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 |
SA00026WI | | New nose wheel spacer. | | Issued | | 2/9/1993 |
SA00035SE | | Installation of wing front lower spar cap replacement and reinforcement kit. | | Issued | | 11/11/1993 |
SA00042WI | | Installation of a nacelle mounted electrical fuel boost pump system. | | Issued | | 3/4/1993 |
SA00047DE | | Installation of copilot left front passenger right front passenger bulb windows. (S/N 3083) | | Reissued | | 6/21/2012 |
SA00051WI | | New nose landing gear scissor fitting. | | Issued | | 3/26/1993 |
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 |
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 |
SA00105SE | | Modify Flap Pulleys. | | Reissued | | 6/17/1999 |
SA00111WI | | New main landing gear scissor fittings. | | Issued | | 10/28/1993 |
SA00148WI | | Installation of T.K.S. Ice Protection System | | Issued | | 4/4/1994 |
SA00161BO (2 OF 3 | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 0:00 |
SA00169SE | | Install Lycoming IO-540-M1C5 engine and Hartzell HC-C3YR-2UF/FC8468()-6R propeller. | | Amended | | 6/2/2000 |
SA00243BO (3 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 (2 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 |
SA00333NY | | Installation of alternator system. (S/N 500A-1141-61) | | Issued | | 5/16/1995 |
SA00387SE | | Modification of the existing fuel system to increase its capacity by the installation of additional fuel tanks and associated hardware | | Issued | | 11/12/1996 |
SA00529SE | | Modification inspection and repair of the wing to fuselage attachment straps wing leading edge close outs and wing station 24.0 ribs. | | Amended | | 11/17/1998 |
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 |
SA00729SE | | Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. | | Amended | | 11/30/2005 |
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 |
SA00794CH | | Replace Twin Commander fuel cap assembly with Shaw Aero Devices Fuel Cap (P/N 416-50) and adapter (P/N 416-938). | | Amended | | 8/10/2009 |
SA00804SE | | Installation of an engine failure indicator system also referred to as a low Thrust Detector system. | | Amended | | 7/16/2000 |
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 |
SA00874WI | | Installation of elevator and rudder trim actuator. | | Issued | | 4/18/2000 |
SA00944CH | | Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) | | Amended | | 6/20/2000 |
SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
SA01105SE | | Installation of two (2) Hartzell Model HC-B3Z20-2A/10151(B)-8(R) or two (2) HC-93Z20-2C/10151(B)-8(R) propellers on the above model aircraft per James Metzger | | Amended | | 6/24/2004 |
SA01142SE | | Installation of the Merlyn Products Inc. Model 290 or 300 Turbocharger system | | Amended | | 9/24/2012 |
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 |
SA01212SE | | Manufacture of Merlyn 320 Turbo Twin Commander Conversion Kit | | Amended | | 7/2/2013 |
SA01222SE | | Modification of the existing fuel system to increase its capacity | | Amended | | 5/20/2008 |
SA01229SE Page 2 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
SA01240SE (1 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
SA01314WI | | Replace the original equipment oil temperature oil pressure and fuel pressure 3-in-1 gauges and dual cylinder head temperature gauge with oil temperature oil pressure and cylinder head temperature 3-in-1 gauges and dual fuel pressure gauge. | | Issued | | 4/1/2005 |
SA01384CH | | Installation of various de-icer harnesses. | | Issued | | 1/30/2001 |
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 |
SA01444AT | | Installation of an Enviro Systems AirConditioner. | | Amended | | 6/10/1999 |
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 |
SA01660CH | | Remove Janitrol P/N C15C54 or Twin Commander P/N 88035-5 combustion heater and install C & D Associates Model CD35K heater kit 10 P/N 12043K10. | | Issued | | 6/24/2002 |
SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
SA01677AT | | Installation of Electrosystems 90 Amp Alternators. | | Amended | | 1/25/1999 |
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 2) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
