| 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 |
| 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 |
| SA00079SE | | Installation of low oil pressure warning in conjunction with ADC (Oberg) oil filter. | | Amended | | 11/10/1994 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00159SE | | 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 |
| SA00175DE | | Installation of Oilamatic Preoiler system. | | Amended | | 4/14/2003 |
| SA00193AT | | Installation of carbon steel discs. | | Reissued | | 11/14/1994 |
| SA00198AT | | Installation of carbon steel brake discs. | | Reissued | | 11/14/1994 |
| SA00198LA | | Relocation and replacement of the fuel boost pumps. (PA-24-250 S/N 24-2999) | | Issued | | 5/20/1996 |
| 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 |
| 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 |
| SA00290AT | | Installation of cowl flaps NACA air vent scoops for cabin ventilation and additional main landing gear doors. | | Issued | | 8/2/1993 |
| 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 |
| SA00327WI | | Installation of seals on lower surface of airplane between wing ailerons and flaps. | | Issued | | 6/6/1995 |
| SA00336NY | | Installation of second wind auxiliary vacuum system. | | Reissued | | 6/18/2002 |
| SA00343AT | | Installation of engine cowl and full length gear doors and relocation of engine oil cooler and replacement exhaust system. For PA-24-250 S/N 24-103 and up for PA-24-260 S/N 24-3642 24-4000 to 24-4782 and 24-4784 to 24-4803. | | Reissued | | 5/2/2001 |
| SA00391SE | | Installation of Rajay Model 315 F10 turbocharger on the above aircraft with a Lycoming O-360-A1A engine installed. | | Reissued | | 5/18/1999 |
| 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 |
| SA00423LA | | Installation of Hartzell HC-C3YR-1RF/F7590 propeller. | | Issued | | 8/21/1997 |
| SA00424AT | | Installation of flap gap seals. | | Issued | | 2/14/1994 |
| SA00426AT | | Installation of a composite WHOLLEY COWL. | | Amended | | 1/24/1996 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00484WI | | Installation of shoulder harness for two front seats. | | Reissued | | 3/25/2009 |
| SA00618AT | | Installation of a stabilator modification kit. | | Issued | | 12/9/1994 |
| SA00631CH | | Installation of the Hartzell propeller model HC-C2YR-1BF/F7666A-4 or HC-C2YR-1BFP/F7497 propeller | | Amended | | 5/14/2013 |
| 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 |
| SA00695SE | | Replacement of certain Rotomaster and Rayjay scavenge pumps | | Amended | | 2/14/2003 |
| SA00746WI | | Installation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901) | | Reissued | | 3/25/2009 |
| 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 |
| SA00773CH | | Installation of McCauley propeller model B3D32C412/82NDA-5 and McCauley governor model DC290D1/T34. | | Reissued | | 7/19/2006 |
| 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 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00927AT | | Installation of composite propeller spinner. | | Amended | | 5/20/2004 |
| SA00947AT | | Installation of composite spinner. | | 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 |
| SA01026SE (PAGE 1) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01082AT | | Installation of new fiberglass cowling full length gear doors relocation of engine oil cooler and replacement of the exhaust system. (PA-24-180) | | Amended | | 1/26/1998 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| 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 |
| SA01201AT | | Installation of left hand side and right hand side auxiliary tank fuel cell assemblies. | | Reissued | | 5/1/2009 |
| 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 |
| SA01257AT | | Installation of composite spinner assemblies. | | Amended | | 10/13/2000 |
| SA01280CH | | Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) | | Issued | | 8/29/2000 |
| SA01299SE | | Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics Inc. Drawing Package Document MA2191 Revision IR dated September 17 2003 and Installation Manual MA2192 Revision IR dated October 27 2003 or later FAA approved revision to either of these documents. | | Issued | | 11/14/2003 |
