Supplemental type certificates

49,117 STCs, most recently changed first. Search by what an STC changes, its holder or a model.

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duckdb -csv -c "SELECT stc_number, description, holder, status, status_date
  FROM 'https://openairdocs.org/data/latest/faa_stc.parquet'
  ORDER BY status_date DESC NULLS LAST, stc_number"

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STC SA5781NMInstallation of Model 3140-51630.5 gallon wing fuel tanks.F Atlee Dodge Aircraft Service · Jan 9, 2004STC SR01362SEInstallation of the support assembly for the ground handling wheel on the skid tube of the above model rotorcraftMicro AeroDynamics Inc · Jan 9, 2004STC ST00192BORevised mid-cabin seating limitation. Limited to installation on serial number 9067 only.Learjet Inc. · Jan 9, 2004STC ST01706NYInterior Completion Modification. Limited to installation on BD-700-1A10, serial number 9114 ONLY.Bombardier Completion Center Inc · Jan 9, 2004STC ST01927CHInstallation of an ELTA ADT 406 AF/AP Emergency Locator Transmitter (ELT) System.EAD Inc. · Jan 9, 2004STC SA531NEInstallation of a Simmonds Precision total fuel/Vref dual indicator, P/N 393080-203 thru -223. Must be installed concurrently with STC SA520NE.Simmonds Precision Products Inc · Jan 8, 2004STC ST00040BOInstallation of BFGoodrich No. 20191 remote fuel height measurement sticks.BF Goodrich Aerospace · Jan 8, 2004STC ST01332NY-DInstallation of a cabin interior 3-place divan. Limited to installation on model 900EX, serial number 006 ONLY.Dassault Falcon Jet - Wilmington Corp · Jan 8, 2004STC ST01257LA-DInstallation of an Airshow 400 System. Limited to installation on Learjet 45 (Learjet 40), serial numbers 45-2001 through 45-4000.Learjet Inc. · Jan 7, 2004STC SA01852NYInstallation of a Communicator System. Limited to installation on serial number UE-227.Northeast Engr & Dev Ltd · Jan 6, 2004STC SA867NEInstallation of lower wing front spar cap reinforcement kit. (C90A S/N LJ-1063 THUR LJ-1087 EXCEPT LJ-1085)SK Aircraft Company Inc · Jan 6, 2004STC ST00187BOInstallation of a revised Mid Cabin Bulkhead. Limited to installation on model BD-700-1A10, serial number 9064 ONLY.Learjet Inc. · Jan 5, 2004STC ST02210AKInstallation of the Spectrum Aeromed Ambulance Module System 5300-002.LMM Inc · Dec 31, 2003STC ST09483AC-DInstallation of Scientic Power Distribution System.FAA Aviation System Standards AVN-300 · Dec 31, 2003STC ST09626SCInstallation of a single Honeywell Laseref IV Inertial Reference System (IRS).Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09629SCInstallation of an Artex ELT (110-406 NAV) Emergency Locator Transmitter System with a NAV interface unit.Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09748SCInstallation of a second 77 cubic-foot oxygen bottle in nose radome area, above existing bottle.Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09837SCInstallation of Collins ADC-87 No. 2.Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09847SCInstallation of an AlliedSignal digital flight data recorder (DFDR).Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09848SCInstallation of side-facing divan certified for take-off and landing use.Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09941SCInstallation of BFGoodrich Stormscope WX-1000E Weather Mapping System.Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09953SCInstallation of B/E Aerospace, Aircraft Modular Products Forward/Rearward Facing Single Seat.Gulfstream Aerospace Corporation · Dec 31, 2003STC ST09954SCInstallation of an Oxygen Filler Panel with Pressure Gauge.Gulfstream Aerospace Corporation · Dec 31, 2003STC SA00189BOInstallation of landing gear axles (P/N 1441003-1).Aero LLC · Dec 30, 2003STC SA00977CHReplacement of certain BFGoodrich pneumatic deicer boots.SMR Technologies Inc · Dec 30, 2003STC ST10202SCInstallation of Honeywell Mark VII EGPWS Computer & Collins WXA-1000 weather radar adapter.Frederick A. Whitson P.E. · Dec 30, 2003STC ST10211SCInstallation of Dual Collins Air Data Computer (ADC) for Reduced Vertical Separation Minimums (RVSM) Operational Capability.Frederick A. Whitson P.E. · Dec 30, 2003STC SA00364LARetirement life extension of de Havilland DHC-6-300 wing in accordance with FAA approved Structural Integrity Engineering Master Drawing List SIE-23-900, Revision B, dated April 7, 1997, or later FAA approved revision.Structural Integrity Engineering · Dec 29, 2003STC SA5053NMInstallation of acrylic window liners in accordance with FAA approved Gale R. Calhoon Report No. 3, no revision, dated September 1, 1990, or later FAA approved revision.G & D Aero Products Inc. · Dec 29, 2003STC 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 Engineering · Dec 