TCDS A24CE
STCs approved under this data sheet · 895
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 = 'A24CE') 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 = 'A24CE') 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 SA00232WI-DInstallation of Collins FDS-255 Flight Display System. Must be installed concurrently with STCs SA00234WI-D, SA01037WI-D, SA01038WI-D, and SA01039WI-D.STC SA00234WI-DInstallation of Collins TCAS II Traffic Alert and Collision Avoidance System. This STC must be installed concurrently with STCs SA00232WI-D (Drawing Index AAC-0251-001), SA01037WI-D, SA01038WI-D and SA01039WI-D.STC SA01037WI-DInstallation of Collins FMS-3000 System.STC SA01038WI-DInstallation of Collins ARC-210 VHF/UHF Communication System.STC SA01039WI-DInstallation of AlliedSignal EGPWS System. This STC must be installed concurrently with STCs SA00232WI-D (Drawing Index AAC-0251-001), SA00234WI-D (Drawing Index AAC-0250-001), SA01037WI-D and SA01038WI-D.STC SA02264CHInstallation of Air Data SystemsSTC SA01812CHInstallation of a Honeywell MK VI Enhanced Ground Proximity Warning System (EGPWS).STC SA10500SCInstallation of a TCAS 4000 and Dual TDR-94D Mode-S Transponder SystemSTC SA00171BOInstallation of Pratt & Whitney Engine Services, Inc. Aircraft Data Acquisition System ADAS+, P/N ADAS-K-010.STC SA2842SOInstallation of ground cooling freon system.STC SA2843SOInstallation of ground cooling freon system.STC SA3299SOInstallation of an aircraft security system.STC SA01058CHInstallation of McCauley Propeller Model 4HFR34C754/94LA-0.STC SA01157CHInstallation of McCauley Propeller Systems 5HFR34C1008/96LTA-0 5 bladed model propeller.STC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.STC ST01456SEGroup approval for Reduced Vertical Separation Minimum (RVSM).STC SA01336WI-DModification of a Collins CDU-2000/3000 Control Display Unit(s) installationSTC SA02160CHInstallation of Medical Storage Cabinet.STC SA09477AC-DInstallation of: Garmin GNS-530 integrated navigation and communication system, Honeywell TPU-66A TCAS-I system, Collins TDR-90 Dual
Transponders, Collins DME-40 system, Honeywell ART-2000 weather Radar
Assembly and a KMD-850 Multi-Function Display, BF Goodrich AI-804 Standby Horizon- and a Sigtronics SDB-800 Intercom.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA09907SCInstallation of a Honeywell KGP-560 Enhanced Ground Proximity Warning System to reduce the likelihood of controlled flight into terrain and/or collision with another aircraft.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA01981NYInstallation of a Universal Avionics Terrain Awareness Warning System (TAWS).STC SA01175WIInstallation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS).STC SA01176WIInstallation of Collins TCAS-4000 Traffic Alert and Collision Avoidance System (TCAS-II).STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA02217AKInstallation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.STC SA1021GLRemoval of TC P/N 213762 propeller synchrophaser control box and electrical connector and installation of P/N A213796.STC SA02021NYRelocate fire detection control box from behind instrument panel to below cockpit floor. Add protective box to fuel shutoff circuitry in engine nacelle.STC SA01458LAInstallation of Universal Avionics Unilink 60X/70X Airborne Communications System.STC SA01980NYInstallation of a cabin power bus system.STC SA01945NYCockpit voice recorder replacement with Universal CVR 30B or CVR 120.STC SA02222AKLimit maximum seating capacity to 9 passengers or less.STC SA3067NMInstallation of monorail sun visor system.STC SA00872CHInstall air ambulance conversion in accordance with Aeromed Systems, Inc. Drawing list Report 3052, Revision -, dated September 2, 1997, or later FAA approved revisions.STC SA01639NYReplacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.STC SA4475SWInstallation of Omega Navigation System CMA-771 consisting of a suppressed plate antenna, control display unit, and receiver processor unit.STC SA01888NYInstallation of a Communicator System.STC SA01622CHInstallation of an SEI Quick Access Recorder.STC ST02815ATInstallation of a cockpit door and modification of the forward bulkhead in accordance with U. S. Technical Master Drawing List Document No. 4099-25-000, revision G, dated March 4, 2004, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement (AFMS), U.S. Technical Document No. U10-0127, dated March 8, 2004, or later FAA approved revision, is a required part of this modification. Instructions for Continued Airworthiness can be found in U. S. Technical Document No. U10-0129, release 1, dated March 4, 2004, U. S. Technical Document U10-0128, release 1, dated March 4, 2004, and U. S. Technical Document U10-0130, release 1, dated March 4, 2004.STC SA01921CHInstallation of upgraded Bendix/King EFIS-10 Symbol Generators.STC SA00948CHInstallation of various de-icer wire harnesses. (E90 modified by STC SA3593NM, F90 modified by STC SA4131NM, B200 modified by STC SA2698NM-S, DHC-6 Series modified by STC SA3532NM)STC SA01852NYInstallation of a Communicator System. Limited to installation on serial number UE-227.STC SA00523SEReplacement of certain BF Goodrich pneumatic deicer boots.STC SA01914CHInstallation of dual Rockwell Collins AHS-1000S Attitude Heading System.STC SA4361NMThe Apollo II IFR Model 614R Loran-C Navigation System is installed in Beech King Air airplane S/N BB-946. The Loran Unit is defined by Configuration Index Document D-253, Revision 0, or later FAA approved revision, and the system is installed in accordance with Installation Manual 560-4007, Revision 6, or later FAA approved revision, and Installation Report R-89, Revision 7, or later FAA approved revision.STC ST02718ATInstallation of a Honeywell Model MK VI Enhanced Ground Proximity Warning System (EGPWS).STC SA01190WI-DInstallation of the Bendix/King KGP 860 GA-EGPWS as a Class B TAWS.STC SA01873CHReplacement of certain Goodrich pneumatic deicer boots.STC SA00522DEReconfigure aircraft to a maximum seating of 9 passengers. Limited to installation on model B300, serial number FL-213 ONLY.
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