SA01754SE | | Installation of the Merlyn Products Inc. remote oil filter | | Issued | | 4/19/2007 |
SA01787AT | | Installation of Brake and Rudder pedal extension. | | Issued | | 1/15/1999 |
SA01788AT | | Installation of Windshield sunscreens for pilot and copilot. | | Issued | | 1/15/1999 |
SA01789AT | | Installation of pilot and copilot frameless vent windows. | | Issued | | 1/15/1999 |
SA01790AT | | Installation of Split Engine Bowl. | | Issued | | 1/15/1999 |
SA01791AT | | Installation of Tinted Passenger Windows. | | Issued | | 1/15/1999 |
SA01792SE | | Installation of the Hartzell HC-C3YR-2UF/FC8468(A)(B K)-6R propeller and the Hartzell C-3258 (P) spinner assembly | | Issued | | 9/25/2007 |
SA01800SE (PG 4) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
SA01820AT | | Installation of Exhaust Deflectors. | | Issued | | 2/19/1999 |
SA01828SE | | Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System | | Reissued | | 5/12/2011 |
SA01841SE | | Installation of Teledyne Continental engines modified. | | Issued | | 5/12/2008 |
SA01861SE (PAGE 3) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
SA01861SE (PAGE 5) | | 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 (5 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
SA01956AT-D | | Installation of replacement fuel cell assemblies | | Reissued | | 5/5/2009 |
SA01988SE (PAGE 4) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
SA02005NY | | Installation of SMR Technologies pneumatic deicer models. | | Amended | | 2/3/2006 |
SA02013CH | | Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). | | Amended | | 5/2/2011 |
SA02013SE | | Modification of the fuel system structures and engine installation | | Issued | | 7/27/2009 |
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 5) | | 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 |
SA02110CH (PAGE 4) | | 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 |
SA02153LA-D (Page 2) | | Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System | | Amended | | 12/16/2013 |
SA02154AK (PAGE 2) | | Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. | | Amended | | 1/12/2005 0:00 |
SA02203AK (PAGE 2) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
SA02212AK (PG 4) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. | | Amended | | 5/4/2011 |
SA02217AK (3 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 |
SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
SA02268CH (PAGE 5) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
SA02268CH (PAGE 6) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
SA02293AK (2 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
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 |
SA02655AT (2 OF 2) | | Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. | | Amended | | 9/1/2004 0:00 |
SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
SA02738CH (PAGE 3) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
SA09162AC-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-634-40/50. | | Amended | | 9/6/1996 |
SA09164AC-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-528. | | Issued | | 8/8/1996 |
SA09165AC-D | | Installation of S-TEC yaw damper system Model ST-529. | | Issued | | 9/18/1996 |
SA09530AC-D | | Installation of S-TEC System 55X Two-Axis Automatic Flight Guidance System Model ST-904. Eligibility limited to model 500S serial number 01755 through 03305. Also eligible when modified per STC SA585SW (extended nose). | | Issued | | 9/20/2002 |
SA1-142 | | Modified ARC A13-B antenna. | | Issued | | |
SA1-143 | | Installation of Chamberlain 2001X series radome kits. | | Reissued | | 7/6/2005 |
SA1-342 | | Oil-free vacuum pump. | | Issued | | |
SA1-385 | | Installation of BFGoodrich lightweight reservoir type pneumatic de-icing system. | | Reissued | | 3/1/1996 |
SA1-445 | | ARC Type A13-B VHF navigational antenna on vertical fin. | | Amended | | |
SA1-455 | | ANC-3A computer and ANC-C2 or ANC-D2 controller in conjunction with Lear L2C autopilot. | | Amended | | |
SA1-520 | | Electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
SA1-525 | | ARC A13-B antenna on vertical fin with rotating beacon. | | Amended | | |
SA1-541 | | Electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
