TCDS 1A17

STCs approved under this data sheet · 259

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 = '1A17')
  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 SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)Precise Flight Inc.STC ST238CHInstallation of BFGoodrich TCAS I.Acron Aviation Inc.STC ST01930LAInstallation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI)Sandel Avionics LLCSTC SA2-931Installation of Sperry SP-40 Gyropilot.Honeywell International IncSTC SA1732GLInstall air ambulance conversion.Spectrum Aeromed LLC dba Spectrum AeromedSTC SA571SWInstallation of Collins radio altimeter system.Associated Air Center, Inc. - c/o CT Corporation SystemSTC ST00425WIInstallation of Keddeg Company P/N 21BC120 Coalescer Assembly as a replacement for P/N 83237-14 on Gulfstream G-159 AirplanesPurolator Facet, IncSTC ST02628LAInstallation of Honeywell CAS-67A Traffic Alert Collision Avoidance System (TCAS II) with Dual Honeywell MST-67A Transponder System and removal of L-3 TRC-497 Skywatch TCAS systemBattelle Memorial Institute, Pacific Northwest DivisionSTC SA1536SWInstallation of Foxtronics TRAMM BTI-600 nickel cadmium battery temperature system and an optional generator voltage control systemFoxCart GSE, LLCSTC SA2016NMInstallation of a de-icing system on the Rolls Royce P/N RK29954A engine inlet cowlROBERT W. MURRAYSTC SA302WEIncorporate a de-icing system (as manufactured by applicant) externally on Rotol propeller spinner as an alternate to Dowty Rotol internal elements. If applied to original spinner, Montgomery Systems Tech., Inc. P/N 72196-2 will apply. If applied to a new aluminum nose spinner P/N 72196-1 will apply. Dowty Rotol Service Bulletin Section 61-170 pages 1 and 2 outlines a revised spinner de-icing system. This is a Napier external system. Approval of the A.R.B. is indicated. (Continued on page 3)ROBERT W. MURRAYSTC SA122CEInstall Hoskins supplementary light system consisting of colored Model A(or clear or colored Model E) wing tip lights, a Model C or 2 tail light, and optionally, two of Model 2 fuselage lights with M-3 or M-5 power supply.BF Goodrich AerospaceSTC SA3687SW: Installation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing List G1-1000, Revision C, Dated December 02, 1986 or later FAA approved revisionBF Goodrich AerospaceSTC ST00682WI-DModification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions.Rockwell Collins IncSTC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)Electronics International Inc.STC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.Electronics International Inc.STC ST02540AT-DInstallation of replacement fuel tank sealant systemFFC ManufacturingSTC SA1681GLInstallation of Chrysler Pentastar Aviation auxiliary generator adapter assembly.Phoenix Air Group IncSTC SA1699GLInstallation of electrical system.Phoenix Air Group IncSTC SA1610SOInstallation of a composite custom executive interior.Page AvJet CorpSTC SA1612SOInstallation of the Collins FCS-80 flight control system.Page AvJet CorpSTC SA1704SOInstallation of a single Global GNS-500A series 3B VLF/Omega Navigation System.Page AvJet CorpSTC SA2072SOInstallation of 24-passenger interior.Page AvJet CorpSTC SA2079SOInstallation of emergency lighting system.Page AvJet CorpSTC SA2080SOInstallation of a Fairchild A100A cockpit voice recorder.Page AvJet CorpSTC SA3154SOInstallation of an interior.Page AvJet CorpSTC ST01483WI-DInstallation of Cabin Re-configuration.Duncan Aviation IncSTC SA888EAInstallation of Grimes three light strobe kit 34-0303-1 as supplemental lighting.Honeywell International Inc.STC ST00844WI-DModification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter.Rockwell Collins IncSTC ST03055ATInstallation of either a Single or Dual Sandel Model 3400 TAWS with RMI System.Phoenix Air Group IncSTC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.Electronics InternationalSTC SA2893SWInstallation of one, two, or three- place side facing seat attached to seat tracks.Aviation Fabricators IncSTC ST00743NY-DInstallation of AlliedSignal GTCP36-150J Auxillary Power Unit.Phoenix Air Group IncSTC SA1181EAInstallation of Garrett AiResearch GTCP36-100(H) APU.PATS Aircraft LLCSTC SA1204EAInstallation of Solar T-62T-40C2 APU.PATS Aircraft LLCSTC SA1222EAReplacement of bleed-air driven fan with electrically powered fan.PATS Aircraft LLCSTC SA3304NMInstallation of monorail sun visor system in accordance with FAA approved Rosen Product Development, Inc., Drawing List RG-I-II-00DL, Revision N/C, or later FAA approved revision.Rosen Sunvisor Systems LLCSTC ST01676CHInstallation of a Honeywell/AlliedSignal CAS-81 TCAS II Traffic Alert and Collision Avoidance System.Flight Systems Engineering, IncSTC ST01605CHInstallation of an Allied Signal CAS-67A TCAS II Traffic Alert and Collision Avoidance System in accordance with Pro-Tech Avionics Corporation Master Drawing List Document No. 81-328L001, Revision E, dated December 6, 2001, or later FAA approved revision.Phoenix Air Group IncSTC SA1373GLInstallation of Norton Radome Kit No. 4772W.Saint-Gobain Performance Plastics CorpSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.STC SA2-1020Interior arrangement in the cabin from Station 133 to 525.Signature Flight Support CorporationSTC SA2-910Installation of electronic and interior equipment.Signature Flight Support CorporationSTC SA2899SWInstallation of hostess jump seat and table.Signature Flight Support CorporationSTC SA2900SWInstallation of toilet and outside toilet service.Signature Flight Support CorporationSTC SA1202SWModification to aircraft electrical power system.Rockwell Collins IncSTC SA1514SWInstallation of following dual Collins equipment: 618M-2D VHF transceivers, 51RV-2B VHF NAV receivers, 621A-3 transponders; installation of the following single equipment: Collins 346D-1B Paging Amplifier, Collins DN101/NC103 Doppler, Collins 860F-1 DME; IDC 519-227022 Encoding Alimeter; IDC 22719-101 Vertical Speed Indicator, and Dayton Aircraft Products EB-28CD Emergency Locator TransmitterRockwell Collins IncSTC SA1745SWInstallation of ANS-70A Area Navigation System.Rockwell Collins IncSTC SA1852SWInstallation of dual FD-109 flight director/AP-105 autopilot, 54W-1C comparator, dual ALT-50 radio altimeter, dual MC-103 compasses, dual ILS-70/Bendix RVA33A VOR/ILS, 51Z-4 marker, dual 860E-3 DME, dual DF-203 ADF, 621A-6 transponder, 621A-3 transponder, dual 346B-3 audio system, AVQ-10 radar, and IDC air data system.Rockwell Collins IncSTC SA815SWInstallation of Collins VOR antenna type 837B-1 on vertical fin.Rockwell Collins Inc
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