TCDS 1A16
STCs approved under this data sheet · 183
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 = '1A16') 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 = '1A16') 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 SA1571SOInstallation of Duke Solid Chemical Dispersal System in accordance with Duke Drawing Number 10102, dated September 21, 1983, or later FAA approved revisions.STC SA03029CHInstallation of Honeywell Engine Model TPE-331-1-151A with a Hartzell HC-B3TN-5M/T10282N+4 model propeller in accordance Project Report Number JTC2010ST001, Revision NC, date March 3, 2011, and submitted previously FAA Approved data accomplished under Federal Aviation Administration (FAA) Field Approval process.STC SA4942SWInstallation of Vortex control wing tip in accordance with Frakes Aviation Drawing No. FA-7042 dated 11/24/82, or later FAA approved revision.STC SA02985CHInstallation of a Cool Start System in accordance with Installation Instructions , Revision A, dated April 14, 2011, or later FAA Approved revision.STC SA2700SWInstallation of geared elevator tab according to Drawing FA-7023, Revision F, dated 11/28/77, Sheets 1 through 3; E.O. s FA-7023G dated 1/23/78; FA-7023H (6 sheets) dated 3/24/78, or later FAA approved revision.STC SA2747SWInstallation of lockable, full swivel tail wheel per Drawing FA7027H, dated 5/11/78, or later FAA approved revision.STC SA3522SWRemoval of the three degree offset from the vertical stabilizer, addition of the airfoil shape to the top of the horizontal stabilizer, and move of the turbine aft by 13 inches in accordance with Drawing Numbers 7061, 7062, 7063, and Drawing List No. 70001 revised 10/10/85.STC SA3528SWInstallation of airfoiled horizontal stabilizer and straightening of the vertical fin in accordance with Frakes Drawing List 70002 dated 10/31/85, or later FAA approved revision.STC SA4003SWAddition of servo-tabs to upper ailerons according to Drawing FA 7039, Sheets 1 and 2, dated 5/15/79, or later FAA approved revision.STC SA4035SWManufacture and installation of Frakes Aviation PN FA 7040-2 Cockpit Air Inlet Scoop according to Drawing FA 7040 dated 8/10/79 and Installation Instructions.STC SA4941SWInstall two additional 17 gallon fuel tanks in each upper wing in accordance with Frakes Aviation Drawing Number 7045.STC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA02786CHInstallation of a Single Point Ground Fueling SystemSTC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.STC SA4172NMInstallation of Aviation Development oil filter.STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA00173DEInstallation of Oilamatic preoiler system.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA7987SWInstall Garrett TPE 331-1-151A, -151G, or -151K engine and Hartzell HC-B3TN-5/T10282(-0 to +4) propeller. Approved for model G-164B (serial numbers 1 through 827B)STC SA241CHInstall Ceconite 101 fabric.STC SA01353CHInstallation of Walter a.s. turboprop engine model M601E-l l or M601D-l l with the AVIA Propeller
Ltd.
model V510AG, V508E-AG/99 or V508E-AG/106 in accordance with Turbine Conversions Drawing List,
Report 3100, Revision C, dated August I, 2005, or later FAA approved revision.STC SA436NWInstallation of WAC-2D30-425/AG-100-4S propeller assemblySTC SA99NWInstallation of Efficiency Aircraft Components, Inc. propeller
blades and Hamilton Standard hubs on G-164 series aircraft.STC SA2683NMInstallation of Precise Flight, Inc. stand-by vacuum system (SVS)STC SA01639NYReplacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.STC SA2384NMInstallation of Pacific Propeller, Inc. 22D40/AG200-2 and 22D40/6533A-12 propellers, governors, and associated systems on Pratt & Whitney R-1340 series engines in accordance with FAA sealed Pacific Propeller, Inc. Installation Instructions No. 8002 and 8003, respectively.STC SA434NWInstallation of EAC-12D40-AG-100S-4S prop on Pratt & Whitney R-1340-AN-1 engine.STC SA445NWInstallation of EAC-22D30-AG-200-4S prop or P&W R-985-AN-1 engine.STC SA8075SWInstallation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER)STC SA01258SEInstallation of the Automatic Flagman Dispenser Models in accordance with Automatic Flagman Master Drawing Lists specified in attached AML, or later FAA approved revision.This STC supercedes several existing STC s as listed in the notes on the attached AML.STC SA01295LAInstallation of modified Pratt & Whitney R-1340 engine. This mod must be done concurrently with STC SE01200LA which modifies R-1340 engine.STC SA1008WEInstallation of Poly-Fiber covering material.STC SA01236CHInstallation of Motorlet Walter M601E-11 turbine engine with an AVIA-Hamilton Standard VJ8.510 or VJ8.510AG model propeller.STC SA1257GLSurrendered and incorporated into STC SA241CH.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA02440ATRemoval of chemical hopper tank and installation of 2-place passenger bench seat and associated restraint system. Must be operated under Restricted Category operating limitations of FAR 91.313. A placard which states 'Never Exceed Speed (Vne) = 132 mph' must be installed in full view of pilot.STC SA00622LAInstallation of an electronic digital engine tachometer horizon model P-1000.STC SA1295WEInstallation of Automatic flagman Model no 4, marker dispensing unit.STC SA02168AKInstallation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA693CEReplace existing engine induction air filter with AC Spark Plug filter.STC SA71GLInstallation of air filtersSTC SA1282SWInstallation of Jacobs-Page R-755SM engine and Grumman 5404/M96K propeller.STC SA00506SEInstallation of an AlliedSignal TPE331-1-151G turboprop engine and a Hartzell HC-B3TN-5E/T10282+4 propeller. (Restricted Category)STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA2-952Installation of fiberglass covering.STC SA4772NMInstallation of Lund Flying Service forward spray boom.
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