SA1-555 | | ANC-3A computer and ANC-C2 or ANC-D2 controller. | | Amended | | 1/1/1960 |
SA1-606 | | Installation of electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
SA1-607 | | Electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
SA1-624 | | Oxygen system. | | Amended | | 1/1/1960 |
SA1-64 | | Federal F-400 autopilot. | | Issued | | 1/1/1960 |
SA1-652 | | Dry vacuum pump and instrument vacuum system. | | Issued | | 1/1/1960 |
SA1-92 | | Fuselage to accommodate aerial photographic equipment. | | Issued | | 1/1/1961 |
SA1-93 | | RCA AVQ-50 radar equipment and AVQ-50 antenna mounting bracket. | | Issued | | 1/1/1961 |
SA1007NW | | Installation of a low thrust detector system. | | Reissued | | 3/6/1998 |
SA1017EA | | Installation of vertical tail floodlights. (680-F INCLUDES PRESSURIZED VERSIONS) | | Amended | | 10/29/1984 |
SA101GL | | Installation of Collins AP-107 autopilot. | | Reissued | | 2/11/1976 |
SA10236SC (3 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
SA102EA | | Pump type pneumatic deicing system. | | Reissued | | 3/1/1996 |
SA1064SW | | Wild RC-8 aerial survey camera. | | Issued | | 8/8/1969 |
SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
SA1072SW | | Universal camera. | | Issued | | 1/1/1961 |
SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
SA111RM | | Modify exhaust stacks by installing straight slip joint. | | Issued | | 3/27/1978 |
SA1122SW | | Dual cameras and navigation sights. | | Issued | | 1/1/1961 |
SA1125SW | | Aerial survey camera and navigation. | | Issued | | 3/2/1970 |
SA1135SW | | Modification of fuselage for installation of Bendix ANA-12 doppler antenna. | | Issued | | 3/30/1970 |
SA1138SW | | Fiberglass tail cone. | | Issued | | 4/8/1970 |
SA114CE | | Windshield anti-ice system. | | Issued | | 1/1/1960 |
SA1158GL | | Replace standard wing tip assembly with winglet tip assembly. | | Reissued | | 9/13/1999 |
SA115EA | | Pump type pneumatic deicing system. | | Reissued | | 3/1/1996 |
SA1182SW | | Dual camera and navigation sight. | | Issued | | 8/19/1970 |
SA118CE | | Installation of a Woodward propeller unfeathering system. | | Reissued | | 3/20/1992 |
SA120CE | | Windshield anti-ice system. | | Issued | | 1/1/1960 |
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 |
SA132EA | | Install electrothermal propeller deicing system. | | Reissued | | 3/1/1996 |
SA1332SW | | Modify fuselage for camera and navigation sight. | | Issued | | 6/24/1971 |
SA133CE | | Installation of windshield wiper. | | Reissued | | 1/31/1997 |
SA1359GL | | Install winglet wingtips. | | Reissued | | 9/13/1999 |
SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
SA136SO | | Installation of Turbosupercharged GO-480-D1A engines. | | Reissued | | 6/26/2006 |
SA137CE | | Lower window line in cabin area. | | Issued | | 1/1/1960 |
SA1393SW | | Mitchell automatic flight system FD/AP282-353 consisting of flight director/autopilot with automatic command trim system. | | Reissued | | 7/10/1984 |
SA1394SW | | Mitchell automatic flight system Model AK353 consisting of Century III autopilot with optional auto- matic/command trim radio coupler glide slope coupler. | | Reissued | | 7/10/1984 |
SA13WE | | M-4 autopilot. | | Amended | | 2/24/1967 |
SA1445SW | | Modification of Mitchell automatic flight system AK221 installed per STC SA680SW. | | Reissued | | 7/13/2012 |
SA1454WE | | Installation of Brittain Model B-4A flight control system. | | Issued | | 1/1/1960 |
SA1457GL | | Installation of a Cleveland nose wheel. | | Issued | | 3/15/1990 |
SA1566GL | | Installation of flap gap wing fairings. | | Reissued | | 9/13/1999 |
SA1580WE | | Installation of Brittain Model B-5 flight control system. | | Issued | | 1/1/1960 |
SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
SA1629CE | | Installation of Avcon stretcher. | | Reissued | | 8/21/1990 |
SA1662SW | | Installation of outboard fuel system. | | Reissued | | 9/4/1992 |
SA166WE | | Removal of main cabin door and hinge pins. | | Issued | | 1/1/1960 |
SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
SA1686WE | | Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. | | Amended | | 10/17/2002 |
SA168CE | | Twin engine synchronizer. | | Reissued | | 4/30/2007 |
SA1847WE | | Installation of Brittain Up-Command Signal Adapter Kit. | | Reissued | | 10/20/1972 |
