TCDS A-691
STCs approved under this data sheet · 233
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-691') 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-691') 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 SA01768SEInstallation of an oil cooler system.STC SA02604CHInstallation of a battery powered engine starting system.STC SA4305WEInstallation of GAR-AERO wheel adapters and tundra type tires on the main landing gearSTC SA01669CHInstallation of Challenger Reusable Air FilterSTC SA02436AKInstallation of F. Atlee Dodge Inverted DoglegSTC SA10921SCInstallation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulatorsSTC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 2Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA02428AKInstallation of a hydraulically actuated ski drag assemblySTC SA02295SEInstallation of an alternate method of fastening aluminum wing ribs to wood sparsSTC SA02128LAInstallation of aileron and flap hinge repair bushingsSTC SA01765SEInstallation of Alaskan Bushwheel TSO-C26d wheels, Part Number (P/N) ABI-1010STC SA01026SEImproved fuel gascolator assembly.STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA214ALInstallation of Airglas Engineerins Model L-1650A and L2000A Wheel Replacment SkisSTC SA01251SEThe manufacture of a Sunvisor System.STC SA460SWInstall wing tips in accordance with Cub Crafters, Inc. Master Drawing List., MDL102400, Revision C, dated May 30, 2001, or later FAA approved revision.STC SA68ALFabrication and installation of Stoddard Model 3 wing tank per Stoddard Aero Service Drawing List No. 68, dated February 7, 1975, or later Federal Aviation Administration approved revision.STC SA00243BOInstallation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).STC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA00270BOInstallation of a Teledyne Continental A-65-8, A-65-8F, A-65-9, A-75-8, A-75-8F, A-75-9, C-75-8, C-75-12, C-85-8, C-85-12, C-90-8F or C-90-12F engine and corresponding propeller identified under Limitations and Conditions, and components for a landplane maximum gross weight of 1220 lbs.STC SA3ALInstallation of Fred A. Shaw tundra-bird Model 2500 skis.STC SA5-13Installation of 8.50x6 tires and tubes with Hayes 6-inch wheels.STC SA501ALInstallation of fiberglass wing tips.STC SA02002SEInstallation of vortex generators on the above model aircraftSTC SA593CHInstall Champion SlickSTART magneto booster system.STC SA02316AKInstallation of 8.50-6 and 8.50-10 tiresSTC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA02171AKInstallation of a 24-gallon right wing fuel tank, P/N DC18049-24G-25R and 24-gallon left wing fuel tank, P/N DC10849-24G-32L.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA02299AKInstallation of a replacement fuel selector valve.STC SA02295AKInstallation of a high capacity fule gascolator assembly.STC SA4615NMFabrication and installation of welded steel universal aft fuselage float strut attachment fittings.STC SA01516SEReplacement of the Scott Master Brake Cylinder (Non-Vented Diamphram type) with a Steve s Aircraft Model SA6-01 Master Cylinder with a vented reservoir.STC SA02387CHInstallation of Piper Part Number 12649-00 Stabilizer and Piper Part Number 12647-00 Elevators in lieu of original components.STC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA3-111Removed 18 from the outboard end of each wing. Removed the first rib inboard of bow, and also the bow. Manufactured from .032 24ST al. Alloy sheet, a full size rib, installed on wing in place of the rib removed. Manufactured skin from .025 24ST and installed on wing, fastened to the first and second rib with #4 sheet metal screws. Three 4 lightning holes were cut in the new rib for inspection purposes and 8-32 nutplates were riveted to inside of rib for attaching of tip plate. The outboard ends of the ailerons were modified to conform to the chord length of the wing. The completed assembly is fabric covered upon covering of wing. The material for the Tip Plate is Prestwood T. and protrudes in a chordwise manner 1-3/4 .STC SA02007AKInstallation of main landing gear long step no. 3195.STC SA241CHInstall Ceconite 101 fabric.STC SA4629NMFabrication of Model 8400 brake booster assemblies, and modification of Scott Aviation Model B-711 brake master cylinders by installation of said assemblies.STC SA4-977Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA03112ATInstallation of Gomolzig Quietflight low noise silencer P/N PA-18-606500.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA02236AKFabrication and installation of F. Atlee Dodge Heavy Duty Standard Length Main Landing Gear, P/N 3225A, in accordance with F. Atlee Dodge Master Data List No. 3225-1.5, Revision: None dated March 14, 2005, or later FAA approved revisions.STC SA02234AKInstallation of a high Pressure Brake Master Cylinder assembly DCA1248-1260.STC SA1486GLFabricate and install engine mount to accept Continental Aircraft engine C-85-12 rated at 85 H.P. at 2575 RPM.STC SA1487GLFabricate and install engine mount to accept Continental Aircraft engine O-200 rated at 100 H.P. at 2750 RPM.STC SA1765GLFabricate and install engine mount to accept Continental Aircraft C90 and O-200 engines.STC SA5-65Installation of Goodyear 25 x 11.0 - 4 Type IV tires with tubes on Goodrich Model 841696 4-inch wheels on main landing gear, using Alaskan Aircraft Equipment Supply Model A-1 rim adapters
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