29, 2003STC SA6073NMInstallation of fatigue sensor and structural life extension of wing spar in accordance with FAA approved SIE Master Drawing List 91000, Revision A, dated September 23, 1993, or later FAA approved revision, and FAA approved Airplane Flight Manual Supplement Report No. SIE-12-601, Revision N/C, dated October 19, 1993 or later FAA approved Airplane Flight Manual Supplement, and Report No. SIE-12-602, Revision N/C, dated December 21, 1993, or later FAA approved Revision. (SIE-12-601 is for model C99 only, and SIE-12-602 is for the remaining models, 99, 99A, A99A, and B99.)Structural Integrity Engineering · Dec 29, 2003STC ST00633ATApproval of maximum zero fuel weight increase from 138,000 pounds to 146,000 pounds. (727-200 SERIES S/N 19483, 19484, 19486, 19491, 20180, 20184, 20185, 20187, 20995, 20996, 19480, 19492, 19481, 19482, 19485, 20191 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST00671ATApproval of maximum landing weight increase from 160,000 pounds to 164,000 pounds. (727-200 SERIES S/N 21930 AND 21931 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST00719ATApproval of increased operating weights as substantiated by the design data listed in Structural Integrity Engineering (SIE) Master Report List or Master Document List No. SIE-28-703, no revision, dated February 24, 1995, or later FAA approved revision. Aircraft with Increase of Maximum Takeoff or Landing Weight must also be modified in accordance with: Drawing SIE-28-901 (taxi weight up to 183,000 lb, landing weight to 164,000 lb), 28-904 (taxi weight up to 178, 500 lbs, landing weight to 164,000 lbs), 28-905 (taxi weight up to 191,000 lb, landing weight to 164,000 lbs), Rev NC or later FAA approved revisions.Structural Integrity Engineering · Dec 29, 2003STC ST00720ATApproval of maximum zero fuel weight and maximum landing weight (Flaps 30) increases to 157,500 pounds and 166,000 pounds, respectively. (727-200 SERIES S/N 22080 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST00778LAInstallation of splitter locks and floor modifications to increase the main deck cargo floor capacity.Structural Integrity Engineering · Dec 29, 2003STC ST00779LAInstallation of side vertical restraints in accordance with approved Master Drawing List SIE 37-703, Revision A, dated May 25, 1999, or later FAA approved revisions. Structural Integrity Engineering FAA Approved Airplane Flight Manual Supplement, SIE 37-607 dated May 26, 1999, or later FAA approved revisions and Weight and Balance Supplement, SIE 37-608, dated February 9, 1999, or later FAA approved revisions, are required as part of this modification.Structural Integrity Engineering · Dec 29, 2003STC ST00782ATApproval of maximum zero fuel weight increase to 132,000 pounds. (727-100 SERIES S/N 19183 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST00901ATApproval of increased operating weights as substantiated by the design data listed in SIE-28-902. (727-200 S/N 21269, 21245 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST00926ATApproval of increased operating weights as substantiated by the design data listed in SIE No. SIE-28-713. (727-200 S/N'S 21085, 20997 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST00949ATApproval of increased operating weights as substantiated by the design data listed in SIE Master Report List SIE-28-717. (727-200 SERIES S/N 21161 ONLY)Structural Integrity Engineering · Dec 29, 2003STC ST01013ATApproval of increased operating weights. Limited to installation on serial numbers 21327, 21328, 21329, 21330, and 21331 ONLY.Structural Integrity Engineering · Dec 29, 2003STC ST01181LAInstallation of modifications to the 9-G rigid barrier, cargo door surround structure and other attendant modifications.Structural Integrity Engineering · Dec 29, 2003STC ST00181WI-DInstallation of a Magnastar C-2000 Digital Airborne telephone.Learjet Inc · Dec 27, 2003STC ST09701SC-DLimited to serial number 333 ONLY.Dassault Falcon Jet · Dec 26, 2003STC SR09172RCInstallation of a replacement main rotor blade without a leading edge abrasion strip, part number 500P2100-BSC and BS-1 per Helicopter Technology Company (HTC) Maintenance Manual HTCM-001 latest FAA approved revision.Helicopter Technology Co · Dec 24, 2003STC ST10037SC-DS/N 075 ONLY: Installation of an executive cabin interior.Gulfstream Aerospace Corporation · Dec 24, 2003STC SA00523SEReplacement of certain BF Goodrich pneumatic deicer boots.SMR Technologies · Dec 23, 2003STC SR01848NYIncrease in maximum takeoff weight from 2850 Kg to 3000 Kg.Agusta Aerospace Corporation · Dec 23, 2003STC ST00519DEInstallation to upgrade the existing VHF analog data link system to a VHF Digital Data Link (VDL) Mode 2 system.Rockwell Collins Inc · Dec 23, 2003