TCDS A16WE

STCs approved under this data sheet · 2,302

Current certificates first, most recently changed first.

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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 = 'A16WE')
  ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number"

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STC SA5627NM-DInstallation of Galley Cart Controllers in accordance with United Air Lines, DAS-1-WE, Approved Drawing List No. 5627 dated December 9, 1991, or later approved revisions.United Airlines IncSTC SA5628NM-DInstallation of upgraded Digital Flight Data Acquisition Unit with new database software, in accordance with United Air Lines, DAS-1-WE, Approved Drawing List No. 5628 dated January 10, 1992, or later approved revisions.United Airlines IncSTC SA5632NM-DInstallation of Windshear/Ground Proximity Warning SystemUnited Airlines IncSTC SA5642NM-DReplace GTCP85-129 auxiliary power unit (APU) with GTCP85-129CK in UA 737-200 series aircraft.United Airlines IncSTC SA5910NM-DInstallation of Collins ACARS and VHF-3 system upgrade, and Bendix ACARS printer. (737-291)United Airlines IncSTC SA5987NM-DRemove the tourist class triple seat assemblies at the Type III overwing exits (LH and RH) and install inboard double seat assemblies in their place. The resulting interior arrangement will change from 8F/120Y to 8F/118Y. This installation is in accordance with United Air Lines, DAS-1-WE, Approved Drawing List No. 5987 dated January 11, 1994, or later FAA approved revisions.United Airlines IncSTC SA5988NM-DInstallation of upgraded Flight Data Acquisition unit as a replacement to existing installed unit. (737-322)United Airlines IncSTC SA5993NM-DInstallation of Collins ACARS, VHF-3 transceiver, and Bendix ACARS printer installation. (737-222)United Airlines IncSTC ST00283LA-DReconfiguration of interior arrangement per U. S. Technical Consultants Master Control List 2403-25-000, Revision NC, dated March 4, 1997. Master Control List 2403-25-000, Revision A, dated April 15, 1997. Master Control List 2403-25-000, Revision B, dated August 8, 1997, or later FAA approved revisions; and as revised by United Air Lines Master Document List No. 00283, Revision Original, dated August 23, 2003, or later FAA approved revisions.United Airlines IncSTC ST00549LA-DModifies existing Flight Data Acquisition Management System (FDAMS) Flight Recorder frame format database and replaces Oil Pressure indicatorsUnited Airlines IncSTC ST00550LA-DModifies the aircraft to install BE Aerospace -SPG First Class seats, and refurbished PTC seats in Economy Class. The installation is in accordance with DAS-1-WE Approved United Air Lines Document List No. 00550, dated October 6, 1998, or later FAA approved revisions.United Airlines IncSTC ST00553LA-DModifies the aircraft to install an AlliedSignal Flight Data Acquisition Unit, part number 965-0649-004, and status relay, installation of wiring from sensors and autopilot system to the FDAU, installation of wiring from the FDAU to the flight data recorder, installation of a circuit breaker for the new sensors, and re-routing of some existing wiring. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00553 dated August 17, 1999, or later FAA approved revisions.United Airlines IncSTC ST00563LA-DModifies the aircraft to install an AlliedSignal Enhanced Ground Proximity Warning System with imbedded Global Positioning System Card. