SA00002SE | | Installation of fiberglass reinforced plastic wing tips | | Issued | | 6/14/1993 |
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 1) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 |
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 |
SA00197AT | | Installation of Appalachian carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
SA00208AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
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 |
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 ( PAGE 2) | | 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 |
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 |
SA00478CH (PAGE 3) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
SA00638WI | | Installation of Concorde Battery Corporation (vrsla) Valve Regulated Sealed Acid Battery. | | Amended | | 8/10/2012 |
SA00747SE | | Installation of a Lycoming IO-360-A1B engine and a McCauley B3D36C429-82NPA-6 propeller. | | Issued | | 10/21/1999 |
SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
SA00780SE (PAGE 2) | | 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 |
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 |
SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
SA01158WI (2 OF 2) | | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | Amended | | 3/29/2005 1:00 |
SA01229SE Page 2 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
SA01240SE (3 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 |
SA01269LA | | Installation of replacement wing tip fairing assembly. | | Issued | | 11/21/2001 |
SA01280CH | | Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) | | Issued | | 8/29/2000 |
SA01330LA (PAGE 2) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 0:00 |
SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
SA01473SE (5 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 1) | | Installation of a GDL 69 or GDL 69A XM Satellite Receiver | | Amended | | 5/4/2012 |
SA01555SE | | Installation of vortex generators on the wings and tail surfaces. | | Issued | | 5/25/2005 |
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 |
SA01690SE | | Installation of S-TEC Autotrim System Model ST-667. | | Issued | | 7/19/2006 |
SA01692SE (Page 2 of 2) | | Installation of a Garmin GMX 200 Multi-Function Display | | Reissued | | 10/3/2012 |
SA01695SE (5 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
SA01714WI (Page 1) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
SA01800SE (PG 4) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
SA01860NY (1 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
SA01861SE (PAGE 4) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
SA01923LA | | Installation of the P-1000 Digital Electronic Tachometer. | | Issued | | 1/23/2007 |
SA01933LA-D Page 1 | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
);INSERT INTO stc_table VALUES ( System | | Amended | | 4/1/2013 |
SA01933LA (5 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
SA01988SE (PAGE 2) | | 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 |
SA02019SE-D | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/13/2013 |
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 |
SA02053SE | | Cockpit Sun Visor installation | | Issued | | 2/23/2010 |
SA02110CH (PAGE 3) | | Installation of a Time Trac Data Recorder | | Reissued | | 1/11/2010 |
SA02119SE Page 1 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
SA02153LA-D (Page 1) | | Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System | | Amended | | 12/16/2013 |
SA02168AK (PG 1) | | Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. | | Issued | | 3/23/2001 |
SA02217AK (5 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 |
SA02268CH (PAGE 4) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
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 1) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 |
SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
SA02738CH (PAGE 6) | | 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 |
SA03231AT | | Installation of an improved performance exhaust system. | | Issued | | 4/24/2006 |
SA09235AC-D | | Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance system Model ST-667 with Optional Autotrim System. | | Amended | | 10/25/2001 |
SA09409AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic flight Guidance Systems Model ST-855-20/30. | | Issued | | 5/24/1999 |
SA09510AC-D | | Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems model ST-889-20/30. | | Issued | | 6/22/2001 |
SA09514AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-893. | | Issued | | 11/19/2001 |
SA10126SC (1 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 (4 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
SA106GL | | Installation of Gerdes Products wheels and brakes. | | Issued | | 2/13/1976 |
SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
SA1147EA | | Installation of DeVore vertical tail floodlights on upper surface of horizontal stabilator. (23 S/N M-555 AND UP) | | Reissued | | 2/28/1980 |
