issued | | 1/1/1960 |
| SA1800SO | | Installation of Laminar landing gear fairing additions. | | Reissued | | 6/21/2000 |
| SA180EA | | Geared starter. | | Issued | | 1/1/1960 |
| SA1842NM | | Installation of an Avco Lycoming O-360-A4M engine and a Sensenich 76EM8-0-60 propeller and associated installation components. | | Reissued | | 5/10/2005 |
| SA1898SW | | Installation of wing leading edge cuff flow fences optional wing tips and dorsal fin. | | Reissued | | 9/5/1979 |
| SA1914SO | | Installation of a STOL kit or STOL/Speed kit combination. | | Issued | | 4/23/1986 |
| SA191NE | | Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. | | Reissued | | 10/4/1984 |
| SA194GL | | Installation of Lycoming IO-360-C1C6 engine in lieu of Lycoming IO-360- C1C engine using original instal- lation hardware and components. | | Reissued | | 2/10/1997 |
| SA1963CE | | Operation on unleaded and/or leaded automotive gasoline. | | Issued | | 3/23/1984 |
| SA1964CE | | Operation on unleaded and/or leaded automotive gasoline. | | Issued | | 3/23/1984 |
| SA1971WE | | Installation of Model ARB-3 Automatic Downed Aircraft Marker( ADAM ). | | Amended | | 11/21/1969 |
| SA2-952 | | Installation of fiberglass covering. | | Reissued | | 9/10/1996 |
| SA2052WE | | Installation of Hartzell HC82XL-6F/8433-12 propeller(after conversion of engine to Lycoming O-320-E1A model). | | Reissued | | 3/25/2004 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2143WE | | Installation of recontoured wing leading edge drooped ailerons in flaps down mode wing stall fences fuselage flap raked wing tips flap actuated elevator trim spring modified flap cove and dorsal fin. (PA-28-235 S/N28-10001 thru 28-7210023) | | Reissued | | 9/8/2005 |
| SA2144NM | | Installation of a modified air induction system to the Continental TSIO-360 engine turbocharger compressor (Rayjay) system. | | Reissued | | 10/15/2007 |
| SA2145NM | | Installation of Turboplus intercooler system. | | Reissued | | 10/15/2007 |
| SA2147NM | | Installation of Continental TSIO-360-FB(C) (converted)* engine and associated system. (PA-28RT-201T Turbo Arrow III) (PA-28-201T Cherokee) | | Reissued | | 10/15/2007 |
| SA2147WE | | Installation of Brittain Industries B-7 flight control system. | | Reissued | | 11/20/1972 |
| SA2148NM | | Installation of Turboplus engine nacelle cowl flaps. | | Reissued | | 10/15/2007 |
| SA2156CE | | Installation of flap and aileron gap seals. | | Amended | | 12/14/1988 |
| SA2167NM | | Installation of the Precise Flight stand-by vacuum system (SVS). | | Amended | | 11/7/2003 |
| SA2171NM | | Installation of Precise Flight speedbrake system. | | Amended | | 3/10/2005 |
| SA2178SO | | Replacement of Cleveland brake discs P/N 164-25A or 164-125A with Appalachian Accessories stainless steel brake discs P/N 75-25A. | | Issued | | 9/25/1987 |
| SA2179WE | | Installation of leading edge cuff drooped ailerons in flaps down mode wing stall fences raked wing tips fuselage flap stabilator trim spring and dorsal fin (optional). (PA-28-180 S/N 28-03 28-1 thru 28-7205318 S/N 28-E13) (PA-28 SERIES 7305001 AN D UP | | Reissued | | 9/8/2005 |
| SA2190NM Page 2 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2194CE | | Installation of Hoerner style wing tips. | | Issued | | 9/26/1986 |
| SA21NW | | Installation of a 70 pound baggage compartment in either or both EDO 89-2000 89A-2000 or 689-2130 floats | | Amended | | 9/25/2009 |
| SA2202WE | | Installation of recontoured leading edge drooped ailerons in flaps down mode fuselage flap stabilator trim spring wing stall fences raked wing tips and dorsal fin (optional). (PA-28R-200 s/n 28R-35001 thru 28R-7135329 and s/n 28-R-235001 and up) | | Reissued | | 10/10/1986 |
| SA2213WE | | Conversion of Lycoming O-360-A3A engine to Model O-360-A1A engine and installation of Hartzell HC-C2YK1-B/7666A-0 propeller. | | Reissued | | 3/25/2004 |
| SA2223NM | | Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA222SW | | Hartzell HC-82XL-6N/7636D-4 propeller and cowl rework. | | Issued | | 1/1/1960 |
| SA2230CE | | Installation of replacement stabilator tips. | | Issued | | 2/27/1987 |
| SA2241SO | | Fabrication and installation of main wheel fairings. | | Reissued | | 7/17/1989 |
| SA224CE | | Installation of Model A3000 main skis and NB-1200 nose skis. | | Reissued | | 2/16/1993 |
