TCDS A-777
STCs approved under this data sheet · 470
Current certificates first, most recently changed first.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = 'A-777') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = 'A-777') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
STC SA02930NYInstallation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) InstrumentsSTC SA10682SCInstallation of alternator and voltage regulatorSTC SA10921SCInstallation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulatorsSTC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02283SE PAGE 2Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA3531NMInstalling copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP)STC SA02121SEInstallation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic SystemSTC SA01110CHInstallation of wing fuel tank quick valve drains.STC SA999WEInstallation of a Jasco #6540-1 (35a.) Alternator Kit or Jasco #6555-1 (50a.) Alternator KitSTC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleSTC SA00789LAInstallation of Clear View Sunvisor.STC SA02015SE-DInstallation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.STC SA04165CHInstallation of an Enhanced Exhaust System, D Shannon Products, Ltd. kit DSP-KIT-15-009STC SA1150WEInstallation of Brittain Industries, Inc. Installation Modification Kit #11977 (relocation of gyro sense element to remote position)STC SA269WEInstallation of Brittain/Beech Pneumatic Pitch Assist Model PC-1STC SA322WEInstallation of Brittain/Beech Pneumatic Pitch Assist M del PC-1STC SA323WEInstallation of Beech Pneumatic Pitch Assist Model PC-1STC SA4-1260Installation of Brittain/Beechcraft AutopilotSTC SA4-716Installed Brittain/Beech Autopilot in accordance with Brittain Industries, Inc. Installation Manual 11905-1 (Aileron only) or Brittain/Beech AutopilotSTC SA662WEInstallation of Brittain Industries, Inc., Model B1-400 Hi-Lo Sensitivity AdaptorSTC SA533WEInstallation of Brittain/Beech Model B4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold, and NAV-1 Navigational CouplerSTC SA631WEInstallation of Brittain/Beech Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold, and NAV-1 Navigational CouplerSTC SA677WEInstallation of Brittain/Beech Model B-4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.STC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemSTC SA2361SWInstallation of Continental IO-470-N engine and McCauley 2A36C23/84B-0, or 2A37C223/90RB-6, or Beech 278-100-11/278-214-82, or 278-100-13/278-214-82, or Flottorp F12A-3/8400-2 propellerSTC SA1493WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemSTC SA153EAInstall Beryl D Shannon Aviation Specialties, Inc. 15-gallon Tip Tanks B1400-01, -02, Rev. B, dated 8-15-78* or D Shannon Products, Ltd. 20-gallon Tip Tanks Part List DLB1400, Rev. E, dated 9-17-10STC SA1476WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemSTC SA02460CHInstall Genesis Aero, LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanksSTC SA2633WEInstallation of enlarged window and baggage compartment.STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplaySTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemSTC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemSTC SA5721NMInstallation of replacement cockpit control knobs for throttle, mixture, propeller,parking brake, heater, cowl flaps.STC SA5156NMFabrication and installation of Pulsar-MOSFET Landing Light Flasher SystemSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverSTC SA02434NYInstallation of a Digital Engine Monitoring system.STC SA2375CEInstallation of B&D Instruments & Avionics, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 0535-003-011, Rev. B, or later FAA Approved revision; and (2) copy of this certificate.STC SA09337SCAn increase gross weight of 100lbs for Beech models A35, B35, C35, D35, E35, F35, G35, and 35R when equipped with Vortex Generators per J.V.E., Inc., STC SA09145SC.STC SA1584CEInstallation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.STC SA1650CEInstallation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8, 1981, or later.STC SA1703CEInstallation of flap and aileron fairings and seals.STC ST01494LAInstallation 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.STC SA1-368Installation of auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company s Manual SFE-35(III) dated July 15, 1959, Tip Tank Installation, Type III Kit, utilizing parts listed on Bamber Wing Tanks Type III Kit Contents dated July 15, 1959.
This wing tip tank installation may be used in combination with either the wing auxiliary tanks or a baggage auxiliary tank, but not when both are installed. Complete installed weight empty is 23.7 lb. at 89.1 inches. The CG of the tip fuel is 87.0 inches.STC SA1-460: Installation of auxiliary wing tip fuel tanks in accordance with Drawing Number RB1-001B and Installation Instructions number RB-1, Revision of April 1, 1960.
This wing tip tank installation is acceptable with either the baggage auxiliary tanks, or the wing auxiliary tanks. However, it is not acceptable with both auxiliary installations incorporated simultaneously.STC SA144EAApproval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing Solenoid Fuel System (ref STC SAl-303 dated February 20, 1959). No wing or baggage compartment auxiliary tanks are permitted with this system. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. D dated February 15, 1964 is required.STC SA181EAApproval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing tip fuel tanks (ref STC SA3OEA, Configuration 2 or 3) and Type II or III Kit transfer fuel system. This system eligible with Beech 20 gal wing aux. tanks or baggage compartment tanks, but not both. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. C dated February 15, 1964 is required.
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