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 SA2775SOInstallation of an emergency induction air door in accordance with Aircraft Specialist Installation Instructions, Alternate Air Door Adapter, dated April 30, 1990, or later FAA approved revision and Drawing Nos. AAD 16670-1, revised April 21, 1990; AAD 16670-2, revised April 21, 1990; and AAD16670-3, dated April 21, 1990, or later FAA approved revisions.STC SR02139SEFabrication of Onboard Systems Model 200-355-00 and 200-369-00 Cargo Hook Fixed Provision Kits, Model 200-356-00 Cargo Hook Suspension Kit, and Model 200-357-00 Load Weigh Kit, in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-160-00, Revision 2, dated September 27, 2011, or later FAA approved revision. Installation of the Onboard Systems Model 200-355-00, 200-356-00, 200-357-00, or 200-369-00 kits in accordance with FAA approved Onboard Systems Owners Manual 120-141-00, Revision 0, dated April 25, 2011, or later FAA approved revision.
This modification must be inspected and maintained in accordance with section ATA 5 of FAA approved Onboard Systems Instructions for Continued Airworthiness Document 123-036-00, Revision 0, dated May 5, 2011, or later FAA approved revision, and Onboard Systems Cargo HookSTC SR09518RCInstallation of Night Vision Goggle (NVG) compatible interior lighting system in accordance with Ahlers Aerospace, Inc. Master Drawing List 350-01(E99-129), Rev W, dated July 12, 2011, or later Federal Aviation Administration (FAA) approved revision. Rotorcraft Flight Manual Supplement: Ahlers Aerospace, Inc., Document No. E99-150, Rev. B, dated August 4, 2010; or E99-271, Rev. IR, dated July 12, 2011; or laterSTC SA566NEMedevac interior installation.STC SR01960NY-DInstallation of Baggage Access Panel (Ground Use Only), Forward Facing Seat, Seat Pan, and Wet Floor.STC SA100CEInstallation of Hoskins Supplemental Model A or B High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 1 or 2 High Intensity Fuselage Lights.STC SA103CEInstallation of Hoskins Supplemental Model B High Intensity Wing Tip Lights, Model C Tail Light, with or without Models 1 or 2 High Intensity Fuselage Lights.STC SA104CEInstallation of Hoskins Supplemental Model B High Intensity Wing Tip Lights, Model C Tail Light, with or without Models 1 or 2 High Intensity Fuselage Lights.STC SA106CEInstall Hoskins Model F or B Wing Tip Lights and Model C or K Tail Lights, with or without two Model 1 or 2 Fuselage Lights.STC SA107CEInstallation of Hoskins Supplemental Model A high intensity wing tip lights, model C or K tail lights, with or without models 1 or 2 high intensity fuselage lights.STC SA122CEInstall Hoskins supplementary light system consisting of colored Model A(or clear or colored Model E) wing tip lights, a Model C or 2 tail light, and optionally, two of Model 2 fuselage lights with M-3 or M-5 power supply.STC SA123CEInstallation of Model B high intensity wing tip lights, Model C tail lights, with or without models 1 or 2 high intensity fuselage lights.STC SA125CEInstallation of Hoskins Supplemental Model B of F High Intensity Wing Tip Lights, Model C or 30-0329-3 Dual Tail Light, with or without Model 2 High Intensity Fuselage Lights.STC SA1771WEInstallation of Hoskins MK V B Anti-Collision Light System in accordance with FAA Sealed Hoskins Top Drawing No. 10-0051.1 This Anti-Collision Light System meets the requirements of FAR 25.1397, 25.1401 (b) (c) and (f), (400 effective candles minimum) effective August 11, 1971. Hoskins Inc., FAA approved AFM supplement Dated June 06, 1972, is required with this modification.STC SA192CEInstallation of Hoskins Supplemental Model A High Intensity Wing Tip Lights, Model C Tail Light with or without Models 2 High Intensity Fuselage Lights.STC SA236CEInstallation of Hoskins Supplemental Model B High intensity wing tip lights, Model C tail lights, with or without Model 2 high intensity fuselage lights.STC SA2404WEConsolidation of STC s SA355CE and SA362CE into one STC having a Master Eligibility List and amendment of these STC s to include and improved Power Supply Assembly and Subchassis Timer Assembly for the Twilighter MK III high intensity supplementary lighting system in accordance with the applicable FAA sealed drawing listed on the attached sealed Master Eligibility List Number SA2404WE.STC SA249CEInstall supplementary lighting system using Model B or Model F Wing Tip Lights, Model C or Model K Tail Light. Optionally, two Model 2 fuselage lights may also be used with Model B Wing Tip Lights.STC SA253CEInstallation of Hoskins Supplemental, Model E, High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 2 High Intensity Fuselage Lights.STC SA2543WEInstallation of Hoskins Model 700801Anti-Collision Light in accordance with FAA sealed Master Eligibility List No. SA2543WE. While the requirements of FAR 23.1401(a), (c), (d), (e) and (f) are met by this installation, the requirements of FAR 23.1401(b) are not met. Since the aircraft was type certificated under airworthiness regulations that contained no Anti-Collision Light Standards for intensity and field of coverage, this installation is accepted. Hoskins FAA approved AFM Supplement (see MEL SA2543WE) is required with this modification.STC SA2588WEA Hoskins Model MK III (Twilighter) Anti-Collision Lighting System is installed in accordance with Hoskins Top Drawing 10-0043-1, Revision I as amended on December 21, 1972, or later FAA approved revision. The Anti-Collision Lighting System has been found to meet the Anti-Collision Light Standards of FAR 25.1401 in effect prior to August 11, 1971.