SA1904WE | | Installation of Vibration Isolation Products (VIP) engine mount P/N VIP-50804-10 on various aircraft as shown on FAA Approved Model List (AML) No. SA1904WE. | | Amended | | 10/17/2002 |
SA193SO | | Installation of turbocharged Lycoming GO-480-C1B6 or GO-480-G1B6 engines per STC SE124SO. | | Reissued | | 6/26/2006 |
SA1966WE | | Removal of main cabin door. (Mr. Biljanic contacted AFS-610 1/16/97. Said he is no longer in the business and wishes this STC to revert to public domain. Contact FAA s office in Long Beach for further info) | | Issued | | 1/1/1960 |
SA1971WE | | Installation of Model ARB-3 Automatic Downed Aircraft Marker( ADAM ). | | Amended | | 11/21/1969 |
SA199SW | | Four auxiliary fuel cells in each outer wing panel between wing stations 127 and 163. | | Issued | | 1/1/1960 |
SA2-22 | | Install 2 each 3/8 O.D. lines from LH nacelle to RH firewall. | | Reissued | | 8/31/2000 |
SA2-26 | | Installed 3/8 O.D. line from RH propeller governor pad on RH engine to LH propeller pad on LH engine. | | Reissued | | 8/31/2000 |
SA2-318 | | Installation of Goodyear brake 9530303 and related equipment. | | Reissued | | 8/31/2000 |
SA2-67 | | Install Eclipse Pioneer fuel flow indicating system. | | Reissued | | 8/31/2000 |
SA2-75 | | Revised and installed new electrical components. | | Reissued | | 8/31/2000 |
SA2-89 | | Installation of Lycoming GO-480-C1D6 engines and Hartzell HC 83X20-2C/8833-2 propellers. | | Reissued | | 8/31/2000 |
SA20GL | | Installation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO) | | Reissued | | 4/30/2007 |
SA2113CE | | Installation of single Gill G-24724-volt battery as a replacement for original dual 12-volt batteries. | | Amended | | 11/17/1987 |
SA2114CE | | Installation of Electro Delta VR300-28-50 Central Air Charter VR-0015 or Central Air Charter GR2850VI voltage regulator as a replacement for original Delco Remy 1119656 voltage regulator. | | Amended | | 9/2/1988 |
SA2186CE | | Install passenger compartment cargo restraint system and baggage compartment cargo restraint system. | | Amended | | 7/16/1990 |
SA2240CE | | Replacement of dual 50-amp generator system with dual 50-amp Prestolite alternator system. | | Issued | | 3/30/1987 |
SA2279WE | | Removal of main cabin door. | | Issued | | 11/23/1970 |
SA2303CE | | Install cargo restraint and cargo provisions. | | Issued | | 11/10/1987 |
SA2478SW | | Installation of Lycoming IO-720- B1B engine and increase take-off and landing weight to 7800 lbs. | | Reissued | | 4/16/2008 |
SA250CE | | Installation of Woodward electronic propeller synchraphaser system. | | Reissued | | 4/30/2007 |
SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
SA256WE | | Control wheel replacement. | | Issued | | 1/1/1960 |
SA2573CE | | Install wing and tail leading edge anti-icing shoes. | | Amended | | 5/7/1992 |
SA257CE | | Installation of turbocharged Lycoming engines Model IO-540-A1A5 with Hartzell HC-A3VK-2/V7636D propellers. | | Reissued | | 7/3/2006 |
SA2586NM (PAGE 3) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
SA258SW | | Camera and camera view finder opening in main cabin floor of 30-inch x 39-inch maximum dimension. | | Issued | | 6/5/1970 |
SA2604CE | | Install passenger compartment and baggage compartment cargo restraint system. | | Issued | | 4/5/1990 |
SA260SW | | Installation of a Protective Device in the ground side of the Battery and External Power relays | | Reissued | | 11/12/2009 |
SA2624CE | | Installation of GR2850V1 voltage regulator. | | Issued | | 5/23/1990 |
SA265EA | | Installation of Chamberlain radome kit #2001K-B for use with Bendix radar RDR-100 or RDR-110. | | Amended | | 3/11/1970 |
SA2691WE | | Installation of Lycoming IO-720-B1B or | | Reissued | | 4/16/2008 |
SA2796CE | | Limit maximum weight to 6000 pounds. Data required: (1) FAA approved Airplane Fliht Manual Supplement dated February 20 1992 or later FAA approved revision. (2) Placard on the pilot s instrument panel near the top center of hte panel stating Airplane Maxium Weight - 6000 Pounds. | | Issued | | 2/20/1992 |
SA2826SW | | Installation of auxiliary fuel tank according to Report No. MDL 60700 Master Drawing List revised 7/27/78 or later FAA approved revision.