| 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 |
| SA01352LA | | Replacement of Piper Battery box part numbers 20659-00 21524-00 21524-02 25338-00 or 26240-00 and venting battery with Riley Aircraft Battery Box part number 1001TR and Gill manifold battery Model G-35M. | | Issued | | 7/18/2002 |
| SA01421AT | | Installation of an OCEM AP-3C autopilot. (PA-24-180) | | Reissued | | 4/6/2004 |
| SA01435DE | | Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine. | | Reissued | | 5/25/2011 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01462WI | | Installation of 3-blade MT-Propeller model MTV-9-B/198-58a propeller and P-296-5 spinner | | Issued | | 12/21/2007 |
| 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 |
| SA01538AT | | Installation of Hartzell HC-C3YR-1RF/F7590 or HC-C2YK-1A or HC-C2YK-1B propellers. | | Issued | | 12/31/1997 |
| 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 |
| 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 |
| SA01834CH (1 OF 2) | | Installation of the High Intensity Discharge Light Assembly Kit. | | Amended | | 3/20/2009 |
| SA01853AT | | Replace Aluminum alloy propeller spinner with composite spinner. | | Amended | | 10/13/2000 |
| 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 (4 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
| 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 |
| 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 |
| SA02033AT (PAGE 6) | | Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) | | Amended | | 7/25/2008 0:00 |
| 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 |
| 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 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 |
| SA02260SE | | Move the main wheel brake calipers from the outboard side of the wheel forks to the inboard side of the wheel forks and modify the wing rib at station 33 | | Issued | | 1/7/2014 |
| 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 |
| SA02492CH | | Installation of a Three Point Torso Restraint System. | | Issued | | 10/29/2007 |
| 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 |
| 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 |
| 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 |
| SA04016AT | | Installation of The Aeronautical Design Service (ADS) part number 1008020828 Stabilator Horn | | Reissued | | 9/12/2013 |
| SA09012AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system model ST-595 with optional automatic electric trim system. Eligible on Piper models PA-24 (PA-24-180) PA-24-260 when modified per STC SA4-1351 or STC SA4-1235 as applicable (wing tip tanks). | | Amended | | 5/30/2001 |
| SA09260AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-715-20/30. (PA-24-180) | | Issued | | 7/29/1997 |
| SA09266AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-716. | | Issued | | 8/12/1997 |
| SA09413AC-D | | Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-777-40X/50X. | | Issued | | 9/12/2000 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA1-340 | | Oil-free vacuum pump PA-201. | | Issued | | |
| SA1-383 | | Lube oil filter PB 55-1. | | Issued | | |
| SA1-544 | | External electrical power receptacle. | | Reissued | | 10/15/1974 |
| 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 |
| SA1021NE | | Installation of a 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 |
| SA1026SW | | Mitchell automatic flight system Model AK186 consisting of Piper altimatic IIIB IIIB1 automatic auto-flite automatic/command electric pitch trim radio and glide slope couplers. | | Reissued | | 7/9/1984 |
| SA1027SW | | Mitchell manual electric pitch trim AK267. | | Reissued | | 7/9/1984 |
| SA1033EA | | Replace steel oil cooler lines with Aeroquip type 303-8 hose using AN-823-8D elbows AN-816-8D nipples and AN-321-8 hose fittings. | | Issued | | 1/29/1976 |
| 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 |
| SA108NE | | Replacement of brake disc Piper P/N 751672. | | Reissued | | 6/18/2002 |
