TCDS A-765

STCs approved under this data sheet · 532

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-765')
  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 SA00269BOInstallation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.Avidyne CorporationSTC SA3-134Installation of electric fuel boost pumps.Sabreliner Aviation LLCSTC SA3-252Radome installation.Sabreliner Aviation LLCSTC SA3-86RCA AVQ-50 radar antenna mount installationSabreliner Aviation LLCSTC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleVoiceFlight Systems LLCSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.J P InstrumentsSTC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemJ P InstrumentsSTC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsAerospace Logic Inc.STC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplayGarmin International IncSTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemLatitude Technologies CorporationSTC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemGarmin International IncSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverGarmin International IncSTC SA00281BOInstallation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000Avidyne CorporationSTC SA407CEInstallation of Hoskins Twilighter Mark III High Intensity Lighting System consisting of Model A Wing Tip Lights and Model D or Model P Tail Light.BF Goodrich AerospaceSTC SA97CEInstallation of Hoskins Supplemental High Intensity Position Light System consisting of Model A or B Wing Tip Lights, Model C or D Tail Lights with or without Model 1 or 2 Fuselage Lights.BF Goodrich AerospaceSTC 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).Icarus Avionics, LLCSTC 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.Universal CorporationSTC SA00290BOInstallation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXXAvidyne CorporationSTC SA02110CHInstallation of a Time Trac Data RecorderP2 IncorporatedSTC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.Electronics International Inc.STC SA2-433Installation of a carburetor air induction system.BlackHawk Aircraft Maintenance Inc.STC SA4-32Internal combustion heaters.Staggerwing Museum Foundation Inc.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.M-20 Oil Separators LLCSTC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeGarmin AT Inc.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemPrecise Flight IncSTC SA899EAInstallation of Grimes three-light strobe system as a supplemental light system.Honeywell International Inc.STC SA174CETwin-engine electronic sychronizer for aircraft equipped with Hartzell propellers.Ontic Engineering and Manufacturing Inc.STC SA250CEInstallation of Woodward electronic propeller synchraphaser system.Ontic Engineering and Manufacturing Inc.STC SA1708WERemoval of cargo door (approved under STC SA995WE) to permit aircraft to engage in special operations such as aerial photography, parachute jumping, etc.SOUTHWESTERN AERO EXCHANGE INC.STC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.K S Avionics IncSTC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.K S Avionics IncSTC SA01695SEInstallation of an antennaGarmin AT Inc.STC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)Aviation Development CorporationSTC SA1-398Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injectorStaggerwing Museum Foundation Inc.STC SA1-427Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injector per STC SE1-391, and takeoff weight increase to 9,800 lbs. and landing weight to 9,400 lbs. per STC SA2-820.Staggerwing Museum Foundation Inc.STC SA2-1230Installation of extended tail wheel assembly.Staggerwing Museum Foundation Inc.STC SA2-1246Increase in take-off Gross Weight to10,200 pounds and landing weight to9800 pounds. Extension of Aft. C.G. limits to +120.5 at 10,200 pounds.Staggerwing Museum Foundation Inc.STC SA2-1261Install Fiberglas bubble tail wheel enclosure doors (enclosing entire wheel).Staggerwing Museum Foundation Inc.STC SA2-204Installation of one-peice windshield and flush cockpit side-windows.Staggerwing Museum Foundation Inc.STC SA2-213Installation of modified wing tips.Staggerwing Museum Foundation Inc.STC SA2-280Increase in take-off weight to9800 pounds, and increase in landing weight to 9400 pounds, when P&W R-985-AN14B, or -AN4, -AN10 (modified per P&W Special Instruction No. 15F-45), or-AN1M1 (with NAR-9N-19 carburetor) modified per P&W Special Inst. No 15F-45 is installed.Staggerwing Museum Foundation Inc.STC SA2-328Installation of Hartzell propeller unfeathering crossfeed system.Staggerwing Museum Foundation Inc.STC SA2-338Installation of two (2) 25,000 BTU Janitrol Heaters installed one (1) in each wheel well.Staggerwing Museum Foundation Inc.STC SA2-383Raise horizontal stabilizer and installation of elevator seal assembly.Staggerwing Museum Foundation Inc.STC SA2-621Installation of Hartzell propellers, Model HC-93Z30-2C, -2D/10152-5 1/2, or HC-B3Z30-2D/10152-5 1/2.Staggerwing Museum Foundation Inc.STC SA2-622Approval of existing Jack and HeintzA3A autopilot installation.Staggerwing Museum Foundation Inc.STC SA2-623Approval of existing installation of47 gallon nose fuel tanks.Staggerwing Museum Foundation Inc.STC SA2-625Delete righthand rudder tab and system; install rudder control system bungee and shut-off valve.Staggerwing Museum Foundation Inc.STC SA2-686Installation of Fiberglas Nose.Staggerwing Museum Foundation Inc.STC SA2-725Installation of oil cooler, G & O Mfg. Co. #E703, modified with Fullerton Syphon DV5 thermostat.Staggerwing Museum Foundation Inc.
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