);INSERT INTO stc_table VALUES ( | | Reissued | | 12/30/2004 |
SA2827CE | | Installation of an aircraft voice recorder. | | Issued | | 4/29/1992 |
SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
SA2903SW | | Installation of wing flap gap seals. | | Amended | | 2/7/1995 |
SA29SW | | Auxiliary outboard fuel tank. | | Amended | | 4/23/2002 |
SA3-118 | | Installation of A.R.C. type A-13B navigational antenna. | | Reissued | | 6/22/1983 |
SA3-259 | | Collins glide slope VOR navigation and VHF communications antenna Aircraft Radio Corp. ADF antenna and Grimes rotating beacons. | | Issued | | 1/1/1960 |
SA3-406 | | Installation of AVQ-50 radar. | | Reissued | | 5/27/1983 |
SA3-525 | | 37R-2 antenna. | | Issued | | 1/1/1960 |
SA3-721 | | Cabin temperature control system with Janitrol S-25 heater. | | Issued | | 1/1/1960 |
SA300CE | | Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) | | Amended | | 5/14/1992 |
SA303GL | | Install Cleveland conversion kit No. 199-74 on models which use MIL-H-5606 brake fluid (red oil) or install conversion kit No. 199-74A on models which use Skydrol brake fluid (nonpetroleum base). | | Reissued | | 10/28/1980 |
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 |
SA30CE | | 210405 governor. | | Issued | | 1/1/1960 |
SA3142SW-D | | Mitchell automatic flight system AK600 consisting of Century IV autopilot or Model AK600FD consisting of Century IV flight director autopilot with optional remote annunciator. | | Reissued | | 6/6/1984 |
SA3143SW-D | | Installation of Century automatic flight system. | | Amended | | 9/12/1997 |
SA315SO | | Nose weather radar and radome. | | Issued | | 1/1/1960 |
SA321EA | | Install wheels P/N 301174 P/N s2-993 and/or 2-1107. | | Reissued | | 9/4/1974 |
SA3335NM | | Cockpit Sun Visor installation in accordance with FAA approved Rosen Drawing List Number RAC-00DL dated January 7 1986 or later FAA approved revision. | | Reissued | | 3/24/2003 |
SA3392SW-D | | Mitchell automatic flight system AK890 consisting of Century IIB autopilot. | | Reissued | | 8/24/1983 |
SA340SO | | Continental IO-520E engines and Hartzell 3-bladed propellers. | | Issued | | 1/1/1960 |
SA3476WE | | Replacement installation of tail cone assembly. | | Reissued | | 12/7/1988 |
SA3492WE | | Replacement installation of vertical tip assembly. | | Amended | | 2/7/1995 |
SA3516WE | | Installation of cockpit overhead windows. | | Amended | | 2/7/1995 |
SA366SO | | Gross weight increased to 6530 pounds. | | Reissued | | 2/10/2011 |
SA3867WE | | Installation of Model CFS-2000 -2001 or FT-200 fuel indicating system. | | Reissued | | 1/30/1998 |
SA38CE | | B21043 governor. | | Issued | | 1/1/1960 |
SA396SW | | Automatic pilot AK118 lateral guidance radio coupler AK123 and pitch trim AD135. | | Issued | | 1/1/1960 |
SA4-1234 | | Installation of electrical low fuel warning device to indicate last 25 gallons of useable fuel in main (center) tank. | | Reissued | | 3/10/2009 |
SA4-1309 | | L-2C autopilot. | | Issued | | 1/1/1960 |
SA4-1382 | | L2-C autopilot. | | Issued | | 1/1/1960 |
SA4-1414 | | Autopilot. | | Reissued | | 10/1/1973 |
SA4-1442 | | Installation of collins AF-102 Autopilot. | | Reissued | | 11/18/1999 |
SA4-1579 | | Aerofilter 30690B full flow lube oil filter with element 1A0286. | | Issued | | 1/1/1960 |
SA4-1655 | | Outer wing non-icing fuel tank vent fairings. | | Issued | | 1/1/1960 |
SA4-443 | | Fiberglas wing tips. | | Reissued | | 11/4/1970 |
SA4-447 | | Fiberglass wing tips. | | Reissued | | 11/4/1970 |