| SA1109WE | | Hanlon and Wilson exhaust system. | | Issued | | 1/1/1960 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1115SW | | Dual brakes. | | Reissued | | 11/22/1998 |
| SA112CE | | APU receptacle. | | Issued | | 1/1/1960 |
| SA113CE | | APU receptacle. | | Issued | | 1/1/1960 |
| SA1152SW | | One-piece windshield. | | Reissued | | 3/14/1983 |
| SA1153SW | | Square wing tips with dual navigation lights. | | Amended | | 9/7/1999 |
| SA1167NW | | Installation of an updated instrument panel | | Issued | | 2/10/1981 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA1178EA | | Installation of Silver Instruments fueltron IG or IP or Fuelgard digital fuel flow indicating system | | Reissued | | 4/29/1991 |
| SA1182NW | | Installation of a Hartzell propeller on a Lycoming engine | | Issued | | 2/18/1981 |
| SA1202WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1216NW | | Installation of B.F. Goodrich de-icing boots | | Issued | | 4/14/1981 |
| SA1268NW | | Installation of a Hoskins FT-101 computerized fuel system | | Issued | | 7/20/1981 |
| SA127EA | | Installation of Monitair angle of attack system Model AA-2. | | Reissued | | 2/14/1972 |
| SA1315CE | | Chrome-plated brake disc installations. | | Issued | | 6/1/1977 |
| 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 |
| SA1331SW | | Mitchell automatic flight system AK326 consisting of Piper autoflite II and optional tracking system. | | Reissued | | 7/9/1984 |
| SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
| SA1394GL | | Installation of Pamco Emergency Backup Pneumatic System. (PA-24-400 S/N 26-2 AND UP) | | Amended | | 10/17/1989 |
| SA1412NM | | Installation of a Beech Craft Vernier throttle PN 35-944046 and associated changes | | Issued | | 12/30/1981 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| SA1485WE | | Installation of Brittain Industries Inc. Model B-11 B2C or BSS Flight Control System | | Reissued | | 1/29/2013 |
| SA148SW | | Replacement of right front seat with stretcher. | | Reissued | | 8/21/1987 |
| SA1497NM | | Installation of Shadin Digiflo fuel flow indicator system and removal of fuel pressure indicator system | | Issued | | 4/2/1982 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1521SW | | Mitchell automatic flight system AK393 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/13/1984 |
| SA1531GL | | Installation of on-board engine analyzer system. | | Reissued | | 10/25/1990 |
| 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 |
| SA1605WE | | Installation of Brittain Industries B-4A Flight Control System | | Reissued | | 7/2/2013 |
| SA160SW | | Automatic pilot AK115 AK115E or AK115E-3 and lateral guidance radio coupler AK123. | | Issued | | 1/1/1960 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1628NM | | Installation of nose gear doors and mounting of wheel brakes on inboard side of wheel fork | | Issued | | 4/30/1982 |
| SA1661GL | | Installation of rudder fin cap fairing with a strobe. | | Reissued | | 5/7/1997 |
| SA1665NM | | Installation of a Shadin Digiflo P/N 910501 or Miniflo P/N 912001 series fuel flow indicator system. | | Reissued | | 4/12/1988 |
| SA1667NM | | Installation of a Shadin Digiflo digital fuel flow indicator system | | Issued | | 6/28/1982 |
| SA1689SO | | Installation of shoulder harness. | | Issued | | 10/19/1984 |
| SA1706SW | | Portable solid oxygen system. | | Issued | | 7/27/1973 |
| SA1711GL | | Installation of Gear Lobe fairings. | | Reissued | | 5/7/1997 |
| SA1735GL | | Installation of Master Nag warning system. | | Amended | | 3/21/1994 |
| SA1755NM | | Installation of positive flap retraction system. | | Reissued | | 9/8/2005 |
| SA17CH | | Installation of windshield cowler fairing. | | Reissued | | 5/7/1997 |
| SA1806SO | | Installation of nose landing gear tire. | | Issued | | 7/10/1985 |
| SA1845WE | |
);INSERT INTO stc_table VALUES ( Installation of Vibration Isolation Products (VIP) engine mount P/N VIP-50804-20 on various aircraft as shown on FAA Approved Model List (AML) No. SA1845WE. | | Amended | | 10/17/2002 |