SA1237GL | | Installation of a Shadin Co. fuel flow indicating system. | | Reissued | | 6/8/2006 |
SA1262WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
SA1276GL | | Installation of an auxiliary vacuum system. | | Reissued | | 4/21/1988 |
SA1290WE | | Installation of Quazar high- intensity supplemental exterior flashing lights. | | Amended | | 11/25/1969 |
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 |
SA1346SW | | Installation of Mitchell automatic flight system model AK341consisting of Century I autopilot and optional Omni Tracker. | | Reissued | | 7/10/1984 |
SA1348SW | | Installation of Mitchell automatic flight system AK342 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 7/10/1984 |
SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
SA1376WE | | Installation of Brittain Industries BSA-3 stability augmentation system. | | Reissued | | 10/20/1972 |
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 |
SA1475WE | | Installation of Brittain Model B2C Flight Control System. | | Reissued | | 10/20/1972 |
SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
SA1512WE (2 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 0:00 |
SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
SA1626NM Page 1 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
SA1680SO | | Installation of an adjustable nine-inch trim tab on the left aileron. | | Issued | | 9/20/1984 |
SA1701SW | | Mitchell command electric trim system Model AK454. | | Reissued | | 7/16/1984 |
SA1724WE | | Installation of Brittain Model B-5 flight control system. | | Reissued | | 10/20/1972 |
SA1735GL | | Installation of Master Nag warning system. | | Amended | | 3/21/1994 |
SA1952SO | | Installation of Appalachian Access. stainless steel brake discs P/N 75-43. | | Amended | | 1/14/1987 |
SA2054SO | | Installation of Appalachian Acces. stainless steel brake discs P/N 75-69. | | Amended | | 5/19/1992 |
SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
SA2148WE | | Installation of Brittain Industries B-VII NAV-2B B2C and BSA-6 flight control systems. | | Reissued | | 10/20/1972 |
SA2160NM | | 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 |
SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
SA2687NM (PAGE 1) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 |
SA2693NM (PAGE 1) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 |
SA2940SW | | Addition of Hydro Seal Fluid Additive to landing gear shock struts. | | Reissued | | 8/8/1980 |
SA3001SO | | Installation of Appalachian Accessories stainless steel brake discs P/N 75-43. | | Reissued | | 9/29/1995 |
SA3016SW-D | | Mitchell automatic flight system AK499 cons. of Century IV autopilot or AK499FD consisting of a Century IV flight director autopilot with opt. remote annunciator. | | Reissued | | 8/1/1984 |
SA308EA (1 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 |
SA3106SW-D | | Installation of Mitchell automatic flight system Model AK544consisting of a Century III auto-pilot with optional radio coupler and glide slope coupler. | | Reissued | | 5/24/1984 |
SA3153SW-D | | Installation of Mitchell automatic flight system Model AK632 consisting of a Century IIB autopilot with optional radio coupler. | | Reissued | | 6/6/1984 |
SA3154SW-D | | Installation of Mitchell automatic flight system Model AK633consisting of a Century I autopilot with optional omni tracker. | | Reissued | | 6/6/1984 |
SA3156WE | | Installation of Pathfinder autopilot systems. | | Reissued | | 9/30/1998 |
SA3160SW-D | | Installation of Mitchell command electric trim system Model AK454. | | Reissued | | 6/6/1984 |
SA3204SO | | Installation of Appalacian Accessories stainless steel brake discs P/N 75-69. | | Reissued | | 9/29/1995 |
SA3214SW-D | | Mitchell automatic flight system AK342 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 3/28/1984 |
SA3223SW-D | | Mitchell automatic flight system consisting of Century I autopilot and optional omni tracker. | | Reissued | | 3/28/1984 |
SA3291WE | | Installation of Pathfinder autopilot systems. | | Reissued | | 7/3/2002 |
SA3312SW-D | | Installation of Mitchell automatic flight system Model AK767 consisting of a Century I autopilot with optional omni tracking system. | | Reissued | | 8/15/1983 |
SA3313SW-D | | Mitchell automatic flight system AK768 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 9/21/1983 |
SA3314SW-D | | Mitchell automatic flight system AK769 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 9/21/1983 |
SA3315SW-D | | Mitchell command electric trim AK770. | | Reissued | | 9/21/1983 |
SA3331SW-D | | Mitchell automatic flight system AK779 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 9/21/1983 |
SA3332SW-D | | Mitchell automatic flight system AK780 consisting of Century IIB autopilot with optional radio couplers. | | Reissued | | 9/21/1983 |
SA334SW | | Installation of InterAv Alternator. | | Reissued | | 7/20/1981 |
SA3404SO | | Installation of Appalachian stainless steel brake disks. | | Issued | | 4/30/1992 |
SA3799WE | | Installation of flexible stainless steel oil cooler hoses. | | Issued | | 11/28/1978 |
