Cessna U206G
STCs that may be installed · 415
In force first, then newest. The registry doesn’t record which STCs an aircraft has.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('2073356', '2073315', '2073314')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
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, m.matched_model
FROM (
SELECT stc_number, min(matched_model) AS matched_model
FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
WHERE aircraft_model_code IN ('2073356', '2073315', '2073314')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_numberRun 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 SA01436SECockpit sunvisor retrofit kit.STC SA00312WIInstallation of 15 and 17-gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 61 or65 gallon capacity bladder tank or62 gallon fiberglass fuel tanks. (thru S/N U20604649)STC SA2343CEInstallation of standard range 62 gallon capacity or long range 77 gallon capacity fiberglass fuel tanks in place of original bladder fuel tanks.STC SA2380CEInstallation of fuel caps.STC SA2455CEInstallation of fuel inlets and caps. (U206G S/N U20604650 - U20606921)STC SA00887SEInstallation of vortex generators on the wings, tail surfaces, and vertical fin, in accordance with Micro AeroDynamics Drawing Package MA2146, Revision A, dated
March 11, 2004, and installed in accordance with Installation Manual MA2147, Revision IR, dated January 25, 2001 (for the 206 series) or MA2196, Revision IR, dated March 11, 2004 (for the 207 series), or later FAA approved revisions.STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA1817NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.STC SA5467NMInstallation of acrylic window liners. (206 SERIES 402B0301 AND ON)STC SA00473SEInstallation of SpeedbrakeSTC SA2163NMInstallation of the Precise Flight, Inc. Stand-By Vacuum System (SVS) in accordance with Installation Report 08074, Revision -, dated January 7, 2000, or later FAA approved revision.
NOTE: As a prerequisite to this change, the engine must be modified in accordance with Precise Flight, Inc. STC No. SE1780NM, dated April 21, 2000, or later FAA approved revision. Also, modified aircraft must be equipped with a vacuum indicator.STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA01077SEInstallation of fluoropolymer film.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC SA2382NMInstallation of Aileron and Flap Gap Seals.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC ST02547ATInstallation of a voice alert system.STC SA02198AK-DFabrication and installation of remote nose gear strut service port.STC SA10010SCInstallation of TCM IO-550 engine.STC SA1310SOReplacement and relocation of the Pre-select flap switch with a continuous input flap switch which allows simultaneous pilot operation of the throttle and flap controls.STC SA1005SCInstallation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA00709LAInstallation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.STC SA01456NYInstallation of Technisonic Industries Ltd OSAT-100 Airborne Position/Data Communicator.STC SA8406SW-DInstallation of S-TEC System 55/55X two axis automatic flight guidance system, Model ST-555STC SA2-1178Replacement of right front seat with stretcher.STC SA4599SWInstallation of an auxiliary engine driven vacuum pump system.STC SA7367SWInstallation of vacuum pump cooling shroud.STC SA8504SW-DInstallation of a Century automatic flight system, Model AK1021 consisting of a Century autopilot.STC SA09470SCInstallation of Starter Indicator light system.STC SA00426DEInstallation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat.STC SA8886SW-DInstallation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-556, with Optional Autotrim System.STC SA01079LAInstallation of Accessory Power Receptable in accordance with FAA Approved Master Drawing List, Document No. 206-APR-100, Rev IR, dtd 8/15/00 or later FAA approved revision.STC SA02277ATInstallation of a passenger seat. STC SA1335SO is a required part of this STC.STC SA00124DEInstallation of Oilamatic preoiler system.STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA01280CHInstallation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna 421C model, s/n 1017 thru 1404)STC SA00270WIInstallation of fiberglass replacement wing tips.STC SA2502CEInstallation of strut/wing and strut/ fuselage fairings, lightning hole covers, and aerodynamic putty.STC SA71GLInstallation of air filtersSTC SA3231NMInstallation of 14.9 gallon usable fuel-containing lighting resistant wing tips.STC SA4368WEInstallation of 14.9 gallon usable fuel-containing wing tips. (U206F, TU206F, U206G, TU206G LANDPLANES, SKIPLANES, FLOATPLANES)STC SA813NEInstallation of aft cabin storage utility box. (U206F, TU206F S/N U20601701 TO U20603521) (U206, TU206G S/N U20603522 and up) (206H, T206H S/N T2068001 and up)STC SA02003AKFabrication and installation of main gear gravel deflector kit no. GD6-200.STC SA09389AC-DInstallation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-837-20/30.STC SA00678SEInstallation of J. P. Instruments 8Jimline EGT-100 series primary instrumentsSTC SA00748WICertification of a repair kit for the rudder pedal torque tube assembly for the stowable rudder pedal installation.STC SA00512ATInstallation of either a Hartzell model PHC-C3YF-1RF/F7691(), PHC-C3YF-1RF/F8468A()-6R, PHC-J3YF-1RF/F7691(), or PHC-J3YF-1RF/F8468A()-6R and associated spinner assembly.STC SA01777ATInstallation of either a McCauley model D3A34C401/90DFA-10 or D3A34C402/90DFA-10 propeller and associated spinner assembly.STC SA2830SOInstallation of a Teledyne Continental Motors model IO-550F engine along with either a McCauley or Hartzell (various P/N's) propeller.
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