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List 00563 dated February 9, 2000, or later FAA approved revisions. United Air Lines AFM Supplement dated February 9, 2000, to FAA Approved Flight Manual No. D6-8737-291A for 737-291 aircraft, or AFM Supplement dated May 19, 2000 to AFM No. D6-8737-4A1A or 737-2A1 aircraft, or later FAA approved revision to both Airplane Flight Manuals is required for this modification. In addition, accomplishment of Boeing Service Bulletin 737-53-1174, dated September 29, 1994, or later FAA approved revision is required for this modification.United Airlines IncSTC ST00564LA-DThe modification will remove one row (six seat places) of Burns TSO C-39b seats in the forward area of economy class on our B737-200 series aircraft. When removed, the forward five rows of economy seats aft of the class divider will be relocated, increasing the seat pitch from 31 to 35 inches. The final seat configuration count is 8F/95Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00564 dated January 26, 2000, or later FAA approved revisions.United Airlines IncSTC ST00566LA-DThe modification will remove one row (six seat places) of B/E Aerospace TSO C-39b seats in the forward area of economy class on our B737-200 series aircraft. When removed, the forward five rows of economy seats aft of the class divider will be relocated, increasing the seat pitch from 31 to 35 inches. The final seat configuration count will be 8F/95Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00566 dated January 30, 2000, or later FAA approved revisions.United Airlines IncSTC ST00568LA-DModifies the aircraft to remove B/E Aerospace seats in economy class. The modification changes the passenger capacity to 8F/96Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00568, dated February 7, 2000, or later FAA approved revisions.United Airlines IncSTC ST00569LA-DModifies the aircraft to remove Burns seats in economy class. The modification changes the passenger capacity to 8F/96Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00569 dated February 3, 2000, or later FAA approved revisions.United Airlines IncSTC ST00570LA-DModifies the aircraft to remove Weber seats in economy class. The modification changes the passenger capacity to 8F/96Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00570 dated February 3, 2000, or later FAA approved revisions.United Airlines IncSTC ST00571LA-DModifies the aircraft to remove one row (six seat places) of Weber TSO-C39b seats in the forward area of economy class on our Boeing 737-300 Series aircraft. With the removal of one seat row, six seat rows of Weber economy seats aft of the class divider will be increased in pitch from 31 to 35 inches. The seat row at the Type III exit and the row forward of the Type III exist will increase in pitch from 32 to 38 inches. The modification changes the passenger capacity to 8F/112Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00571 dated February 5, 2000, or later FAA approved revisions.United Airlines IncSTC ST00572LA-DModifies the aircraft to remove one row (six seat places) of B/E Aerospace TSO C-39b seats in the forward area of economy class on our B737-300 series aircraft. With the removal of one seat row, six seat rows of B/E Aerospace economy seats aft of the class divider will be increased in pitch from 31 to 35 inches. The seat row at the Type III exit and the row forward of the Type III exit will increase in pitch from 32 to 38 inches. The modification changes the passenger capacity to 8F/112Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00572 dated February 6, 200, or later FAA approved revisions.United Airlines IncSTC ST02976CH-DInstallation of a Cabin reconfiguration to a VIP cabin configuration in accordance with Standard Aero Master Data List 1020585, Revision (F), dated November 21, 2011 or later FAA approved revision.Diversified Aviation ServicesSTC ST03037CHInstallation of Supplemental Water Disinfection System P/N 9101-010000 in accordance with AeroControlex Installation Instructions report #90-0103 as listed on AeroControlex Master Drawing and Document List 90-0091, Rev. P, dated November 22, 2011, or later FAA approved revision.AeroControlex Group TransDigm IncSTC ST01182SEInstallation of a flight deck door in accordance with Duganair Technologies Inc., Index List, QS-00001-3A, Revision B, dated August 27, 2003, or later FAA approved revisions. FAA Approved Flight Manual Supplement No. QWC737101-4, Revision 1, dated December 16, 2004, or later FAA approved