| SA188SO | | Flight control wheel. | | Issued | | 1/1/1960 |
| SA18SO | | Cockpit operated fuel drain valve. | | Issued | | 1/1/1960 |
| SA1918WE | | Installation of Fiberglass wing tips. | | Issued | | 4/24/1969 |
| SA191NE | | Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. | | Reissued | | 10/4/1984 |
| SA203SO | | Fyr-Fyter 23-4 2-1/2 pound dry chemical fire extinguisher. | | Issued | | 1/1/1960 |
| SA2062WE | | Installation of Lycoming IO-540-R1A5 engine and Rajay turbosuperchargers. | | Reissued | | 6/1/1970 |
| SA2071SO | | Installation of an adjustable trim tab on the left aileron. | | Issued | | 3/4/1987 |
| SA208GL | | 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 |
| SA2167NM | | Installation of the Precise Flight stand-by vacuum system (SVS). | | Amended | | 11/7/2003 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2269SO | | Replacement of Cleveland brake discs P/N 164-9 or 164-109 with Appalachian Accessories stainless steel brake discs P/N 73-9. | | Reissued | | 9/29/1995 |
| SA2272NM | | Installation of fiberglass window mouldings. (PA-24-260 24-1 thru 24-4299) | | Issued | | 4/16/1984 |
| SA230CE | | Airspeed indicator landing gear warning system. | | Issued | | 1/1/1960 |
| SA2336SO | | Replacement of Cleveland brake discs P/N 164-19 or 164-119 with Appalachian Accessories stainless steel brake discs P/N 73-19. | | Reissued | | 9/29/1995 |
| 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 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2359WE | | Installation of Turbocharged Lycoming 10-720-A1A engine | | Reissued | | 6/26/2006 |
| SA2485CE | | Installation of side windows with an increase of thickness from 1/8 inch to 1/4 inch. | | Issued | | 4/14/1989 |
| SA2495WE | | Installation of recontoured wing leading edge staff fences drooped ailerons in flaps down mode flap actuated stabilator trim system new wing tips SC-100 stall warning system. | | Reissued | | 9/8/2005 |
| SA2541NM | | Installation of fiberglass wing tips. | | Issued | | 12/19/1984 |
| SA2549CE | | Installation of a Webco door latch kit. | | 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 |
| SA2584CE | | Installation of LH and RH main fuel cell bladders P/N s DF054-324 and DF054-325 as replacements for original bladders. | | Reissued | | 7/31/2002 |
| SA2586NM (PAGE 4) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2619WE | | Installation of Pathfinder Model P1-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2620WE | | Installation of Pathfinder Model P2-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2648CE | | Installation of flap actuated gear warning system. | | Amended | | 12/15/1997 |
| SA2652CE | | Installation of main fuel cell bladders as replacements for original bladders. | | Reissued | | 7/31/2002 |
| SA2653WE | | Installation of Beryl D | | Reissued | | 7/14/2011 |
| SA2654WE | | Installation of Pathfinder Model P2A( ) autopilot. | | Amended | | 7/3/1979 |
| SA2674NM | | Installation of a Lamar Model B-00264-2 over-voltage relay and the replacement of the existing voltage regulator with Lamar regulator Model B-00288-1 | | Issued | | 11/27/1984 |
| 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 |
| SA2694CE | | Installation of manually controlled engine induction alternate air heat system. | | Issued | | 2/22/1991 |
| SA270GL | | Installation of forward windows P/N s W- W/T- WG-2058-187 or-250 and W- W/G-20599-187 or -250. | | Reissued | | 11/26/2008 |
| SA2713CE | | Installation of PRONAV global positioning system GPS-100 navigator. | | Reissued | | 10/7/1991 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA288CH | | Installation of Hartzell HC-C3YR-1RF/ F7590 propeller and 835-52P spinner. | | Amended | | 12/9/2002 |
| SA2944SW | | Addition of Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
| SA2SO | | Fifth passenger seat. | | Issued | | 1/1/1960 |
| SA3-309 | | L2-B autopilot with or without altitude control. | | Issued | | 1/1/1960 |
| SA3-315 | | Arcon B automatic rudder control. | | Amended | | 4/26/1966 |
| SA3-351 | | L-2B autopilot with optional altitude control and automatic approach coupler. | | Issued | | 1/1/1960 |