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 |
SA4015WE | | Installation of Hoskins model fuel flow indicating system. | | Reissued | | 1/30/1998 |
SA401SW | | Full flow oil filter. | | Issued | | 1/1/1960 |
SA4152NM | | Installation of a Lycoming engine model O360-A4K | | Issued | | 12/17/1987 |
SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
SA423NW | | Conversion of a Lycoming O-320-E2C (150 HP @ 2700 rpm) to a O-320-D2A (160 HP @ 2700 rpm) with a Sensenich M74DM-0-58 propeller | | Issued | | 4/14/1977 |
SA4302NM (PAGE 1) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
SA437GL | | Installation of Tull microwave landing system airborne equipment. | | Issued | | 8/22/1980 |
SA449WE | | Pneumatic pitch assist PC-1 and optional installation altitude hold AH-1. | | Reissued | | 10/1/1973 |
SA450WE | | Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. | | Reissued | | 10/1/1973 |
SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
SA4762NM | | Installation of fiberglass wing tips. | | Issued | | 8/31/1989 |
SA4762NM | | Installation of fiberglass wing tips. | | Amended | | 8/1/1991 |
SA484CH | | Installation of instrument light dimmer system. | | Issued | | 3/7/1996 |
SA488WE | | Full flow aerofilter 30409A with element 1A0235. | | Issued | | 1/1/1960 |
SA496CH | | Installation of McCauley propeller model B3D36C429/82NPA-6. | | Reissued | | 2/8/2008 |
SA5108SW-D | | Installation of S-TEC System 60two axis automatic flight guidance system Model ST-064 with optional automatic electric trim system. | | Amended | | 4/13/1998 |
SA5127SW-D | | S-TEC System 60 Two Axis Automatic Flight Guidance System ST-124 with Optional Autotrim system. | | Amended | | 1/5/1998 |
SA5128SW-D | | S-TEC System 60 single axis automatic flight guidance system ST-063. | | Amended | | 4/9/1998 |
SA5130SW-D | | S-TEC System 60 Single Axis Automatic Flight Guidance System ST-123. | | Amended | | 1/15/1998 |
SA5142SW-D | | S-TEC System 60 pitch stabilization system ST-122 with optional automatic electric trim system. | | Reissued | | 3/15/1985 |
SA5147SW-D | | S-TEC System 60 pitch stabilization system ST-125 with optional automatic electric trim system. | | Amended | | 11/28/1984 |
SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
SA5246SW-D | | Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-215-40/50. | | Amended | | 10/24/1997 |
SA5254SW-D | | S-TEC System 40/50 single and two axis automatic flight guidance system ST-214-40/50. | | Amended | | 4/13/1998 |
SA5581SW | | Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. | | Amended | | 9/30/2002 |
SA560WE | | Flight control system B-4 including pitch assist PC-1 altitude hold AH-1 and navigational coupler NAV-1. | | Reissued | | 10/1/1973 |
SA562NE | | Installation of a Textron Lycoming O-320-D2B engine(150 h.p.) and a Sensenich model 74DM6-0-60 propeller. | | Issued | | 3/22/1988 |
SA563CH | | Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. | | Reissued | | 2/10/2009 |
SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
SA589WE | | Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. | | Reissued | | 10/5/1976 |
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 (4 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
SA597EA | | Installation of electronic voltage alarm Drawing No. 80106. | | Issued | | 1/1/1960 |
SA6078SW-D | | Installation of S-TEC system65 two axis automatic flight guidance system Model ST-371. | | Amended | | 4/17/1998 |
SA615EA (PAGE 1) | | Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. | | Reissued | | 7/6/2010 |
SA630WE | | Installation of oil filter assemblies. (NAVION A AND B with optional engine) | | Reissued | | 8/29/1974 |
SA662WE | | Hi-Lo sensitivity adaptor BI-400 and autopilot with NAV-1 navigation coupler and heading lock. | | Reissued | | 10/1/1973 |
SA664CE | | Installation of Hoskins MK1B Light System. | | Reissued | | 9/30/2011 |
SA693CE | | Replace existing engine induction air filter with AC Spark Plug filter. | | Reissued | | 6/20/2000 |
SA7152SW-D | | Installation of S-TEC manual electric trim system Model ST-410. | | Issued | | 5/29/1987 |
SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
SA798EA | | Installation of Monitair exhaust gas combustion monitor kit. | | Reissued | | 2/14/1972 |
SA800EA (PAGE 1) | | Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. | | Amended | | 7/6/2010 |
SA812WE | | BSA stability augmentation system. | | Reissued | | 10/1/1973 |
SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
SA8922SW | | Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) | | Issued | | 7/21/1994 |
SA917EA | | Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). | | Reissued | | 6/4/2007 |
SA920NW | | Installation of a spar repair | | Issued | | 4/1/1980 |
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 |
ST01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
ST01494LA (PG 1) | | 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 (1 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 |
ST02547AT (1 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |