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.

STC SA09355SCModifications to reduce airframe aerodynamic dragRAM Aircraft Limited PartnershipSTC SA09544SCInstallation of a wastegate in-line oil strainerRAM Aircraft Limited PartnershipSTC SA3721SWInstall vacuum pump cooling shroud.RAM Aircraft Limited PartnershipSTC SA4213SWInstallation of repaired modified exhaust riser assemblies.RAM Aircraft Limited PartnershipSTC SA4331SWRevised exhaust system.RAM Aircraft Limited PartnershipSTC 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.RAM Aircraft Limited PartnershipSTC SA4592SWInstallation of improved engine cooling baffle and improved exhaust system slip joints.RAM Aircraft Limited PartnershipSTC SA4851SWInstallation of combination aft position/strobe light on aircraft tail stinger.RAM Aircraft Limited PartnershipSTC 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 wingletsRAM Aircraft Limited PartnershipSTC SA5878SWInstallation of range-marked EGT, CHT, oil temperature, and pressure gauges.RAM Aircraft Limited PartnershipSTC 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.RAM Aircraft Limited PartnershipSTC SA7566SWInstallation of throttle, mixture, and propeller control cables.RAM Aircraft Limited PartnershipSTC SA7594SWInstallation of Cablecraft throttle, mixture, and propeller control cables.RAM Aircraft Limited PartnershipSTC SA7773SWInstall propeller governor control bracket.RAM Aircraft Limited PartnershipSTC 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.RAM Aircraft Limited PartnershipSTC SA1763GLInstallation of the Ryan Itn'l traffic collision alert device (TCAD), 9900 series, P/N 71-2100, 71-2200, 71-2400.Ryan Intl CorpSTC SA08996AC-DInstallation of S-TEC System 55/55X Two Axis automatic flight guidance system, Model ST-578S-TEC CorporationSTC SA09401AC-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-853,S-TEC CorporationSTC SA117NWInstallation of Allison 250-B17 or 250-B17B engines and related changes.Alaskan Turbine S.T.O.L. AircraftSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.STC SA01117ATInstallation of Composite Spinner.TCB Composite Co.STC SA1742SWInstallation of vapor cycle air conditioning system.Signature Flight Support CorporationSTC 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)D & K AviationSTC SA00804SEInstallation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'Advanced Aero Safety Inc.STC SA71GLInstallation of air filtersBrackett Aero Filters Inc.STC SA09472SCModifications are only applicable to air conditioner systems.Steinbach & Associates, Inc.STC SA3003WEInstallation of recognition light assembly on horizontal stabilizerDeVore Aviation Corporation of America, a New Mexico CorporationSTC SA00833WIInstallation of a seat headrest.Aviation Fabricators IncSTC SA5786SWInstallation of Pratt & Whitney of Canada PT6A-135, -135A engines and optional McCauley 4HFR34C762/94LMA-4 propellers.Blackhawk Modifications Inc.STC SA00381DEModification of the Cessna 421C for installation of a Space Imaging System.Space ImagingSTC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsJ P InstrumentsSTC SA4956NMOPTION 1: Installation of American Aviation intercooled engines as modified by STC SE4159NM. OPTION 2: This installation with the cowl scoops only.American Aviation IncSTC SA09517SCInstallation of a children's critical care childs stretcher assembly, p/n 100-1.Children's Critical Care, IncSTC SA01680ATNew Maximum gross weight limitation of 6000 pounds.Walliser MarkusSTC SA00537SEInstallation of vortex generators on the wing and rudder surfaces, and installation of nacelle strakes.Micro AeroDynamics IncSTC SA5362SW-DInstallation of S-TEC yaw damper system, Model ST-238.S-TEC CorporationSTC SA8524SW-DInstallation of a Century Automatic Flight System, Model AK1047 consisting of a /Century 2110/2130/2131/2150/2151 autopilot.Century Flight Systems IncSTC SA00514SEInstallation of vortex generators on the wings and rudder and installation of a strake on the outboard side of each engine.Micro AeroDynamics IncSTC SA00074SEInstallation of vortex generator system on the wing and vertical stabilizer of these aircraftAeronautical Testing Service Inc.STC SA1007NWInstallation of a low thrust detector system.Engine-Out Warning Systems, LLCSTC SA09337AC-DInstallation of S-TEC System 30 ALT Altitude Hold System, Model ST-744.S-TEC CorporationSTC SA1806NMInstallation of Hoskins CFS-2002 computerized fuel flow indicating system.Sandia Aerospace CorporationSTC SA2780SWInstallation of Hoskins Model CFS-2000, -20001, or FT-2000 fuel flow indicating system.Sandia Aerospace CorporationSTC SA2812SWInstallation of Hoskins Model CFS-2000, -2001, or FT-200 fuel flow indicating system.Sandia Aerospace CorporationSTC SA2845SWInstallation of Hoskins Model CFS-1000, -1001, or FT-100 fuel flow indicating system.Sandia Aerospace CorporationSTC SA3577NMInstallation of Hoskins CFS-2212 computerized fuel flow indicating system.Sandia Aerospace CorporationSTC SA4231WEInstallation of Hoskins Model CFS-2000, -2001 or FT-200 fuel flow indicating system.Sandia Aerospace CorporationSTC SA00333DEInstallation of wastegate exhaust inlet elbow.Heliarc Welding Service Inc.STC SA00749ATModification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent)Aero Trim, IncSTC SA02095AKInstallation of hourmeter airspeed switch.Avalaska Inc
Back to TCDS A7CE