revision is required as part of this installation.Quiet Wing Technologies, Inc.STC ST00301LAInstallation of flush/fill line Nipple Valve Assembly P/N 062-0009-( ) {DL 0062-0009 Rev -, dtd 8/29/96 or later FAA Approved Revision}.Rockwell Collins Inc.STC ST00339LAInstallation of flush/fill line Lever Lock Cap Assembly P/N 0016-0034-2 {DL 0016-0034 Rev. C, dated October 11, 1996 or later FAA approved revision} in accordance with Service Bulletin No. 95-125-SB/9030-38-35 dated November 1, 1995 or later FAA approved revision.Rockwell Collins Inc.STC SA5749NMInstallation of a galley in accordance with Showa Aircraft Industry Co., LTD. Master Drawing List 60210-000000, Revision G, dated March 10, 1993, or later FAA-approved revisions.Showa Aircraft USA Inc.STC SA5951NMInstallation of two galleys, a stowage unit, and a curtain rail in accordance with Showa Aircraft Industry Co., LTD. Master Drawing List AER-93, Revision 3, dated April 22, 1993, or later FAA-approved revisions.Showa Aircraft USA Inc.STC ST11063SCReplacement of existing metal portable oxygen cylinders with new composite portable oxygen cylinder assembliesMagellan Services CompanySTC SA7420SWReplace existing Grimes P/N 60-4068-1 emergency power supply with Vista Manufacturing, Inc., emergency power supply Model 65-3, P/N 87-5106-3, in accordance with Vista Manufacturing, Inc., Drawing List 88-5100-3, Rev. A, Dated April 11, 1988, or later FAA Approved Revision.BF Goodrich AerospaceSTC SA7426SWReplace existing emergency power supply with Vista Airpak 65B-42 in accordance with Vista Manufacturing, Inc., Drawing List 87-5300, Rev. B, Dated May 5, 1988, or later FAA approved revision.BF Goodrich AerospaceSTC SA7427SWReplace existing Grimes P/N 60-1321-1 emergency power supply with Vista Model 65-2, P/N 87-5106-2 emergency power supply in accordance with Vista Manufacturing, Inc., Drawing List 88-5100-2, Rev. A, Dated April 11, 1988 or later FAA Approved Revision.BF Goodrich AerospaceSTC ST00979LAInstallation of Upper and Lower Red Anti-collision lighting in accordance with FAA Approved Master Drawing List, Drawing No. BFG-R-349-00, Revision "N/C" Dated November 12, 1999, or later FAA approved revision.BF Goodrich AerospaceSTC ST02003ATInstallation of BF Goodrich AFT Fixed Wingtip Halogen Navigation Position Light, P/N 5600(-2)BF Goodrich AerospaceSTC ST01715NY-DONE ONLY STC, S/N 34683: Installation of a Corporate Executive InteriorShangri-La Entertainment LLCSTC ST03932ATInstallation of a Lead Acid Battery as a replacement for the existing Nickel-Cadmium Battery in accordance with Concorde Master Drawing List (MDL) 5-0343, Rev. B, Dated May 09, 2011 or later FAA approved revision.Concorde Battery CorporationSTC ST00146BOInstallation of a Goodrich analog Transient Suppression Device (ATSD)Simmonds Precision Products IncSTC SA2126NMInstallation of a windscreen.AIM Aviation IncSTC SA2127NMInstallation of Galley No. 1 and Galley No. 4.AIM Aviation IncSTC SA2624NMInstallation of Stow-All overheard stowage compartment support structure, stowage compartments and sidewalls panel.AIM Aviation IncSTC SA2920NMInstallation of a Windscreen Assembly.AIM Aviation IncSTC SA3349NMInstallation of a Class Divider/ Curtain, Hatrack Configuration.AIM Aviation IncSTC SA3352NMInstallation of a Class Divider/Curtain and Stow-All ConfigurationAIM Aviation IncSTC SA3699NMInstallation of a class divider.AIM Aviation IncSTC SA4023NMInstallation of a mid-cabin closet.AIM Aviation IncSTC SA5936NMInstallation of 3 galleys.AIM Aviation IncSTC SA781NWInstallation of a coat closet.AIM Aviation IncSTC SA884NWInstallation of windscreens.AIM Aviation IncSTC ST00028SEInstallation of a closet.AIM Aviation IncSTC ST00029SEInstallation of a class divider.AIM Aviation IncSTC ST02142LAInterior Modifications in accordance with BaySys Technologies, LLC Master Data List 8119-MDL, Revision D, dated June 19, 2008, or later FAA approved revision.Interad Limited LLC
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