TCDS A31EU

STCs approved under this data sheet · 161

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 = 'A31EU')
  ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number"

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STC SA00420SEInstallation of a II Morrow Apollo SL50 TSO C129 Class A(2) GPS Navigation Receiver and TSO C37d, C38d, and C128 VHF Airband Communications Transceiver, in accordance with Master Drawing List P/N 560-0966-00, Revision -, or later FAA approved revision.Garmin AT Inc.STC SA00328SEInstallation of a II Morrow Apollo 2001 series TSO C129/C115b Navigation Management System, in accordance with the applicable data listed on the FAA AML, dated May 14, 1996, or later FAA approved revisions.Garmin AT Inc.STC SA00401SEInstallation of a II Morrow Apollo Model 360 MAP display in accordance with the applicable data listed on the attached FAA Approved Model List, or later FAA approved revisions.Garmin AT Inc.STC SA00421SEInstallation of a II Morrow Apollo Model SL40 TSO 37d, C38d, and C128 VHF Airband Communications Transceiver, in accordance with Master Drawing List P/N 560-1002-00-00, Revision -, or later FAA approved revision.Garmin AT Inc.STC SA00464SEInstallation of a II Morrow Apollo Model GX-55 TSO C129 Class A2 GPS for Supplemental IFR Enroute, Terminal, Remote/Oceanic or VFR navigation in accordance with the applicable data listed on the Master Drawing List, II Morrow P/N 560-1000-00, Revision -, and Airplane Flight Manual Supplement, P/N 560-1009-00, Revision -, or later FAA approved revisions.Garmin AT Inc.STC SA00504SEInstallation of the II Morrow s Global Positioning System (GPS) Model GX50 or GPS/Comm Model GX60, per II Morrow Master Drawing 560-0970-00, Revision -, dated December 15, 1997, or later FAA approved revisions; or installation of the II Morrow GPS Model GX50 or GPS/Comm Models GX60 or GX65, per II Morrow Master Drawing 560-0970-01, Revision -, dated June 23, 1998, or later FAA approved revisions.Garmin AT Inc.STC SA3535NMInstallation of the Apollo II Model 612 Loran C navigation system.Garmin AT Inc.STC SA3806NMThe Apollo II Model 612A Loran-C navigation system is installed in Partenavia P68C aircraft in accordance with II Morrow Top Level Drawing MC0050, Revision A, or later FAA approved revisions. This installation includes a dedicated CDI and annunciator panel for the Loran 1 receiver and provides steering signals to the autopilot. This STC allows II Morrow s participation in the FAA sponsored, limited implementation program for evaluating the use of Loran-C during non-precision approaches.Garmin AT Inc.STC SA5699NMnstallation of a II Morrow Navigation Management System (NMS) consisting of two Apollo Model 2001 Navigation Management Computers, two Apollo Model 2010 Multi-Chain Loran-C Sensors, one Apollo Model 2020 Global Positioning System (GPS) Sensor, one Apollo Model 2030 Fuel/Air Data Sensor, and one Apollo Altitude Encoder, in accordance with II Morrow Apollo NMS Document PD0433, Revision B, dated March 20, 1992, Revision C, dated May 22, 1992, or later FAA approved revision.Garmin AT Inc.STC SA5718NMInstallation of a II Morrow Flybuddy GPS navigation receiver, Model 819, 820, or 820+ in accordance with II Morrow VFR STC Data, Flybuddy GPS, Document Number 560-0901, Revision -, Revision A, or later FAA approved revision.Garmin AT Inc.STC SA5719NMInstallation of a II Morrow Flybuddy Loran-C navigation receiver, Model 800 or 800+ in accordance with II Morrow VFR STC Data, Flybuddy Loran, Document Number 560-0905, Revision -, Revision A, or later FAA approved revision.Garmin AT Inc.STC SA5904NMInstallation of a II Morrow Apollo 2001 Navigation Management System, in accordance with the applicable data listed on the attached FAA AML SA5904NM, or later FAA approved revision.Garmin AT Inc.STC SA00165BOInstallation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.Avidyne CorporationSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.M-20 Oil Separators LLCSTC SA09470SCInstallation of Starter Indicator light system.Texas Skyways IncSTC SA02168AKInstallation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.Avalaska