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"
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
STC SA00670SEReplacement of certain Goodrich pneumatic deicer boots in accordance with SMR Technologies, Inc. Installation Instructions as listed on AML No. SA00670SE.STC ST02252NYInstallation of Artex ELT C406-N with a Navigation Interface in accordance with Aero Consulting Services Ltd. Modification Data Summary (MDS) Report Number E618000, Revision D; dated September 09, 2010; or later Transport Canada approved revision.STC ST02679NYReplacement of Water Tank Installation to be completed in accordance with Aero Consulting Services Ltd. Modification Data Summary F250000, Revision D; dated July 02, 2010; or later Transport Canada approved revision.STC ST02877NYAft Cabin Bulkhead Replacement Installation in accordance with Field Aviation Ltd. Modification Data Summary Number MDL-25150000 Revision IR; dated July 15 2010; or later Transport Canada approved revision.STC SB02931CHONE ONLY STC, SN 6616: Replace the Cameron Balloons US burner, and fuel tanks with Thunder and Colt Stratus Triple Burner; Cameron Balloons US 15 gallon fuel tanks, part number CB2901; and 20 gallon fuel tanks, part numbers CBUS1060 and CB2903 via standard burner frame gimbal block and tank straps.STC ST02887CH-DInstallation of Universal Avionics Systems Corporation (UASC) EFI-890r Electronic Flight Display SystemSTC ST01095CH-DInstallation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). Installed per ElectroSonics Drawing ES1329-205075-01, Rev. 2, dated 09-20-00 or later FAA approved revision.STC ST02343LAModification of existing Type Certified Thales Avionics TopSeries In-flight Entertainment (IFE) System in accordance with FAA Approved Thales Avionics Index List, Drawing No. 254112, Revision "B", dated February 01, 2011, or later FAA approved revision.
The Instructions For Continued Airworthiness is called out in its associated Master Drawing Lists (MDL) defined in the above referenced Index List.STC ST03908ATRelocation of the Captain's and First Officer's Oxygen Mask Assemblies from the just forward and outboard of each pilot's position in the P13 and P14 crew sidewall panels respectively, to adjacent to the aft edge of the P13 and P14 crew sidewall panels per Avionic Support Group (ASG) Master Data List (MDL) 210126-MDL, Revision C, dated December 23, 2010, or later Atlanta ACO approved revision.STC ST11042SCInstallation of a Sandel SA4550 Electronic Attitude Display Indicator and a Bendix Vertical Gyro for the copilot use with the existing FGS-70 Flight Director and Autopilot. Airplane Flight Manual Supplement, document number JTECH-FGS70-0102, revision IR, dated February 10, 2011, or later approved FAA revision, is required.STC SA00014ATInstallation of Lycoming model L/TIO-540-J2B engines in accordance with Colemill Enterprises, Inc. Installation Instructions for Modification of Piper Navajo Model PA-31-350 dated October 9, 1992, or later FAA approved, revision.STC SA00336ATInstallation of winglets.STC SA00616ATInstallation of McCauley Propeller Model 3AF32C504/82NEA, on Beechcraft Models 95-C55, 95-C55A, D55, D55A, E55, & E55A and McCauley Propeller Model, 3AF32C512/82NEA, on Beechcraft Models 58 & 58A, per Colemill Enterprises Installations Instructions dated November 11, 1994, or later FAA Approved Revision.STC SA1421SOInstallation of 40:1 gear ratio wing flap transmissions and related changes in accordance with Colemill Enterprises, Inc., Installation Instructions dated February 16, 1983, or later FAA approved revision. This modification provides and equivalent means of compliance with paragraphs (a)1, (a)2, and (a)4 of AD 82-27-13 and restores the 40 (full) flap travel.STC SA1762SOInstall two Teledyne Continental Motors model IO-550-C engines, Hartzell or McCauley propellers, nose cowling (P/N 74000-1) per Colemill Enterprises, Inc. Dwg. No. 74000, Initial Release dated October 29, 1984, and winglets (P/N 66000-50 and -51) per Colemill Enterprises Dwg. No. 66000, Initial Release dated October 29, 1984, in accordance with Colemill Enterprises, Inc. Installation Instructions for Modification of Beechcraft Models: C55, D55, E55, and 58 , dated September 14, 1984, or later FAA approved