TCDS 3A25

STCs approved under this data sheet · 389

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 = '3A25')
  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 SA02366AT-DInstallation of replacement fuel cell assembliesFFC ManufacturingSTC SA02634AT-DInstallation of fuel cell modifications consistentFFC ManufacturingSTC SA593CHInstall Champion SlickSTART magneto booster system.Champion Aerospace LLCSTC SA7063NMInstallation of acrylic window liners in accordance with FAA approved Drawing Lists. Drawing lists are listed on FAA approved Model List Number SA7063NM, or later FAA approved revision.G & D Aero Products Inc.STC SA09574SC-DInstallation of RAM Series VII 335 horsepower (hp) series, increase takeoff weight to 6,390 pounds, andincrease landing weight to 6,075 pounds.RAM Aircraft Limited PartnershipSTC SA09971SC-DInstallation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellersRAM Aircraft Limited PartnershipSTC SA8981SW-DInstallation of McCauley 3AF32C515/82NLA-4.0 propellers on Cessna 340 and 340ARAM Aircraft Limited PartnershipSTC SA8604SW-DIncrease maximum takeoff weight to 6390 pounds and maximum landing weight to 6075 pounds.RAM Aircraft Limited PartnershipSTC SA8055SW-DInstallation of intercooler scoop.RAM Aircraft Limited PartnershipSTC SA7365SW-DInstallation of TCM TSIO-520N or NB engines. Installation of Hartzell PHC-C3YF-2UF/FC7663DB-2Q propellers, McCauley 3AF32C93/82NC-6.0, or McCauley 3AF32C505/82NEA-6.0 propellers.RAM Aircraft Limited PartnershipSTC SA7382SW-DInstallation of TCM TSIO-520N or NB engines (modified by STC SE3714SW). Increase takeoff weight to 6140 pounds; landing weight remains at 5975 pounds. Installation of McCauley 3AF32C93/82NC-6.0, or McCauley 3AF32C505/82NEA-6.0 propellers.RAM Aircraft Limited PartnershipSTC SA5796SW-DInstallation of Alcor Tru-Flow indicating system, or SDI Hoskins fuel flow indicating system, or Silver Instruments Fueltron fuel flow indicating system.RAM Aircraft Limited PartnershipSTC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.M-20 Oil Separators LLCSTC SA02546NYInstallation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1090-1Lord CorporationSTC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeGarmin AT Inc.STC SA7975SW-DOption 1: Install Vortex Generators on vertical stabilizer in accordance with RAM Drawing No. 1474 Rev. B. dated March 4, 1991 or later FAA approved revision. Option 2: Same as Option 1, except no change in airspeeds; Supplemental Flight Manual not required. Option 3: Install vortex generators on vertical stabilizer and wing topRAM Aircraft, Limited PartnershipSTC SA02510NYInstallation of a 4-blade MT-Propeller Model MTV-14-D-C-F/CF188-30g propellersMT- Propeller Entwicklung GmbHSTC SA2346SW-DOption 1: Install Teledyne Continental Motors Model TSIO-520-J engines (310 horsepower). Option 2: Install Teledyne Continental Motors Model TSIO-520-N or NB engines (310 horsepower) and McCauley or Hartzell propellers. Option 3: Install Teledyne Continental Motors Model TSIO-520-NB engines modified by Supplemental Type Certificate number SE4327SW (325 horsepower) and McCauley or Hartzell propellersRAM Aircraft Limited PartnershipSTC SA02503NYBattery Relocation.North West Geomatics Ltd.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemPrecise Flight IncSTC SA03527ATInstallation of an Avidyne EXP5000 Primary Flight Display (PFD)Star AviationSTC SA01205WI-DInstallation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.Honeywell International IncSTC SA01105WI-DInstallation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).Honeywell International Inc.STC SA568EAInstallation of Grimes Manufacturing Company three light strobe kit P/N 34-0107-1.Honeywell International Inc.STC SA02378NYONE ONLY - Installation of a Remote Sensing Equipment Port S/N 340A0533North West Geomatics Ltd.STC SA20GLInstallation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO)Ontic Engineering and Manufacturing Inc.STC SA250CEInstallation of Woodward electronic propeller synchraphaser system.Ontic Engineering and Manufacturing Inc.STC SA01420WIInstallation of Garmin GNS 430A / 530A COMM/NAV/GPS Systems. Data required: (1) Scandinavian Avionics Design GmbH Drawing List 2027438-DL-02, Issue 2; or later EASA approved revisions. (2) Scandinavian Avionics Design GmbH Approved Aircraft Flight Manual Supplement, Doc. 2027438-AM-02A, Issue 1, and Doc. 2027438-AM-02B, Issue 2, both approved by EASA under approval No. EASA.A.S.01389 dated 07-09-2005, or later EASA approved revision.Scandinavian Avionics Design GmbHSTC SA01284WIInstallation of MT-Propeller Model MTV-14-D-C-F/CF188-30g hydraulic 4-blade variable pitch propeller.MT- Propeller Entwicklung GmbHSTC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.K S Avionics IncSTC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.K S Avionics IncSTC SA01695SEInstallation of an antennaGarmin AT Inc.STC SA1078GLInstallation of Great Lakes windshield P/N W-2070, W/T-2070 or WK-2070.Great Lakes Aero Products IncSTC SA446CEInstallation of 30 gallon auxiliary fuel tank in baggage compartment.Eaglejet Aviation Inc.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.Insight Instrument CorporationSTC SA00729SEInstallation 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.J P InstrumentsSTC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.Garmin AT Inc.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.Electronics InternationalSTC SA1-620Kit No. 2014X for 12-inch RCA AVQ-45, AVQ-47, AVQ-50, AVQ-55 and 12-inch Collins WP-103 radar antenna.Saint-Gobain Performance Plastics CorpSTC SA272EAInstallation of Chamberlain 2014K-B radome kit as follows: Kit No. 2014K-B for Bendix RDR-100 or RDR-110 radar systems with 12-inch antenna and transmitter receiver unit.Saint-Gobain Performance Plastics CorpSTC SA914EAInstallation of Radome kit P/N4057KX.Saint-Gobain Performance Plastics CorpSTC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.Aero Enhancements Inc.STC SA3522NMInstallation of Precise flight series 400 speedbrake system.Precise Flight IncSTC SA5137NMInstallation of sun visor.Rosen Sunvisor Systems LLCSTC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.Avidyne CorporationSTC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.Electronics International Inc.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.Garmin AT Inc.STC SA02217AKInstallation 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.Garmin AT Inc.STC SA00556DEInstallation of a left-hand exhaust stack assembly.Heliarc Welding Service Inc.STC SA01436SECockpit sunvisor retrofit kit.Rosen Sunvisor Systems LLC
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