TCDS 3A16
STCs approved under this data sheet · 608
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 = '3A16') 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.
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 = '3A16') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.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 SA1548WEInstallation of a Brittain Model B-5P flight control system.STC SA1591WEInstallation of Brittain Model B-5 flight control system.STC SA1833WEInstallation of Brittain Model NAV-2B flight control system.STC SA1958WEInstallation of Brittain Industries NAV-2B flight control system.STC SA4016NMInstallation of Vortex Generators on the wings and vertical tailSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.STC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemSTC SA02387AKFabrication and installation of the LSI Exterior LED Lightning SuiteSTC SA2031WEInstallation of Brittain Industries, Inc. Model B-VII (B-7), NAV-2B, or B2C Flight Control SystemSTC SA2048WEInstallation of Brittain Industries, Inc. Model B-VII (B-7), NAV-2B, or B2C Flight Control SystemSTC SA1770WEInstallation of Brittain Industries, Inc. Model B-5, NAV-2B, or B2C Flight ControlSTC SA1677WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemSTC SA1494WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemSTC SA289CHInstallation of Inline Pneumatic Air Filter, P/N CV1J4STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplaySTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemSTC SA09220SCInstallation of D Shannon Products Cooling Air Baffles kitSTC SA01349ATInstallation of winglets, P/N's66000-50 and 66000-51.STC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemSTC SA5156NMFabrication and installation of Pulsar-MOSFET Landing Light Flasher SystemSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverSTC SA00281BOInstallation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000STC SA3845SWInstallation of Teledyne Continental Motors IO-550C engines and McCauley 3AF32C512/82NEA-5 or Hartzell PHC-C3YF-2UF/FC7663 (B, K) -2R or Hartzell PHC-J3YF-2 (U) F/FC7663 (B,K) -2R propellers in accordance with D Shannon Products Drawing List No. DL87001, Revision 4, 08/24/92, or later FAA Approved revisions.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 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 SA378CEInstallation of Hoskins Supplemental Model (A) High Intensity Wing Tip Lights, Model (D) or (K) Tail LightsSTC SA1471CEInstallation of flap and aileron seals per Smith Speed Conversions, Inc. Drawing List 1004 stamped FAA Approved on February 5, 1979, or later.STC SA1472CEInstallation of elevator tail cone fairing per Smith Speed Conversions, Inc. Drawing List No. 1005 stamped FAA Approved on February 5, 1979, or later.STC ST01494LAInstallation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA, or later FAA approved revisions. No flight manual is required.STC SA23EAInstallation of Third Cabin Window on both sides of Fuselage in accordance with Glenn Floyd Stauffer Drawing Nos. 42601, Revision A dated 31 May 1962 and 42602, Revision A dated 13 June 1962.STC SA00243BOInstallation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).STC ST00961LAInstallation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated
June 26, 2000, or later FAA approved revisions.STC SA09222SCInstallation of B-1112 air/oil separator in accordance with J.V.E., Inc. Drawing List DL-8800, Revision 3, dated 03/14/96, Installation Manual BOS-AO1, Revision A, dated 01/22/96, or later FAA approved revisions.STC SA197NWInstallation of Clark three- light gear position indicator system.STC SA2871WEInstallation of right and left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB-1301.STC SA632CEInstall wing leading edge fuel t anks.
Data required: FLOAIR Drawings 56001 Documents 1440
56002 Sheets 1 & 2 1450
56003 1460
56004
56005
56006 56008
56007 56009STC SA681CEInstallation: Wing leading edge fuel tanks
Data required: Floair Document 141-3.21.1 dated June 23, 1972, and approved Airplane Flight Manual Supplement, Floair Document 141-3.91 dated July 24, 1972.STC SA02676CHInstallation of left and right hand fuselage external doublers per attached FAA Approved Model List (AML) No SA02676CH, issued June 8, 2011, or later FAA approved revision.STC SA02561CH-DInstallation of the Hartzell propeller model PHC-C3YF-2UF/FC7391D(B) and PHC-J3YF-2UF/FC7391D(B) propellers in accordance with installation instructions INST_102210 dated October 22, 2010, or later FAA Approved revisions.STC SA1315WEInstallation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.STC SA03913ATInstallation of the Astronics LED Replacement Lighting Bulbs in accordance with Chippewa Aerospace Master Drawing List (MDL) No. P23-3340-01-0001, Rev. 1, Dated November 01, 2010, or later FAA approved revision.STC SA00670SEReplacement of certain Goodrich pneumatic deicer boots in accordance with SMR Technologies, Inc. Installation Instructions as listed on AML No. SA00670SE.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 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 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 SA2997SOInstallation of McCauley propeller governor.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 SA01085SEInstallation of BAS, Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE, dated May 13, 2002, or later FAA approved revision.STC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)
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