revision of this document or either drawing.STC SA1835SOInstall Teledyne Continental Motors Model IO-550-B engine, Hartzell HC-C4YF-1E/FC7063Q propeller and Hartzell D4511P, spinner on all models per Colemill Drawing P/N 82000C. Install Teledyne Continental Motors Model IO550-B engine, McCauley 3A32C76/82NB-2 propeller and McCauley D3584 spinner on models S-35, V35A, V35B, E33A, E33C, 35-C33A, F33A, and F33C per Colemill Drawing No. 82000, Rev. D. dated 10-30-87 or later FAA approved revision. Engines installed on models S35, V35, V35A, V35B, E33A, E33C, 35-C33A, F33A, and F33C are derated to 285 horsepower per AFMS. For 36/A36 models only, stall strip P/N 82000-4, per Colemill Drawing P/N 82000C, is required.STC SA2103SOInstallation of auxiliary fuel wing tips and winglets in accordance with Colemill Enterprises Installations Instruction for Modification of Beechcraft Baron Model 55 and 58 Aux Fuel Tank Installation revised July 28, 1986 and Colemill Enterprises Drawing No. 7800 Rev. A dated July 28, 1986. Colemill Enterprises Airplane Flight Manual Supplement dated April 28, 1987, is required with this installation.STC SA2109SOInstallation of Teledyne Continental Motors Model IO-470K engine in accordance with Colemill Enterprises Installation Instructions for Modification of Cessna Model 305-A-C-D-F Revised April 24, 1987 and Colemill Enterprises Drawing No. 3000 Revision A dated May 6, 1987.STC SA2207SOInstallation of two Teledyne Continental Motors Model IO-550-A engines in accordance with Colemill Enterprises Installation Instructions for Modification of Cessna model 310R in Accordance with Colemill Enterprises, Inc. Drawing AC6200 dated June 15, 1987, or later FAA approved revision. Colemill Enterprises Pilot s Operating Handbook and FAA Approved Flight Manual Supplement dated November 20, 1987, or Pilot s Operating Handbook and Airplane Flight Manual Supplement dated February 18, 2000 or later FAA approved revision is required for S/N 310R1501 and subsequent. Colemill Enterprises Supplemental Airplane Flight Manual Revised May, 11, 2001 or latter FAA approved revision is required for T310P S/Ns 310P0001 through 310P0240, T31Q S/Ns 310Q0001 through 310Q1160 and 310R/T 310R S/Ns 310R0001 through 310R2140.STC SA2996SOInstallation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-15 Rev. A dated July 5, 1991.STC SA2997SOInstallation of McCauley propeller governor.STC SA2998SOInstallation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-10 February 15, 1991.STC SA366SOGross weight increased to 6530 pounds.STC SA412SOInstallation of Continental IO-520-E or IO-550-E engines per Colemill Enterprises, Inc. Installation Instructions for modification of Cessna 310 and Drawing AC5400, as revised March 19, 1969, or later FAA approved revision of these documents.STC SA432SOInstallation of two Teledyne Continental Motors (TCM) model IO-520-E engines (derated to 260hp) and Hartzell model EHC-A3VF-2B/V7636D propellers and related changes in accordance with Colemill Enterprises Drawing AC5600 dated February 23, 1970, revised April 22, 1970.STC SA518SOInstallation of Continental IO-520-E derated engines and McCauley D3AF32C87/82NC-6 or -8 propellers. Modification to be accomplished in accordance with Colemill Enterprises, Inc. Drawing AC5800 Rev. A and AC5801 Rev A and Installation Instructions dated 7 July 1972 and revised 21 August 1972. Owner s Manual Supplement dated 21 August 1972 included in data.STC SA970SOInstallation of Lycoming TIO-540-J2BD or TIO-540-J2B engines and Hartzell propellers HC-C4YR-2/FC7663D-4R or HC-C4YR-2/FC7663D-6Q, additional fuel pump and related cowling changes.Modification Drawing Piper Navajo PA-31 Navajo-Panther-Drawing 68000, Revision D, Dated 5/17/82.
Installation Instructions for Modification of Piper Navajo Model PA-31 and PA-31-325, Drawing 68000, change D dated 5/17/82 and Supplemental Type Certificate (STC) SA970SO.
Installation Procedures Boost Pump PA-31 Drawing 62000 A Change dated November 30, 1977. (PA-31 Only)
Piper Kit 760-905
Colemill Enterprises, Inc., Process Specification for Drawings 64000 and 66000, dated August 31, 1977.
Colemill Enterprises, Inc., Process Specification #500 for Piper Wing Caps and Winglets, dated September 1, 1981.
