TCDS A-694
STCs approved under this data sheet · 131
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 = 'A-694') 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 = 'A-694') 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 SA5156NMFabrication and installation of Pulsar-MOSFET Landing Light Flasher SystemSTC SA01251SEThe manufacture of a Sunvisor System.STC SA02194SEInstallation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package MA2233, Revision IR, dated September 27, 2010, Installation Manual MA2234, Revision IR, dated September 6, 2011, and Instructions for Continued Airworthiness, MA0666, Rev A, or later FAA approved revisions.
NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.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 SA01256SEInstallation of BAS, Inc. shoulder harness with inertia reelSTC SA3816NMInstallation of a BAS, Inc., tail pull handle in the aft fuselage.STC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA593CHInstall Champion SlickSTART magneto booster system.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA02283AKInstallation of a 30 amp permanent magnet generator system.STC SA1-271Replacement of fabric covering with metal skins.STC SA02097NYDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in LUSCOMBE, 8E, Serial Number 5236. Installation of Continental 0-200-A Engine, Cessna 60 Amp Alternator, and McCauley 1A100 MCM Propeller.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA2683NMInstallation of Precise Flight, Inc. stand-by vacuum system (SVS)STC SA2248CEInstallation of Continental 0-200-A engine and fixed pitch propellers. Data pertinent to this modification are considered inadequate for duplication in other airplanes. This approval is limited to the installation made in Luscombe Model 8A, Serial Number 4938, only.STC SA01944CHModify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.STC SA730GLSuperseded by SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.STC SA8075SWInstallation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER)STC SA1008WEInstallation of Poly-Fiber covering material.STC SA01135WIDesign change to modify Skylight Window Panel to use fitted window stripping for better weatherproofing, corrosion protection, and ease of installation and replacement.STC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA01092WI3-point Lap Belt-Shoulder Harness Restraint System installation using inertia reel.STC SA1076GLSurrendered and incorporated into STC SA00478CH.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA09470SCInstallation of Starter Indicator light system.STC SA71GLInstallation of air filtersSTC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA2715WEInstallation of carry-through spar beams.STC SA00215NYInstallation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.STC SA1084NEInstallation of McCauley Model1B90/CM7447 fixed pitch metal propeller.STC SA5926NMInstallation of manifold pressure instrument.STC SA5159NMInstallation of chip detector system.STC SA5755NMInstallation of a propeller anti theft device.STC SA2241CEOperation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock indes (RON+MON)/2.STC SA3214SOInstallation of Basic Type BYE-14, No. 1008 air driven alternator.STC SA2705SOInstallation of inspection openings.STC SA3364NMInstallation of a 6.5 gallon auxiliary fuel tank in the right wing.STC SA5639SWUse of autogas.STC SA3363NMReplace standard wheels and brakes with McCuley wheels and brakes and Scott actuating cylinders.STC SA2181NMInstallation of new baggage compartment floorboard material.STC SA1938CEONE ONLY STC, SN 1874: Operation of airplane on unleaded automotive gasoline, 87 minium antiknock index (RON+MON)STC SA5622SWUse of unleaded automobile gasoline.STC SA1351WEReplace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12)STC SA2100NMInstallation of fuselage reinforcement patch and stiffner, a Continental 0-200-A4B engine and a McCauley 1890/CN7146 propeller.STC SA1249NWInstallatino of a McCauley propeller, belly-mounted air driven generator and associated wiring, modified rear baggage compartment, fishing rod box, hat shelf, "D" windows, and cockpit floorboardsSTC SA4-1210Installation of Eonnex cover on aircraft surfaces.
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