TCDS 3A15

STCs approved under this data sheet · 999

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 = '3A15')
  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.

STC SA3459SW-DInstallation of Century automatic flight system Model AK964.Century Flight Systems IncSTC SA02149AKInstallation of GX50/60 GPS Navigator, Capstone configured MX20 Multi-Function Display and UAT transceiver.Garmin International IncSTC SA00331BOInstallation of Avidyne Corporation AutopilotAvidyne CorporationSTC SA1916WEInstallation of Brittain Model NAV-2B Flight Control System.Brittain Industries, IncSTC SA2030WEInstallation of Brittain B-VII, NAV-2B, B2C and BSA-4 Flight Control Systems.Brittain Industries, IncSTC SA1379WEInstallation of Brittain Industries Model B-4A Flight Control SystemBrittain Industries, IncSTC SA1530WEInstallation of Brittain Model B-4AP Flight Control System.Brittain Industries, IncSTC SA1558WEInstallation of Brittain Industries Model B-5P flight control system.Brittain Industries, IncSTC SA1711WEInstallation of Brittain Industries B-5P Flight Control System.Brittain Industries, IncSTC SA1762WEInstallation of Brittain Industries Models B-5, NAV-2B and B2C Flight Control Systems.Brittain Industries, IncSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.J P InstrumentsSTC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemJ P InstrumentsSTC SA02387AKFabrication and installation of the LSI Exterior LED Lightning SuiteASTRONICS - LSISTC SA2660SWInstallation of Continental IO-470-N engineD'Shannon Products Ltd.STC SA5527SWInstallation of Continental IO-470-C, or IO-470-N and either a McCauley 2A36C23/84B-0, 2A37C223/90RB-6, 3A34C423/90DFA-10, or 3A36C434/80VEA-0; Beech 278-100-11/278-214-82, or 278-100-13/278-214-82; Flottorp F12A-3/8400-2; or Hartzell PHC-I3YF-1RF/F8468A-6R PropellerD'Shannon Products Ltd.STC SA5635SWInstallation of Continental IO-470-N engine and Hartzell PHC-L3YF-IRF/F8468A-6R or McCauley 2A37C223/90RB-6, 3A34C423/90DFA-10, 3A36C434/80VEA-0 propellersD'Shannon Products Ltd.STC SA09254SCIncrease in maximum takeoff and landing gross weight by 100lbs. when equipped with vortex generators per STC SA09074SC.D'Shannon Products Ltd.STC SA01671WIInstallation of interior configurationsMillennium Concepts IncSTC 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 9-17-10D'Shannon Products Ltd.STC SA09074SCInstallation of vortex generators on wing upper surface and vertical stabilizerD'Shannon Products Ltd.STC SA1476WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemBrittain Industries, IncSTC SA289CHInstallation of Inline Pneumatic Air Filter, P/N CV1J4Aerotech Components IncSTC SA02460CHInstall Genesis Aero, LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanksD'Shannon Products Ltd.STC SA02461CHInstall Genesis Aero, LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanksD'Shannon Products Ltd.STC SA2633WEInstallation of enlarged window and baggage compartment.D'Shannon Products Ltd.STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsAerospace Logic Inc.STC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplayGarmin International IncSTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemLatitude Technologies CorporationSTC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemGarmin International IncSTC SA5655NMInstallation of rdesigned rudder hinge brackets.D'Shannon Products Ltd.STC SA5721NMInstallation of replacement cockpit control knobs for throttle, mixture, propeller,parking brake, heater, cowl flaps.D'Shannon Products Ltd.STC SA5156NMFabrication and installation of Pulsar-MOSFET Landing Light Flasher SystemAvTekSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverGarmin International IncSTC SA00281BOInstallation 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 700-00165-000Avidyne CorporationSTC SA02434NYInstallation of a Digital Engine Monitoring system.Ultra Electronics Flightline SystemsSTC SA2373CEInstallation of B&D Instruments & Avionics, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 0535-003-008, Rev. B, or later FAA Approved revision; and (2) copy of this certificate.Teledyne ControlsSTC SA1416CEInstallation of flap and aileron fairings and seals.D'Shannon Products Ltd.STC SA1417CEInstallation of elevator tail cone fairings per Smith Speed Conversions Drawing List No. 1001 stamped FAA Approved on May 17, 1978, or later.D'Shannon Products Ltd.STC SA1448CEInstallation of elevator tail cone fairings per Smith Speed Conversions Drawing List No. 1003 stamped FAA Approved on October 6, 1978, or later.D'Shannon Products Ltd.STC SA1550CEInstallation of elevator and ruder tail cone fairingsD'Shannon Products Ltd.STC SA1585CEInstallation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.D'Shannon Products Ltd.STC SA1649CEInstallation of either the tail safe support angles or a stub spar at the 3% chord station on the root rib of horizontal stabilizer.D'Shannon Products Ltd.STC SA1734CEInstallation of alternate Ram Air System for engine induction and sealed cowling.D'Shannon Products Ltd.STC SA2087CEExtended baggage compartment installation, per Mike Smith Aero Drawing 36-1012-1, Rev. A, dated January 7, 1985, and stamped FAA Approved on February 6, 1985, or later.D'Shannon Products Ltd.STC SA2149CERemove V tail and install a Beech Model F33A straight tail per Mike Smith Drawing List Number 35-1013, stamped FAA Approved with a date of October 24, 1985, or later. The aircraft are also identified as Models S35TC, V35ST, V35AST, and V35BST by Mike Smith Aero, Inc., with nameplate installed adjacent to the existing nameplate.D'Shannon Products Ltd.STC SA02723CHInstall D Shannon Products, Ltd. 20-gallon fiberglass auxiliary wing-tip fuel tanks DLB1400, Rev. B dated May 14, 2009, in accordance with Installation Manual KB-1401-1, Rev. A, dated May 14, 2009, or later FAA Approved revision for 4010-lb gross weight normal category operation.D'Shannon Products Ltd.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.Superior Panel TechnologySTC 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.D'Shannon Products Ltd.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.D'Shannon Products Ltd.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.D'Shannon Products Ltd.
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