Later FAA approved revisions of the above data are acceptable.STC SA981GL-DInstallation of a Bendix/King (AlliedSignal Avionics) CAS 81A Traffic and Collision Avoidance System (TCAS II) and two MST 67A Mode S Transponders in accordance with Garrett Aviation Services drawing list DL981, revision E, dated January 05, 2001, or later FAA approved revision.STC SA02378AKInstallation of structural provisions for a fuselage side mounted baggage door in accordance with Alaska Aircraft Products, LLC drawing number 8029, Revision - , dated May 27, 2010 or later FAA approved revision.STC SR01474NYInstallation of a Honeywell Mk-XXII Enhanced Ground Promixity Warning System.STC SR01697AT-DReplacement Low or High Skid Tubes and Lightweight Flotation Skid Tubes in accordance with Aeronautical Accessories, Inc. Drawing List Report AA-98007, Revision I, dated July 18, 2006, and installation per Report AA-98006, Revision D, dated March 31, 2003, or per Report AA-99024, Revision F, dated November 29, 2005, or later DAS approved revisions.STC SR02162LAInstallation of Mounting Provisions for a Tail Boom Radar Altimeter in accordance with FAA approved Meeker Aviation Drawing List for Radar Altimeter Mount Kit, AA-TBA-16-010, Revision A, dated August 18, 2008 and Document List for Radar Altimeter Mount Kit,
AA-TBA-16-011, Revision IR, dated February 20, 2008 or later FAA approved revisions.STC SR09254RCInstallation of Scuba Seats in accordance with Premier Aviation, Inc. Master Drawing List Number B00-13035, Revision B, dated August 17, 2000 or later FAA approved revisions. Rotorcraft Flight Manual Supplement Drawing Number B09-63004, dated
August 3, 2000, or later FAA approved revision.STC SR09324RC-DInstallation of Passenger Photo Window in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-01095, Revision B, dated March 19, 2003, or later FAA/DAS approved revision.STC SR09325RCInstallation of Bulged Skylight in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-01070, No Revision dated May 23, 2001, or later FAA approved revision.STC SR09326RCDevelopment and Installation of High Visibility Crew Door in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-01073, No Revision, Dated July 20, 2001, or later FAA approved revision.STC SR09327RCInstallation of a Bendix-King EFS 40/50 Electronic Flight Information System and LITEF LCR-92 Attitude Heading Reference System with Aeronautical Accessories, Inc. (AAI). AAI Drawing List Report Number AA- 01062, No Revision, dated July 11, 2001, or later Federal Aviation Administration (FAA) approved revision (s).STC SR09329RCInstallation of an Enhanced Ground Proximity Warning System (EGPWS) in accordance with Aeronautical Accessories, Inc., Document Number AA-01100, Revision B, dated
October 17, 2001, or later Federal Aviation Administration (FAA) approved revision(s).STC SR09330RCInstallation of Replacement Low and High Skid Landing Gear Crosstubes in accordance with data listed on Aeronautical Accessories, INC. drawing list, Report No. AA-00004, Revision C, dated October 2, 2001 or later FAA approved drawing list revision.STC SR09337RCInstallation approval of replacement composite engine cowling doors in accordance with Aeronautical Accessories, Inc. Drawing List, Report AA-98178, Revision B, dated
January 23, 2002, or later FAA approved revision.STC SR09338RC-DInstallation of passenger photo window in accordance with Aeronautical Accessories, Inc. Drawing List AA-02013, Revision F, dated October 14, 2005, or later DAS approved revision.STC SR09340RCInstallation of interior trim kit.STC SR09347RC-DHelicopter Emergency Egress Lighting (HEEL) system kit in accordance with Aeronautical Accessories, Inc. Drawing List Report No. AA-02027, Revision A, dated
September 5, 2002, or later FAA/DAS approved revision. Rotorcraft Flight Manual Supplement, No Revision dated October 23, 2002, or later FAA/DAS approved revision is required.STC SR09369RC-DFlitestep Kit in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-03068, Revision A, dated September 30, 2003, or later DAS approved revision; and installation per Report No. AA-02047, No Revision, dated June 27, 2003, or later DAS approved revisions.STC SR09370RC-DCabin Floor Protector Kits in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-02091. Revision A, dated November 10, 2003, or later DAS approved revisions; and installation per Report No. AA-03090, No Revision, dated September 17, 2003, or later DAS approved revisions.STC SR09371RC-DCabin Floor Protector Kits in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-03084, Revision A, dated February 16, 2004, or later DAS approved revisions; and installation per Report No. AA-03082, No Revision, dated
November 12, 2003, and/or AA-03083, Revision A, dated February 16, 2004, or later DAS approved revisions.STC SR09372RC-DHigh Visibility Crew Door Kits in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-03141, Revision B, dated March 4, 2004, or later DAS approved revisions; and installation per Report No. AA-03137, Revision A, dated
February 9, 2004, and AA-03145, Revision A, dated February 25, 2004 or later DAS approved revisions.STC SR09374RC-DRetractable Hard Point Kit in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-05103, Revision Q, dated April 30, 2007, or later DAS approved revisions; and installation per Report No. AA-05104, Revision K, dated March 28, 2007, or later DAS approved revisions.STC SR09375RC-DFlitestep in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-05095, Revision A, dated December 22, 2005, or later DAS approved revision; and Installation Instructions Report No. AA-05099, Revision A, dated December 8, 2005, or later DAS approved revision.STC SR09376RC-DHigh Visibility Door Kits in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-05155, Revision G, dated January 25, 2007, or later DAS approved revision; and Installation Instructions Report No. AA-06086, Revision D, dated January 25, 2007 or later DAS approved revision.