Hoskins FAA Approved AFM supplement date December 6, 1972 is required with this modification.STC SA2630WEInstallation of Hoskins (Pulstar TM) combined Position Anti-Collision Lighting System in accordance with FAA Sealed Hoskins Top Drawings No. 10-202186 or No. 10-202186-1. These Anti-Collision Lighting Systems have been found to meet the Anti-Collision Light Standards of FAR 23.1401, in effect of August 11, 1972. Hoskins FAA Approved AFM supplement dated December 27, 1972 or later FAA Approved Revision is required with this modificationSTC SA263CEInstallation of Hoskins Supplemental Model A High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 2 High Intensity Fuselage Lights.STC SA2719WEInstallation of Hoskins Britestar Anti-Collision Light in accordance with FAA Sealed Hoskins Top Drawing No. 10-202504-1, Rev. A or later FAA sealed revision as a replacement light for aircraft which have been previously FAA approved with Grimes Model 4285A-1-1105 or 30-0437-1 or Whelen Model HR-14 Anti-Collision Light.STC SA2720WEInstallation of Hoskins IFO-1A Anti-Collision Light in accordance with FAA Sealed Hoskins Top Drawing No. 10-202504 as a replacement light for aircraft which have been previously FAA approved with Grimes Model 4285A-1-1105 or 30-0437-1 or Whelen Model HR-14 Anti-Collision Light.STC SA2842WEInstallation of Novastar Anti-Collision Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-202776.STC SA2846WEInstallation of Hoskins Pulstar Twilight Supplemental Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-202864.STC SA302CEInstallation of Hoskins High Intensity Position Light system. A supplemental condenser discharge (strobe) lighting system. Consists of red/green/white wing tip and tail position lights, with or without white, top and bottom fuselage lights, plus a power supply.STC SA3233WE: Installation of Hoskins Novastar Anti-Collision Light in accordance with FAA sealed Hoskins Top Drawing No. 10-203467, Rev B., Dated June 24, 1975 or later FAA sealed revision.STC SA3418WEInstallation of Hoskins Novastar II Combined Position Anti-Collision Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-204054, N/C Dated February 15, 1977 or later FAA sealed revision.STC SA355CE: Installation of Hoskins Twilighter MK/III B High Intensity Lighting SystemSTC SA362CEDescription of Type Design Change: Install Hoskins Twilighter MK III per Installation Manual and Specification Sheets as amended, dated September 20, 1965. Install Hoskins Twilighter MK IIIB Supplemental Lights per the following required data: Models 310 through 310F and 320 Specification Sheets P/N 65-0025-5 with drawings listed; Models 310G through N and 320-1 through F Specification Sheets P/N 65-0025-6 with drawings listed; Models 401, 401A and 402 Specification Sheets P/N 65-0025-9 with drawing listed; Models 411 and 411A Specification Sheets P/N 65-0025-7 with drawings listed; and Models 421 and 421A Specification Sheets P/N 65-0027-8 with drawings listed.STC SA3660SWInstallation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing List DC-9-1000, Revision C, Dated October 7, 1986 or later FAA approved revisionSTC SA3665SW: Installation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing List DH-8-1000, Revision D, Dated December 02, 1986 or later FAA approved revisionSTC SA3686SWInstallation of floor proximity lighting system.STC SA3687SW: Installation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing List G1-1000, Revision C, Dated December 02, 1986 or later FAA approved revisionSTC SA3693SW: Installation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing Number FF27-1000, Revision C, Dated December 02, 1986 or later FAA approved revisionSTC SA3702SWInstallation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing List DH7-1000, Revision D, Dated December 02, 1986 or later FAA approved revision.STC SA3704SWInstallation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc., Drawing Number F27-1000, Revisions B, Dated December 02, 1986.STC SA3705SWInstallation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc. Drawing number SD3-1000, Revision B, dated December 2, 1986, or later FAA approved revision.STC SA374CEInstallation of Hoskins Twilighter Mk III Supplemental Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-0031.STC SA3768SWInstallation of Floor Proximity Lighting System in accordance with Vista Manufacturing, Inc. Drawing Number 727-1100, Revision C, Dated May 1, 1987STC SA378CEInstallation of Hoskins Supplemental Model (A) High Intensity Wing Tip Lights, Model (D) or (K) Tail LightsSTC SA379CEInstallation of Hoskins Twilighter MK V High Intensity Aircraft Lighting System. This is a Supplemental Condenser Discharge (Strobe) Light System, consisting of five (5) Light Units and a Power Supply.STC SA383CEInstallation of Hoskins Twi. III supplementary high intensity lighting system.STC SA3863SWReplacement of emergency lighting power supplies with Vista Airpak 35D power supplies in accordance with Vista Manufacturing, Inc., Drawing List 87-5200-A, Dated November 4, 1987, or later FAA approved revision.STC SA392CEInstall Hoskins Twilighter Mk V supplementary lighting system including Model E wing tip lights and Model C tal lights.STC SA394CEInstall Hoskins Twilighter MK III Supplemental High Intensity Lighting System consisting of three Condenser Discharge (Strobe) Light fixtures and a Power Supply.STC SA398CEInstall Hoskins Twilighter MK III Supplemental Lighting System consisting of Model F Wing Lights with Model P or K (dual) Tail Light.STC SA399CEInstallation of Hoskins Supplemental Position Light System which includes Model B (Dual) Wing Tip Light, Model C, D, or K Tail Light with or without Model 2 Fuselage Lights.