SA4-454 | | Installation of fiberglass vertical stabilizer cap in lieu of metal repositioning of rotating beacon mounting to leading edge reduction of length of the two spar extensions to facilitate VHF antenna installation inside stabilizer cap area. | | Reissued | | 11/4/1970 |
SA4-455 | | Hamilton Standard governors IM12-G5. | | Issued | | 1/1/1960 |
SA4-777 | | Aerofilter 30409A-12 or full flow filter 30409A with element 1A0235. | | Issued | | 1/1/1960 |
SA4-904 | | Installation of mufflers and modification of carburetor heat system. | | Reissued | | 11/4/1970 |
SA4-989 | | Aerofiter 30690B full flow lube oil filter with element 1A0286. | | Issued | | 1/1/1960 |
SA404CE | | Installation of Hoskins supplemental position light system which includes Model A wing tip lights and Model D or K(dual) tail light. | | Reissued | | 9/30/2011 |
SA4219WE | | Installation of DTL-1000 -1001 and/or -1002/3 autopilot adapters for the Edo-Aire Mitchell Century III autopilot. | | Issued | | 9/2/1980 |
SA4321NM | | Installation of an oil filter filter base and mounting plate on the firewalls of those airplanes listed on AML No SA4321NM that are equipped with an FAA approved Continental model IO-470 engine installation which has been modified by the installation of an external mounted full flow oil adapter and spin-on oil filter | | Reissued | | 7/30/1993 |
SA4325WE | | Installation of aft fuselage ballast. | | Issued | | 4/21/1981 |
SA447SO | | Installation of Bendix Model FCS810 flight control system including manual electric trim and flight director indicator DH 841( ). | | Amended | | 6/17/1976 |
SA454SW | | Installation of windshield alcohol system. | | Reissued | | 9/4/1992 |
SA458EA | | Installation of nose cap radome kit No. 3066X-R. | | Amended | | 4/1/1983 |
SA459EA | | Conversion to Model 500B. | | Issued | | 1/1/1960 |
SA476WE | | Nacelle mounted fuel booster pump. | | Reissued | | 11/4/1970 |
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 |
SA491EA | | Incorporation of B.F. Goodrich ice protection systems. | | Reissued | | 3/1/1996 |
SA50CE | | C210310 governor. | | Issued | | 1/1/1960 |
SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
SA51CE | | C210403 governor. | | Issued | | 1/1/1960 |
SA527EA | | Installation of Collier Model 1AC internally mounted ADF sense antenna. | | Amended | | 11/21/1968 |
SA529WE | | Installation of turbosupercharged Lycoming IO-540 series engines. | | Reissued | | 4/16/2008 |
SA559SW | | Installation of an RMK-A-15/23 aerial survey camera. | | Reissued | | 5/9/2012 |
SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
SA584WE | | Installation of oil filter assemblies. | | Reissued | | 8/29/1974 |
SA585SW | | Installation of Nose Cone. | | Reissued | | 12/7/1988 |
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 |
SA5969NM | | Installation of Lycoming TIO-540- J2B(d) engine Hartzell HC-C3YR-2UF/FC8468D-6R or HC-C4YR-2/ FC6660 propeller and optional Merlyn Products MPI 98-1005-519 turbocharger. | | Amended | | 12/13/1996 |
SA599SO | | Installation of camera opening in fuselage and reinstall seats. | | Reissued | | 1/17/1992 |
SA610NE | | Installation of Safeway deicer boot. | | Amended | | 1/31/1991 |
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 |
SA666SW | | Forward cabin door installation. | | Reissued | | 4/14/2006 |
SA66GL | | Install Collins AP-106 autopilot consisting of Collins 913K-1 two each 334C-9 (662-0964-001 -002) 334C-6 (622-0965-002) 590A-6 614E-1 339T-1 161H-1 590B-3 and 390B-18 units. | | Reissued | | 2/11/1976 |
SA680SW | | Installation of Mitchell automatic flight system model AK221 consisting of Century III autopilot with optional automatic pitch trim radio coupler and glide slope coupler. | | Reissued | | 6/25/1984 |
