TCDS A7CE
STCs approved under this data sheet · 597
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 = 'A7CE') 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 = 'A7CE') 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 SA09355SCModifications to reduce airframe aerodynamic dragSTC SA09544SCInstallation of a wastegate in-line oil strainerSTC SA3721SWInstall vacuum pump cooling shroud.STC SA4213SWInstallation of repaired modified exhaust riser assemblies.STC SA4331SWRevised exhaust system.STC SA4379SWInstallation of Teledyne Continental TSIO-520-NB engines as modified by STC SE4327SW, and Hartzell PHC-C3YF-2UF/FC7663D-2Q or PHC-C3YF-2UF/FC7663DB-2 propellers or McCauley 3AF32C93/82NC-6.0 to-7.0 or 3AF32C505/82NEA-6.0 to-7.0 propellers.STC SA4592SWInstallation of improved engine cooling baffle and improved exhaust system slip joints.STC SA4851SWInstallation of combination aft position/strobe light on aircraft tail stinger.STC SA5811SWIncrease maximum ramp weight to 7610 pounds; maximum takeoff weight to7560 pounds; maximum landing weight is 7200 pounds; decrease zero fuel weight to 6533 pounds; install wingletsSTC SA5878SWInstallation of range-marked EGT, CHT, oil temperature, and pressure gauges.STC SA5981SWIncrease maximum ramp weight to 7610 pounds, maximum takeoff weight to 7560 pounds, maximum landing weight is 7200 pounds, maximum zero fuel weight is 6533 pounds.STC SA7566SWInstallation of throttle, mixture, and propeller control cables.STC SA7594SWInstallation of Cablecraft throttle, mixture, and propeller control cables.STC SA7773SWInstall propeller governor control bracket.STC SA8726SWIncrease maximum ramp weight from 6750 to 7140 pounds and maximum takeoff weight to 7105 pounds, and addition of optional McCauley model 3AF32C515/82NLA-4.0 propellers.STC SA1763GLInstallation of the Ryan Itn'l traffic collision alert device (TCAD), 9900 series, P/N 71-2100, 71-2200, 71-2400.STC SA08996AC-DInstallation of S-TEC System 55/55X Two Axis automatic flight guidance system, Model ST-578STC SA09401AC-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-853,STC SA117NWInstallation of Allison 250-B17 or 250-B17B engines and related changes.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA01117ATInstallation of Composite Spinner.STC SA1742SWInstallation of vapor cycle air conditioning system.STC SA01280CHInstallation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404)STC SA00804SEInstallation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'STC SA71GLInstallation of air filtersSTC SA09472SCModifications are only applicable to air conditioner systems.STC SA3003WEInstallation of recognition light assembly on horizontal stabilizerSTC SA00833WIInstallation of a seat headrest.STC SA5786SWInstallation of Pratt & Whitney of Canada PT6A-135, -135A engines and optional McCauley 4HFR34C762/94LMA-4 propellers.STC SA00381DEModification of the Cessna 421C for installation of a Space Imaging System.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA4956NMOPTION 1: Installation of American Aviation intercooled engines as modified by STC SE4159NM. OPTION 2: This installation with the cowl scoops only.STC SA09517SCInstallation of a children's critical care childs stretcher assembly, p/n 100-1.STC SA01680ATNew Maximum gross weight limitation of 6000 pounds.STC SA00537SEInstallation of vortex generators on the wing and rudder surfaces, and installation of nacelle strakes.STC SA5362SW-DInstallation of S-TEC yaw damper system, Model ST-238.STC SA8524SW-DInstallation of a Century Automatic Flight System, Model AK1047 consisting of a /Century 2110/2130/2131/2150/2151 autopilot.STC SA00514SEInstallation of vortex generators on the wings and rudder and installation of a strake on the outboard side of each engine.STC SA00074SEInstallation of vortex generator system on the wing and vertical stabilizer of these aircraftSTC SA1007NWInstallation of a low thrust detector system.STC SA09337AC-DInstallation of S-TEC System 30 ALT Altitude Hold System, Model ST-744.STC SA1806NMInstallation of Hoskins CFS-2002 computerized fuel flow indicating system.STC SA2780SWInstallation of Hoskins Model CFS-2000, -20001, or FT-2000 fuel flow indicating system.STC SA2812SWInstallation of Hoskins Model CFS-2000, -2001, or FT-200 fuel flow indicating system.STC SA2845SWInstallation of Hoskins Model CFS-1000, -1001, or FT-100 fuel flow indicating system.STC SA3577NMInstallation of Hoskins CFS-2212 computerized fuel flow indicating system.STC SA4231WEInstallation of Hoskins Model CFS-2000, -2001 or FT-200 fuel flow indicating system.STC SA00333DEInstallation of wastegate exhaust inlet elbow.STC SA00749ATModification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent)STC SA02095AKInstallation of hourmeter airspeed switch.
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