TCDS 1A15
STCs approved under this data sheet · 442
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 = '1A15') 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 = '1A15') 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 SA01421ATInstallation of an OCEM AP-3C autopilot. (PA-24-180)STC SA00954ATInstallation of composite bulkhead.STC SA01299SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics , Inc. Drawing Package Document MA2191, Revision IR, dated September 17, 2003, and Installation Manual MA2192, Revision IR, dated October 27, 2003, or later FAA approved revision to either of these documents.STC SA2167NMInstallation of the Precise Flight stand-by vacuum system (SVS).STC SA4150NMInstallation of Precise Flight Series 100 Speedbrake System.STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC ST02547ATInstallation of a voice alert system.STC ST02651ATReplace rudder balance weight kit #760705 with new advanced design used by Piper on PA-24-400 Model aircraft for rudder balance in accordance with Southland Aviation Drawing 24-001, dated April 17, 2003.STC SA00175DEInstallation of Oilamatic Preoiler system.STC SA5983NMCockpit sun visor installation.STC SA00695SEReplacement of certain Rotomaster and Rayjay scavenge pumpsSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA434NEInstallation of William C. Roberts' steel brake discs P/N 201-19-SS dated 6/29/85, in lieu of Piper carbon steel brake discs, Piper 754-530.STC SA2584CEInstallation of LH and RH main fuel cell bladders, P/N's DF054-324 and DF054-325, as replacements for original bladders.STC SA2652CEInstallation of main fuel cell bladders as replacements for original bladders.STC SA01352LAReplacement of Piper Battery box part numbers 20659-00, 21524-00, 21524-02, 25338-00, or 26240-00 and venting battery, with Riley Aircraft Battery Box, part number 1001TR, and Gill manifold battery Model G-35M.STC SA00336NYInstallation of 'second wind' auxiliary vacuum system.STC SA108NEReplacement of brake disc, Piper P/N 751672.STC SA633NEInstallation of William C. Roberts Stainless Steel Brake Discs P/N202-22SS Revised 9/21/86 in lieu of Piper, Carbon Steel Brake Discs, Piper P/N 754 554. Brakes are to be installed.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA6019NMInstallation of an electronic digital engine tachometer.STC SA02410ATReplace existing Auxiliary Electric Standby Fuel Pump with PMA Products, Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v), 1A15-s/n 24-3642, 24-4000 through 24-4782, 24-4784 through 24-4803, 2A13-s/n 28-7690001 through 28-7990626, 28-8090001 and up(14v)STC SA8544SW-DInstallation of a Century Automatic Flight System, Model AK1066 consisting of a Century 2010/2030/2031/2050/2051 autopilot per Bulletin No. 2131.STC SA3565WEInstallation of single piece windshield.STC SA09470SCInstallation of Starter Indicator light system.STC SA09012AC-DInstallation of S-TEC System 55/55X two axis automatic flight guidance system, model ST-595STC SA01349NYInstallation of oil temperature coupler kit, P/N ALH-I-005, with Airparts Installation Drawing List as listed on AML No. Sa01349NY.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA00947ATInstallation of composite spinner.STC SA01257ATInstallation of composite spinner assemblies.STC SA01853ATReplace Aluminum alloy propeller spinner with composite spinner.STC SA09413AC-DInstallation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems, Model ST-777-40X/50X.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 SA693CEReplace existing engine induction air filter with AC Spark Plug filter.STC SA71GLInstallation of air filtersSTC SA1153SWSquare wing tips with dual navigation lights.STC SA00391SEInstallation of Rajay Model 315 F10 turbocharger on the above aircraft with a Lycoming O-360-A1A engine installed.STC SA3070WEInstallation of single piece windshield.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA526GLInstallation of aileron, flap, flap to fuselage, and rudder gap seals, wing root fairings, and dorsal fin.STC SA1115SWDual brakes.STC SA1152SWInstallation of one-piece windshield.STC SA531SWFifth seat installationSTC SA2619WEInstallation of Pathfinder Model P1-( ) autopilot system.STC SA2620WEInstallation of Pathfinder Model P2-( ) autopilot system.STC SA01224ATInstallation of wheel hub cabs with valve stem access door.STC SA3773WEInstallation of Hoskins Model CFS-1000, -1001, FT-100, or FT-101 fuel flow indicating system. *This installation limited to those aircraft with fuel injected engines.STC SA2648CEInstallation of flap actuated gear warning system.
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