Beech H35
STCs that may be installed · 480
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 ('1151520')
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 ('1151520')
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 SA997SOInstallation of a single-piece sloped windshield.STC SA975SWInstallation of cabin air conditioner.STC SA6067NMInstallation of an auxiliary cabin door latch pin and socketSTC SA8031SWInstallation of Zeftronics alternator controller unit P/N R15100 or R15V00.STC SA5926NMInstallation of manifold pressure instrument.STC SA4317NMInstallation of an oil filter, filter base and mounting plate on the fire-walls of those airplanes listed on AML No. SA4317NM that are equipped with an FAA approved Continental Model 0-470 engine installation which has been modified by the installation of an external mounted full flow oil adapter and spin-on oil filter.STC SA4321NMInstallation of an oil filter, filter base and mounting plate on the firewalls of those airplanes listed on AML No SA4321NM that are equipped with an FAA approved Continental model IO-470 engine installation which has been modified by the installation of an external mounted full flow oil adapter and spin-on oil filterSTC SA5932NMInstallation of 100 watt light bulb system.STC SA1626NM PAGE 1Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series)STC SA5886NMLimited to installation on serial number D-5156 ONLY.STC SA1802CEInstallation of Total Flood Corporation fire extinguishing system in the cabin and/or fire extinguishant system in engine compartment.STC SA5159NMInstallation of chip detector system.STC SA4392WPInstallation of a standby pressure system, standby vacuum system or standby electrical system.STC SA2844CEInstallation of a plastic cap enclosure over the anti-collision strobe light system.STC SA300CEInstallation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO)STC SA1583GLInstall Aero Fabricators shoulder harness and seat belt assembly.STC SA4094NMInstallation of Oilamatic engine preoiler.STC SA7128SW-DInstallation of S-TEC system 60 two axis automatic flight guidance system Model ST-010 with Optional Automatic Electric Trim SystemSTC SA2512NMInstallation of Silver Instruments Fueltron IG-RS, IP-RS, IL-RS,IK-RS or Fuelgard R fuel flow indicating system.STC SA2350NM PAGE 1Installation of Electronics International Inc digital carburetor/outside air temperature gaugesSTC SA4721NMInstallation of SynCon alarm system.STC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.STC SA2501CEInstallation of Bendix/King MLS-21Microwave Landing System.STC SA2305CEInstallation of Sperry MLS-910Microwave Landing System.STC SA3862NM PAGE 1Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.STC SA2081WEInstallation of Madras Air Service P/N MAS 102 wing tips.STC SA2798NMInstallation of modified exhaust heat muffler.STC SA2771NMInstallation of photovoltaic battery charging system.STC SA660WEInstallation of HRD-type fire extinguishing system. (AND STC SA111WE)STC SA695CEInstall Frantz oil filter.STC SA5162SW-DInstallation of S-TEC yaw damper system Model ST-135.STC SA7129SW-DInstallation of S-TEC system 65 two axis automatic flight guidance system Model ST-391.STC SA3506NMInstall a Continental IO-470-N engine, McCauley 2A36C23/84B-0 propeller, Duke Astronautics fuel boost pump and miscellaneous partsSTC SA4-1245Installed Flightcraft ski bag compartment.STC SA1455NMInstallation of a flame proof auxiliary heater-dryer, Model12-1600.STC SA1-636Install 300 Series dry vacuum pump conversion kits.STC SA1822CEInstallation of airborne auxiliary dry air pump.STC SA2580NMInstallation of Continental I0-470-N engine and McCauley 2A36C23/84B-0 constant speed propeller.STC SA5391SW-DInstallation of S-TEC manual electric trim system, Model ST-321.STC SA1826NMInstallation of Safe Flight model SC-150 lift detector system.STC SA2660NMInstall a Teledyne continental IO-470-N engine, a McCauley 2A36C23/84B-0 Propeller, and miscellaneous partsSTC SA1644SWInstallation of Mitchell automatic flight system Model AK415 consisting of Century IIB autopilot with optional radio couplerSTC SA1269SWInstallation of Mitchell automatic flight system Model AK328 consisting of Century I autopilot with optional omni tracking system.STC SA824SWInstallation of Mitchell automatic flight system Model AK248 consisting of Century II autopilot with optional radio coupler.STC SA93GLInstall left hand side window, P/N W-2048 or W/T-2048.STC SA94GLInstall right side door window,P/N W-2049 or W/T-2049.STC SA754SWInstallation of Mitchell automatic aileron stabilizer Model AK203.STC SA2189NMInstallation of a Continental IO-470-N engine, Beech 278-100-208-82 propeller, Beech 36-380061-1 mixture control, Beech 35-910293 air inlet duct, Beech 35-380021 fuel flow gauge and associated systemsSTC SA3172SW-DInstallation of Mitchell Yaw Damper System Model YK631.STC SA1418SOReplacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations)
Back to Beech H35