TCDS 4A25

STCs approved under this data sheet · 587

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 = '4A25')
  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 SA2498NMInstallation of dual AiResearch GTCP85-98CK(D) Auxiliary Power Units (APU) in the forward baggage compartment.Airweld Inc.STC SA4118WEInstallation of a Winters Airtair in the aft passenger entry door.Airweld Inc.STC SA4119WEInstallation of a Winters Air Stairs in the forward passenger entry door.Airweld Inc.STC SA4225WEInstallation of 1 or 2 AiResearch GTCP85-98CK auxiliary power units in forward baggage compartment.Airweld IncSTC SA5454NMInstallation of a ground auxiliary air conditioning system.Airweld IncSTC SA1730WEInstallation of cockpit voice recorder, seat lights, passenger service outlets, communication panel relocation, galley wiring changes, flight data recorder and vertical accelerometer, pitot tube with heater circuit, marker beacon.Flying Tiger Line IncSTC SA1731WEInstall single Decca Model 72 doppler radar (ground speed and drift angle only).Flying Tiger Line IncSTC SA1738WEModification of interior arrangement to 221 passenger Military Airlift Command configuration.Flying Tiger Line IncSTC SA1909WEModification of interior arrangement to provide automatic folding attendant seats at the four jet escape exits.Flying Tiger Line IncSTC SA1987WEInstallation of Edo Model 144 ADF-Loran antenna splitter.Flying Tiger Line IncSTC SA2017WEInstallation of Decca Model 72 doppler radar (ground speed and drift meter only).Flying Tiger Line IncSTC SA2018WEInstallation of Decca Model ADL-21 Loran.Flying Tiger Line IncSTC SA2113WEInstallation of two Decca Type 05 Omnitrac 2B Doppler/Loran navigation computer systems with pictorial displays.Flying Tiger Line IncSTC SA2247WEInstallation of Lockheed Aircraft Services Company Model 250-A weight and balance computer system.Flying Tiger Line IncSTC SA2313WEInstallation of Kollsman 'Slim Pac' altitude alerting system.Flying Tiger Line IncSTC SA2314WERevised seating arrangement to 244 passenger all tourist configuration.Flying Tiger Line IncSTC SA2427WEInstallation of a third attitude indicator.Flying Tiger Line IncSTC SA2465WEInstallation of dual Delco Carousel IV inertial navigation system.Flying Tiger Line IncSTC SA2604WEInstallation of Custom Products passenger type seat and flight crew glare protection curtain.Flying Tiger Line IncSTC SA2632WEModification of airplane to provide attitude information from INS in lieu of two vertical gyros (this modification pertains only to aircraft previously modified by STC SA2465WE).Flying Tiger Line IncSTC SA2957WEInstallation of separate differential oil pressure system and associated warning light indication.Flying Tiger Line IncSTC SA3949NMInstallation of a Fairchild Model 800 Digital Flight Data Recorder.Flying Tiger Line IncSTC ST127CHInstallation of strobe upper anticollision light, P/N 30-1585-1.Honeywell International Inc.STC ST01738CHInstallation of a Honeywell Traffic Alert and Collision Avoidance System (TCAS II).Canard Aerospace CorporationSTC ST01707SEONE-ONLY: Non-Group aircraft approval for Reduced Vertical Separation Minimum (RVSM), S/N 45811AeroMech IncorporatedSTC ST10503SCInstallation of a Universal Avionics Systems Corporation EFI-600 Flat Panel Electronic Flight Instrument systemAvionics & Systems Integration GroupSTC 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 ST00171LA-DModifications for combi configuration fire protection.Air Transport LLCSTC ST01073LARequirements for establishing group approval basis for Reduced Vertical Separation Minimum (RVSM) are contained in AeroMech Document No. AMI-QD-DC8-0006 dtd 9/15/00 or later approved FAA revisions.AeroMech IncorporatedSTC ST00525WI-DModification of Collins 618M-4 VHF COMM Receiver Transmitter Installation to a 618M-5 VHF COMM Receiver Transmitter installation with either a Gables G7406-02 or Avtech 7522-1-2 VHF COMM Receiver Transmitter Control Series using with Collins Installation Instructions as listed on AML No. ST00525WI-D, or later FAA approved revisions.Rockwell Collins IncSTC ST01861LAModifications to the 9-G rigid barrier, cargo door surround structure and other attendant modifications.Structural Integrity EngineeringSTC ST01307WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installationRockwell Collins IncSTC SA1471NMInstallation of a galley/closetHeath Tecna Inc.STC SA3144NMInstallation of overhead storage compartments, ceiling and wall linings, and normal and emergency lightsHeath Tecna Inc.STC SA750NWInstallation of Mark I interior retrofit kit.Heath Tecna Inc.STC ST10268SCInstallation of a Universal Avionics Terrain Awareness Warning System (TAWS) in accordance with Aircraft Systems and Manufacturing Top Drawing List 5643-0001-00 A, dated July 20, 2004, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document No. 5643-2160-00, Revision IR, dated July 22, 2004 is required.Aircraft Systems & MfgSTC SA523NEInstallation of two Turbomach (solar) T-62T-40C gas turbine auxiliary powerplants. Limited to installation on serial number 45881 ONLY.PATS Aircraft LLCSTC SA918NEInstallation of fresh waster system. Limited to installation on DC-8-62, serial number 46071 ONLY.PATS Aircraft LLCSTC ST01791CHInstall reinforced flightdeck door and venting system as defined in Drawing List FDS-DL16 latest FAA approved revision per Cockpit Door System Installation Manual FDS-16 latest FAA approved revisions.National Aircraft Service IncSTC SA5510NMModification in accordance with FAA approved SIE Drawing List 9000 N/C,, dated August 7, 1991, or later FAA approved revisions, to permit an increased maximum zero fuel weight (MZFW), and maximum landing weight (MLW) of DC-8-61 airplanes.Structural Integrity EngineeringSTC ST01181LAInstallation of modifications to the 9-G rigid barrier, cargo door surround structure and other attendant modifications.Structural Integrity EngineeringSTC ST09247SCInstallation of dual Universal UNS-1D FMS/GPS navigation systems.Aircraft Systems & MfgSTC SA5971NMInstallation of flame reistant cargo covers.Air Transport International LLC.STC ST01163CHInstallation of an AlliedSignal CAS67A traffic alert and collision avoidance system (TCAS II).EAD Inc.STC SA2811SOInstallation of an air to ground public telephone communication system (Seatfone).GTE Airfone IncorporatedSTC SA2405NMInstallation of Dual Collins EFIS-85A Electronic Flight Instruments. Applies only to serial number 46084.CAMMACORPSTC SA4892NMModification of the aircraft by installation of noise reduction nacelles.Topeka Management Inc.STC SA5455NMModification of the aircraft by installation of noise reduction nacelles.Topeka Management Inc.STC SA3437NMModification to permit an increase in maximum allowable zero fuel weight of DC-8-62 airplanes, (1) which are certified to a 335,000 lbs. maximum takeoff gross weight or (2) which are certified to a 350,000 lbs. maximum takeoff gross weight.Leth & AssociatesSTC SA5848NMInstallation of Nordskog oven/hot cup moduleB/E Aerospace Inc.
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