Beech E35
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 ('1151512')
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 ('1151512')
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 SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA02121SEInstallation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic SystemSTC SA01110CHInstallation of wing fuel tank quick valve drains.STC SA999WEInstallation of a Jasco #6540-1 (35a.) Alternator Kit or Jasco #6555-1 (50a.) Alternator KitSTC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleSTC SA00789LAInstallation of Clear View Sunvisor.STC SA02015SE-DInstallation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.STC SA04165CHInstallation of an Enhanced Exhaust System, D Shannon Products, Ltd. kit DSP-KIT-15-009STC SA1150WEInstallation of Brittain Industries, Inc. Installation Modification Kit #11977 (relocation of gyro sense element to remote position)STC SA269WEInstallation of Brittain/Beech Pneumatic Pitch Assist Model PC-1STC SA322WEInstallation of Brittain/Beech Pneumatic Pitch Assist M del PC-1STC SA323WEInstallation of Beech Pneumatic Pitch Assist Model PC-1STC SA4-1260Installation of Brittain/Beechcraft AutopilotSTC SA4-716Installed Brittain/Beech Autopilot in accordance with Brittain Industries, Inc. Installation Manual 11905-1 (Aileron only) or Brittain/Beech AutopilotSTC SA662WEInstallation of Brittain Industries, Inc., Model B1-400 Hi-Lo Sensitivity AdaptorSTC SA533WEInstallation of Brittain/Beech Model B4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold, and NAV-1 Navigational CouplerSTC SA631WEInstallation of Brittain/Beech Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold, and NAV-1 Navigational CouplerSTC SA677WEInstallation of Brittain/Beech Model B-4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.STC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemSTC SA2361SWInstallation of Continental IO-470-N engine and McCauley 2A36C23/84B-0, or 2A37C223/90RB-6, or Beech 278-100-11/278-214-82, or 278-100-13/278-214-82, or Flottorp F12A-3/8400-2 propellerSTC SA153EAInstall Beryl D Shannon Aviation Specialties, Inc. 15-gallon Tip Tanks B1400-01, -02, Rev. B, dated 8-15-78* or D Shannon Products, Ltd. 20-gallon Tip Tanks Part List DLB1400, Rev. E, dated 9-17-10STC SA1476WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemSTC SA02460CHInstall Genesis Aero, LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanksSTC SA2633WEInstallation of enlarged window and baggage compartment.STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplaySTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemSTC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemSTC SA5721NMInstallation of replacement cockpit control knobs for throttle, mixture, propeller,parking brake, heater, cowl flaps.STC SA5156NMFabrication and installation of Pulsar-MOSFET Landing Light Flasher SystemSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverSTC SA02434NYInstallation of a Digital Engine Monitoring system.STC SA2375CEInstallation of B&D Instruments & Avionics, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 0535-003-011, Rev. B, or later FAA Approved revision; and (2) copy of this certificate.STC SA09337SCAn increase gross weight of 100lbs for Beech models A35, B35, C35, D35, E35, F35, G35, and 35R when equipped with Vortex Generators per J.V.E., Inc., STC SA09145SC.STC SA1584CEInstallation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.STC SA1650CEInstallation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8, 1981, or later.STC SA1703CEInstallation of flap and aileron fairings and seals.STC ST01494LAInstallation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA, or later FAA approved revisions. No flight manual is required.STC SA1-368Installation of auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company s Manual SFE-35(III) dated July 15, 1959, Tip Tank Installation, Type III Kit, utilizing parts listed on Bamber Wing Tanks Type III Kit Contents dated July 15, 1959.
This wing tip tank installation may be used in combination with either the wing auxiliary tanks or a baggage auxiliary tank, but not when both are installed. Complete installed weight empty is 23.7 lb. at 89.1 inches. The CG of the tip fuel is 87.0 inches.STC SA144EAApproval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing Solenoid Fuel System (ref STC SAl-303 dated February 20, 1959). No wing or baggage compartment auxiliary tanks are permitted with this system. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. D dated February 15, 1964 is required.STC SA181EAApproval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG, RBI-IDOL) Fiberglass wing tip fuel tanks (ref STC SA3OEA, Configuration 2 or 3) and Type II or III Kit transfer fuel system. This system eligible with Beech 20 gal wing aux. tanks or baggage compartment tanks, but not both. This STC also places the above aircraft in the Normal and Utility categories, using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders, Inc. Installation Manual FEI-35 (4A) Rev. C dated February 15, 1964 is required.STC SA23EAInstallation of Third Cabin Window on both sides of Fuselage in accordance with Glenn Floyd Stauffer Drawing Nos. 42601, Revision A dated 31 May 1962 and 42602, Revision A dated 13 June 1962.STC SA2653SWInstallation of Instrument Panel in accordance with 1998-54 Installation Manual and Drawings 1998A200, 1998A300, 1998A400, and 1999 all dated July 1, 1977; Battery Box Kit per 1998-84 Installation Manual and Drawing 2000 dated July 1, 1977; Radio Cooling Kit per 1998-86 Installation Manual and Drawing 2002 each dated July 1, 1977.STC SA2771WEInstallation of Long Fiberglass tailcone to replace the short factory installed tailcone in accordance with FAA Sealed N.E. Coote Tool and Machine Drawing List Report No. 1 dated September 2, 1970.STC SA28EAInstallation of 12-gallon fiberglass wing tip fuel tanks.STC SA30EAInstallation of 13.5 gallon fiber-glass wing tip tank assembly.STC SA808SOInstallation of Beryl D Shannon Aviation Specialists, Inc., Fiberglass tip tanks (15 gallons each) and fuel transfer system in accordance with Beryl D Shannon Aviation Specialists, Inc., Installation Kit Drawing KB1401, Rev E, dated May 19, 1977, or later FAA approved revisions. Drawing KB1401 Revision F, dated April 12, 1979, includes optional wing-tip anti-collision light installation. This STC requires operation in the Normal Category.STC SA930SOInstallation of Beech Aircraft wing tip assemblies in accordance with Beryl D Shannon Aviation Specialties, Inc., Drawing B1990, dated December 15, 1976, or later FAA approved revision.STC 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).
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