| SA3042SO | | Installation of Speed Spats main landing gear fairings. | | Issued | | 10/18/1991 |
| SA3045SW-D | | Mitchell automatic flight system consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/22/1984 |
| SA3070WE | | Installation of single piece windshield. | | Reissued | | 4/8/1999 |
| SA3074SW-D | | Mitchell automatic flight system AK547 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 6/21/1984 |
| SA3077SO | | Installation of speed spats main landing gear fairings and/or installation of Comanche speed slipper nose gear fairing. | | Amended | | 1/8/1992 |
| SA307CH | | Replace existing baggage door hold up bracket with an air strut bracket. (PA-24-260 24-4247 24-4300 and up) | | Reissued | | 5/17/1997 |
| 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 |
| SA3134SW-D | | Mitchell automatic flight system AK593 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/5/1984 |
| SA3135SW-D | | Mitchell automatic flight system AK597 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/5/1984 |
| SA3136SW-D | | Mitchell automatic flight system AK609 consisting of Century I auto-pilot with optional omni tracker. | | Reissued | | 6/5/1984 |
| SA313SW | | Pitch trim system AK124. | | Issued | | 1/1/1960 |
| SA315SW | | Fabrication and installation of split rear seat back. | | Issued | | 1/1/1960 |
| SA317NE | | Installation of Auto-Vac-2 manifold vacuum system. | | Amended | | 2/2/1990 |
| SA31NW | | Installation of Madras wing tips. | | Issued | | 3/13/1973 |
| SA3281SO | | Installtion of flap bracket fairings. | | Issued | | 7/13/1992 |
| SA331SO | | External power supply plug. | | Issued | | 1/1/1960 |
| SA334SW | | Installation of InterAv Alternator. | | Reissued | | 7/20/1981 |
| SA3359NM | | Modification of the vacuum system including installation of an engine which has been modified by the addition of a second engine driven vacuum pump. | | Issued | | 4/15/1986 |
| SA341CE | | SAGA (semi-automatic gear actuator) control system. | | Amended | | 9/6/1966 |
| SA3451WE | | Installation of Hartzell HC-A3VK4/V7636D-0 or V7636N-0 constant speed propeller. | | Amended | | 5/27/1980 |
| SA3466SW-D | | Installation of Century automatic flight system Model AK972 consisting of a Century 2010/2030/2031/2050/2051 autopilot. | | Amended | | 12/9/1992 |
| SA3469SW-D | | Installation of Century automatic flight system Model AK975 consisting of a Century 2010/2030/2031 autopilot. | | Amended | | 5/3/1994 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3550NM | | Installation of Hartzell / HC-C2YK-1BF/F8477D-5R . propeller | | Issued | | 12/10/1986 |
| SA3551NM | | Installation of Hartzell HC-C2YK-1BF/F8477D-5R propeller. | | Issued | | 12/10/1986 |
| SA3559NM | | Installation of ARNAV systems FC-10 or FT-10 digital fuel flow indicating system. (PA-24-260 with fuel injected normally aspirated engine) | | Issued | | 12/19/1986 |
| SA3565WE | | Installation of single piece windshield. | | Reissued | | 6/25/2001 |
| SA360CH | | Installation of McCauley propeller Model B3D36C424/74SA-0. | | Reissued | | 7/19/2006 |
| SA362WE | | Pneumatic pitch assist PC-1 and optional altitude hold AH-1. | | Reissued | | 10/1/1973 |
| SA3684WE | | Installation of an air/oil separator. | | Reissued | | 9/28/2001 |
| SA3707NM | | Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. | | Issued | | 5/7/1987 |
| SA371CH | | Installation of wing fillet. | | Reissued | | 5/7/1997 |
| SA3773WE | | Installation of Hoskins Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. *This installation limited to those aircraft with fuel injected engines. | | Reissued | | 1/30/1998 |
| SA3776WE | | Installation of flexible stainless steel oil cooler hoses. | | Issued | | 11/1/1978 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA3872NM | | Installation of an AVCO Lycoming IO-540-R1A5 engine as modified per STC No. SE3873NM for the addition of induction air intercoolers. | | Reissued | | 4/27/1995 |
| SA3955NM | | Installation of Weldon Model 8163A Auxiliary Fuel Pump in lieu of Dukes Model 4140-00-218 Fuel Pump | | Issued | | 10/11/1988 |
