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 |
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 |
SA00196AT | | Installation of Appalachian Accessories carbon steel brake discs that have melonite surface treatment P/N AA-17. | | Reissued | | 11/14/1994 |
SA00208AT | | 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 |
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 |
SA00258AT | | Installation of a Century/Mitchell1 Single Axis autopilot. | | Issued | | 8/5/1993 |
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 |
SA00410SE | | Installation of steel nose landing gear link. | | Issued | | 2/7/1997 |
SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
SA00559SE | | Installation of nose gear bushings | | Issued | | 8/20/1998 |
SA00680SE (5 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
SA00717AT | | Installation of composite aft spinner bulkhead. | | Amended | | 10/13/2000 |
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 |
SA00793SE | | Installation of cabin door loop manufactured | | Amended | | 3/17/2010 |
SA00843SE | | Installation of tailskid | | Issued | | 9/28/2000 |
SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
SA00931AT | | Installation of composite propeller spinner. | | Amended | | 10/13/2000 |
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 |
SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
SA01130SE | | Sterling Aviation Technologies Inc. Kit No. SA500 Piper PA-38-112 Tomahawk Fatigue Life Extension Wing Spar Modification. | | Issued | | 10/10/2002 |
SA01147WI | | Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. | | Reissued | | 7/30/2012 |
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 |
SA01293SE | | Sterling Aviation Technologies Inc. Drawing List No. SA700 Piper PA-38-112 Tomahawk Upper Cabin Door Handle Assembly. Manufactured in accordance with Sterling Aviation Technologies Inc. Drawing List SA700 Revision NC dated September 17 2003 or later FAA approved revisions. | | Issued | | 11/7/2003 |
SA01330LA (PAGE 3) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
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 |
SA01699SE | | Cockpit Sun Visor installation | | Issued | | 9/27/2006 |
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 |
SA02023SE | | Fabrication and installation of Frame Station 260.42 Fuselage Bulkhead for the Piper Aircraft PA-38-112 | | Issued | | 8/3/2009 |
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 |
SA02110CH (PAGE 3) | | 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 |
SA02168AK (PG 1) | | Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. | | Issued | | 3/23/2001 |
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 |
SA02268CH (PAGE 5) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
SA02283SE Page 2 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
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 |
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 3) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
SA02738CH (PAGE 2) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
SA02987CH | | Installation of the Electroair Electronic Ignition System | | Amended | | 7/23/2013 |
SA03114AT | | Installation of Gomolzig Quietflight Low Noise Silencer P/N PA38-606500. | | Issued | | 5/26/2005 |
SA03148NY (PAGE 2 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
SA10126SC (2 OF 2) | | Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision. | | Amended | | 10/23/2003 |
SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
SA191NE | | Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. | | Reissued | | 10/4/1984 |
SA2059NM | | Installation of a modified Lycoming0-235-L2C designated as0-235-L2C(M) in accordance with STC SE3877NM. | | Amended | | 1/8/2008 |
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 |
SA2276SO | | Replacement of Cleveland brake discs P/N 164-69 with Appalachian Acces. stainless steel brake discs P/N 75-69. | | Issued | | 3/23/1988 |
SA2277SO | | Replacement of Cleveland brake discs P/N 164-17 or 164-117 with Appalachian Accessories stainless steel brake discs P/N 64-17. | | Reissued | | 9/29/1995 |
SA2350NM Page 2 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
SA2366SO | | Installation of modified upper door latch. | | Issued | | 6/28/1988 |
SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
SA2586NM (PAGE 4) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
SA2687NM (PAGE 1) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 |
SA2693NM (PAGE 2) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 0:00 |
SA2951SW | | Addition of Hydro Seal Fluid Additive to the landing gear shock struts. | | Reissued | | 8/8/1980 |
SA3204SO | | Installation of Appalacian Accessories stainless steel brake discs P/N 75-69. | | Reissued | | 9/29/1995 |
SA3404SO | | Installation of Appalachian stainless steel brake disks. | | Issued | | 4/30/1992 |
SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
SA4005NM (PG 4) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
SA4135NM | | Install Lycoming 0-235-L2C/L2A(M) engine (modified per STC SE792NW) and Sensenich 72CK-0-52/57 propeller. | | Issued | | 10/30/1987 |
SA4136NM | | Installation of one of the following optional oil cooler: Stewart Warner 10578B 10568A(C) 8046R Harrison 8526250. | | Issued | | 10/30/1987 |
SA4146NM | | Installation of Madras Air Service Model No. 110 Wing Tips. | | Issued | | 4/15/1988 |
SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
SA559CH | | Installation of Inline Air Filter Kit P/N CV1J4-P. | | Reissued | | 1/15/2013 |
SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
SA5755NM | | Installation of a propeller anti theft device. | | Issued | | 8/5/1992 |
SA5924NM | | Installation of RPM instrument. | | Amended | | 11/24/1997 |
SA5925NM | | Installation of oil pressure/temperature instrument. | | Amended | | 12/8/1997 |
SA5926NM | | Installation of manifold pressure instrument. | | Amended | | 8/15/1993 |
SA593CH (3 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
SA8922SW | | Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) | | Issued | | 7/21/1994 |
ST00961LA | | Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29 2000 or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1 Slug Thrower Cartridges Master Drawing List | | Reissued | | 7/13/2011 |
ST01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
ST01494LA (PG 2) | | Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. | | Reissued | | 8/30/2011 |
ST01700NY (2 OF 2) | | Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator. | | Issued | | 7/8/2003 |