IncSTC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.Aero Manufacturing Inc.STC SA00804SEInstallation of an engine failure indicator system, also referred to as a 'low Thrust Detector system.'Advanced Aero Safety Inc.STC SA71GLInstallation of air filtersBrackett Aero Filters Inc.STC SA1784CE-DInstall KAP 150 three axis or KFC 150 three axis flight control system with optional KAS297B vertical speed and altitude selector.Honeywell International IncSTC SA1007NWInstallation of a low thrust detector system.Engine-Out Warning Systems, LLCSTC SA157NEInstallation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent.Insight Instrument CorpSTC SA09000AC-DInstallation of S-TEC System 55 two axis automatic flight guidance system, Model ST-585, with optional autotrim system.S-TEC CorporationSTC SA00061LAInstallation of JPI digital tachometer.J P InstrumentsSTC SA5656NMInstallation of burglar alarm system.Thompson Harold SSTC SA1626NM PAGE 2Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series)Electronics InternationalSTC SA5159NMInstallation of chip detector system.Northwest Aircraft IncSTC SA300CEInstallation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO)Woodward Governor CompanySTC SA688NEInstallation of Safeway Model 6900 deicer boot.Safeway Products, IncSTC SA2350NM PAGE 1Installation of Electronics International Inc digital carburetor/outside air temperature gaugesElectronics InternationalSTC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.Electronics InternationalSTC SA5282SW-DInstallation of S-TEC System 60 single axis automatic flight guidance system, ST-077.S-TEC CorporationSTC SA3862NM PAGE 1Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.Electronics InternationalSTC SA5236SW-DInstallation of S-TEC System 40/50 single and two axis automatic flight guidance system, Model ST-221-40/50.S-TEC CorporationSTC SA7127SW-DInstallation of S-TEC System 65 two axis automatic flight guidance system, Model ST-386.S-TEC CorporationSTC SA3747NMInstallation of a Janitrol cabin heater Model B4050.Marple Aviation, IncSTC SA1247GLInstallation of a winshield heat panel, P/N 1513470-2(P.P.G. Aircon).Joliet Avionics, IncSTC SA5175SW-DInstallation of S-TEC System 60 two axis automatic flight guidance system Model ST-078, with optional automatic electric trim. system.S-TEC CorporationSTC SA779GLInstallation of a Dynamic Air Eng. air conditioning system.Joliet Avionics, IncSTC SA5256SW-DInstallation of S-TEC manual electric elevator trim system, Model ST-160.S-TEC CorporationSTC SA3433SW-DInstallation of Century Automatic Flight System Model AK937 consisting of a Century 21 autopilotCentury Flight Systems IncSTC SA3070SW-DInstallation of Mitchell automatic flight system model AK426 consisting of Century I autopilot with optional omni tracker.Century Flight Systems IncSTC SA3067SW-DInstallation of Mitchell automatic flight system model AK511 consisting of Century III autopilot with optional radio coupler and glide slope coupler.Century Flight Systems IncSTC SA3068SW-DInstallation of Mitchell automatic flight system model AK510 consisting of Century IIB autopilot with optional radio coupler.Century Flight Systems IncSTC SA3069SW-DInstallation of Mitchell automatic flight system model AK539 consisting of Century IV autopilot or AK539FD, consisting of Century IV flight director autopilot with optional remove annunciator.Century Flight Systems IncSTC SA687GLInstallation of a Dynamic Air Engrg. air conditioning system.Joliet Avionics, IncSTC SA2190NM PAGE 2Installation of electronics International Digital Volt/Amp Gauges and Accessories.Electronics InternationalSTC SA5262SW-DInstallation of S-TEC System 60 pitch stabilizer System Model ST-079 with optional automatic electric trim system.S-TEC CorporationSTC SA3399SW-DMitchell automatic flight system AK902 consisting of Century III autopilot with optional radio coupler and glide slope coupler.Century Flight Systems IncSTC SA3419SW-DMitchell automatic flight system AK892 consisting of Century 31 autopilot.Century Flight Systems Inc
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