SA683WE | | Installation of turbocharged Continental IO-470-M engines in accordance with FAA Sealed Roto- Master (Rajay) Drawing List No. RJ2050 or later FAA approved revision. | | Reissued | | 7/3/2006 |
SA688NE | | Installation of Safeway Model 6900 deicer boot. | | Amended | | 1/31/1991 |
SA706GL | | Install Cleveland conversion kit P/N 199-122 (for aircraft using MIL-H05606 brake fluid) or199-122A (for aircraft using Skydrol brake fluid). | | Amended | | 4/28/1988 |
SA70CE | | Federal F-500 automatic pilot. | | Issued | | 1/1/1960 |
SA7164SW-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-101. | | Reissued | | 11/8/1989 |
SA7174SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-102 with optional autotrim system. | | Reissued | | 3/30/1990 |
SA7183SW-D | | Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System Model ST-103. | | Issued | | 8/1/1988 |
SA7186SW-D | | Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-104-40/50. | | Reissued | | 7/1/1991 |
SA7187SW-D | | Installation of S-TEC Manual Electric Trim System Model ST-129. | | Amended | | 6/26/1995 |
SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
SA7224SW-D | | Installation of S-TEC system 60 pitch stabilization system Model ST-326. | | Issued | | 7/23/1990 |
SA798EA | | Installation of Monitair exhaust gas combustion monitor kit. | | Reissued | | 2/14/1972 |
SA798SW | | Radome nose extension. | | Reissued | | 3/8/2000 |
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 |
SA802SW | | Bendix M4-B/C autopilot flight control system. | | Issued | | 1/1/1960 |
SA812NW | | Modification consists of moving the mounting of the roll-servo from fuselage station 71.0 to 180.5 and moving the mounting of the pitch servo from station 85.40 to station 233 | | Issued | | 7/25/1979 |
SA838SW | | Installation of Mitchell glide slope coupler Model 1C493. | | Reissued | | 6/29/1984 |
SA8453SW | | Replace the o-ring seals in the landing gear lower strut. | | Reissued | | 2/26/2007 |
SA8475SW | | Installation of a paralleling relay P/N EQ2500. | | Reissued | | 5/12/1998 |
SA84SW | | Automatic pilot. | | Issued | | 1/1/1960 |
SA854EA | | Installation of Radome Kit No. 4022KX. | | Amended | | 12/16/1976 |
SA8597SW | | Installation of P/N DF062-507 upper center fuel tank bladder cells as a replacement for original bladder P/N 5630062-507. | | Reissued | | 7/31/2002 |
SA863SW | | Modified instrument panel. | | Reissued | | 2/14/1975 |
SA8705SW | | Installation of R25V0N Alternator Control Unit or R2510N Alternator Control Unit or V2510A Over Voltage Sensor. | | Amended | | 6/21/1996 |
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 |
SA90CE | | Installation of Hoskins Supple- mental Model A or B high intensity wing tip lights Model C tail light with or without Models 1 or 2 high intensity fuselage lights. | | Reissued | | 9/30/2011 |
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 |
SA92EA | | Install wheels P/N s 3-1112 and/or311-58 and P/N s 2-878 and/or2-971 and/or 2-1087. | | Reissued | | 9/4/1974 |
SA973SW | | Auxiliary outboard wing tanks. | | Issued | | 1/1/1960 |
SE01840AT | | Installation of Naceele Mounted Recognition Lights. | | Reissued | | 1/18/2000 |
SR02088SE | | Installation of Hartzell PHC-C3YF-2UF/FC8468D( )-8R propellers and C-3567-4P spinners | | Issued | | 9/8/2010 |
ST01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
ST01468CH | | Installation of various SMR Technologies electrical propeller deicer models. | | Amended | | 7/25/2006 |
ST02547AT (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |