Summa 369D
STCs that may be installed · 275
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 ('056266I')
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 ('056266I')
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 SR01581SEFabrication of AMC Part Number AM369D25201 input shaft sleeve assembly.STC SR01605SEFabrication of Aircraft Manufacturing Company (AMC)
Part Number AM369H2039-501/-502 oil cooler access door assemblySTC SH493GLInstallation of a Shadin Co. Digital fuel flow indicating system, a temperature compensated digital fuel flow system, or a temperature compensated digital fuel quantity and fuel flow system.STC SH631NEInstallation of Fibre Reinforced Plastic Interior Trim Panels and Ducting.STC SR00932LAInstallation of Apical emergency float kit, p/n 20491.STC SR02181NYInstallation of an Air Box INspection Panel.STC SR01574SEFabrication of Camera MountSTC SR01430LAInstallation of Stainless Steel Skid shoes.STC SR01104SEFabrication of AMC AM369D21800-501 Tail Rotor Pitch Control AssemblySTC SR01136SEFabrication of AMC AM369A6200-45, -46, -57, -58 Landing Gear Fillet Fairings and AM369H6200-73, and -74 Landing Gear Fairing Guides per AMC Master Drawing List No. MDL-AMC-003, Rev A, dated August 29, 2002 or later FAA approved revision; and installation of this assembly in accordance with the Maintenance Manual for the rotorcraft, document number CSP-HMI-2, Rev 21, or later FAA approved revision.STC SR01171SEFabrication of AMC AM369H8092 engine cooling duct orificeSTC SR01172SEFabrication of AMC AM369H8064 cabin vent valve housing assembly in accordance with AMC Master Drawing List No. MDL-AMC-011, Revision A, dated November 11, 2002, or later Federal Aviation Administration (FAA) approved revision. The housing assembly must be installed in accordance with AMC Installation Instructions MI-02004, Revision IR, dated November 15, 2002, or later FAA approved revision.STC SR01204SEFabrication of AMC AMC369H92827 pin, clevis-rotor brakeSTC SR01210NMFabrication of AMC AM369D23670 horizontal stabilizer tip plates in accordance with AMC Master Drawing List No. AMC-004, Revision C, dated March 25, 2003, or later Federal Aviation Administration (FAA) approved revision. The tip plates must be installed in accordance with AMC Installation Instructions MI-02001, Revision IR, dated November 6, 2002, or later FAA approved revisionSTC SR01265SEFabrication of AMC Part Number AM369D25707-13 oil cooler tube assemblySTC SR01363SEFabrication of AMC Part Number AM369D21308 main rotor spacer in accordance with AMC Master Drawing List No. MDL-AMC-016, Revision A, dated June 30, 2003, or later Federal Aviation Administration (FAA) approved revision. The main rotor spacer must be installed in accordance with AMC Installation Instructions AMC MI-03005, Revision IR, dated March 24, 2003, or later FAA approved revision.STC SR01682LAInstallation of cargo rackSTC SR00452NYInstallation of E.M. Heli-Logistics Engine Air Inlet Diverter.STC SH1510SOInstallation of external cargo rack and work platform between the skid gears. Limited to installation on serial number 911079D.STC SH3233SOIntallation of Airborne spray system.STC SH390NWInstallation of an electronic weighing system, for monitoring cargo hook weight, in accordance with Measurement Systems International, Inc., Installation drawing No. D00327, Sheets 1 and 2, or Drawing D00473, Rev. E.STC SR00811NYInstallation of Technisonic Industries Limited TFM-138 series transceiver models.STC SR09172RCInstallation of a replacement main rotor blade without a leading edge abrasion strip, part number 500P2100-BSC and BS-1 per Helicopter Technology Company (HTC) Maintenance Manual HTCM-001 latest FAA approved revision.STC SR01834NYInstallation of Globalstar Satellite Telephone System.STC SH980NEInstallation of a Heli-Logistics Ltd. P/N HL92116 engine upper firewall.STC SR01282LAInstallation of a tail rotor blade assembly.STC SR09213RCInstallation of a replacement tail rotor blade.STC SA2294SOInstallation of seat access panel in accordance with ALM Technologies, Inc., Drawing List, Document No. 3698001, dated August 21, 1987, or later FAA approved revision.STC SH1528NMInstallation of Freon Compressor Air Conditioning System in accordance with Aero Engineering Corporation Drawing List, DL-9, FAA approval dated November 26, 1982, or later FAA approved revision.STC SR01427LAInstallation of Teledyne Battery Products G-641 and G-641S lead-acid battery.STC SR00716SEInstallation of Concorde RG500 battery in accordance with Aero-Jet Trading 'Installation Instructions Concorde Battery Hughes 500 & MD369 Series Helicopter' Manual Number AJ-369, Revision New, dated May 18, 1999, or later FAA approved revision.STC SH1258SOInstallation of Utah Research and Development Co. Model 124BC101 battery charging system.STC SR00409SERapid removal door system hinges, installed in accordance with Certified Technology Installation Instructions CT9602-1, Revision C, dated January 1, 2000, or later FAA approved revision and manufactured in accordance with Certified Technology Drawing List CT9602, Revision E, dated January 10, 2000, or later FAA approved revision.STC SR00125BOInstallation of a Pratt & Whitney Engine Services, Inc.-Honeywell IntelliStart Plus+TM Electronic Control System P/N DPU-K-010STC SH115NEInstallation of Casey shroud heater P/N 250-CCA-H500.STC SR01169LAInstallation of Aerometals High Speed Acturator Assemblies, P/N 369X27001STC SH849NEInstallation of Utility Equipment Kit consisting of Cargo Mirror, Bearpaws and Bubble or Wedge Door Windows.STC SR01346NYInstallation of Navigation Lights with Vancouver Island Helicopter Master Document List V500-300-MDL, Rev 1, dated February 14, 2001.STC SR00981LAInstallation of landing gear strut assemblies.STC SH201WEInstallation of stirrup assemblies to directional control pedals for operation by handicapped pilot. (US ARMY OH-13E 205A)STC SR09260RCInstallation of forward door and aft door bubble type windows.STC SH5055NMInstallation of Aerometals tailboom, P/N 369X23500-505, 507; or installation of Yehnert tailboom P/N YH-228-X as replacements for MDHI tailboom P/N 369D23500-Y.STC SR00469SEInstallation of engine air inlet particle separator.STC SR01062LAInstallation of Aerometals exhaust tailpipe outlet hangar assemblies, P/N 369X8236.STC SR01041LAInstallation of engine compressor inspection panel in accordance with Installation Instructions RDE 109-20, Rev A, dated 5/10/00, or later FAA approved revisions.STC SR00974LAInstallation of Aerometals Low Speed Actuator Assemblies, P/N 369X7014.STC SH184NWInstallation of Chadwick C-500 aerial spray systemSTC SH567NWInstallation of tanks, pumps, and spray nozzlesSTC SH667NWInstallation of an auxiliary fuel tank in the aft passenger compartment.STC SH654ALInstall Airglas Model L2700-369HD skis.
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