| SA4-1032 | | Aerofilter 30409A full flow lube oil filter with element 1A0235. | | Issued | | 1/1/1960 |
| SA4-1132 | | SP-3 autopilot less altitude and navigation-hold features. | | Issued | | 1/1/1960 |
| SA4-1235 | | Installation of 15-gallon wing tip fuel tanks. | | Reissued | | 8/17/1987 |
| SA4-1248 | | Fuel drain modified to incorporate a handle extending forward through front bulkhead. | | Issued | | 1/1/1960 |
| SA4-1351 | | Wing tip fuel tanks installed. | | Reissued | | 9/17/1987 |
| SA4-1501 | | AB-6562 and AB-6563 brake blocks. | | Issued | | 1/1/1960 |
| SA4-572 | | Autopilot and optional navigation coupler add-on BI-300 BI-301 or BI-304. | | Reissued | | 10/1/1973 |
| SA4-666 | | Installation of a Grimes D-7080-1-12 rotating beacon. | | Reissued | | 4/8/1991 |
| SA4-852 | | Full flow oil filter 30409A with element 1A0235. | | Issued | | 1/1/1960 |
| SA4-925 | | Magnetic flight director 2000. | | Issued | | 1/1/1960 |
| SA4-955 | | Fiberglass vertical fin mount for either Grimes or Whelen WRM rotating beacons. | | Reissued | | 7/14/2005 |
| SA4-956 | | Three seat belts to accommodate three persons or rear seat. | | Issued | | 1/1/1960 |
| SA4-971 | | 20-gallon auxiliary fuel tank in baggage compartment. | | Issued | | 1/1/1960 |
| 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 |
| SA4014NM | | Installation of a McCauley Model B3D32C412/82NDA propeller. | | Reissued | | 4/27/1995 |
| SA4150NM | | Installation of Precise Flight Series 100 Speedbrake System. | | Amended | | 11/7/2003 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA4179WE | | Installation of inflatable door seal. | | Issued | | 6/30/1980 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4313NM | | Installation of a stainless steel exhaust crossover system with dual outlets and dual heat muffs | | Issued | | 4/28/1988 |
| SA4317SW | | S-TEC system 60 two axis automatic flight guidance system Model ST-021 with optional autotrim flight director/steering horizon(14 volt system). | | Issued | | 3/26/1981 |
| SA434NE | | Installation of William C. Roberts steel brake discs P/N 201-19-SS dated 6/29/85 in lieu of Piper carbon steel brake discs Piper 754-530. | | Reissued | | 8/7/2002 |
| SA4361WE | | Installation of Silver Instruments Fueltron IG or Fueltron IP digital fuel flow indicating system. | | Reissued | | 2/2/1993 |
| SA4384SW | | Installation of cabin vent system. (PA-24 SN 24-1 to 24-3687) | | Reissued | | 8/18/1992 |
| SA4390SW | | Installation of single or dual toe brakes. | | Reissued | | 8/18/1992 |
| SA4401SW | | S-TEC system 60 single axis flight guidance system Model ST-020(14 volt system). | | Issued | | 6/30/1981 |
| SA4581SW | | Installation of S-TEC system Model ST-507 with optional autotrim system. | | Issued | | 1/11/1982 |
| SA4582SW | | Installation of JASC 6550 12-volt50 amp alternator J12-100 SP voltage regulator and associated wiring. | | Reissued | | 2/17/1982 |
| SA463GL | | Install instrument panel and instruments. (PA-24-250 24-2299 and above) (PA-24-260 24-3642 24-4000 thru 24-4802) (PA-24-400 26-2 and above) | | Issued | | 10/24/1980 |
| 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 |
| SA478EA | | SAGA (semi-automatic gear actuator) system. | | Issued | | 1/1/1960 |
| SA482WE | | Plastic wing tips replaced with Speedplates . | | Issued | | 6/6/1965 |
| SA489EA | | Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. | | Amended | | 12/5/2002 |
| SA48WE | | Belly-mounted rotating anti- collision light to supplement top fuselage-mounted standard rotating light. | | Issued | | 1/1/1960 |
| SA4958NM | | Installation of a hand control for the rudder. | | Issued | | 8/2/1990 |
| SA5-27 | | Remove Lycoming O-540-A1A5(250 hp) engine and install Lycoming O-540-B1B5 (235 hp) engine. | | Amended | | 3/3/1962 |
| SA510CE | | Modify electrical system to combination 12/24 volt system for starting engine. | | Issued | | 1/1/1960 |
| SA511WE | | Lycoming O-540-B1B5 engine Hartzell HC-A2XK-1/8433-7 propeller required. | | Issued | | 1/1/1960 |
| SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
