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 SA00432SEInstallation of EGT 701 series fuel flow instrument.STC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemSTC SA2660SWInstallation of Continental IO-470-N engineSTC 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 SA09074SCInstallation of vortex generators on wing upper surface and vertical stabilizerSTC 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 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 SA00281BOInstallation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000STC SA02434NYInstallation of a Digital Engine Monitoring system.STC SA2373CEInstallation of B&D Instruments & Avionics, Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics, Inc. Installation Manual Part No. 0535-003-008, Rev. B, or later FAA Approved revision; and (2) copy of this certificate.STC SA1416CEInstallation of flap and aileron fairings and seals.STC SA1585CEInstallation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.STC SA1649CEInstallation of either the tail safe support angles or a stub spar at the 3% chord station on the root rib of horizontal stabilizer.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 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).STC SA838SOInstallation of Beryl D Shannon Aviation Specialties, Inc., Fiberglass Air Scoops (Inlet and Exit) in accordance with DLB 1500 dated June 6, 1974, or later FAA approved revision for the following models:
T. C. A-777: Models A35 through C35, 35 and 35 R
T. C. 3A15: Models H35 through V35STC SA942SOInstallation of Adjustable Directional Trim Device on lower aft fuselage (ventral Location) in accordance with Beryl D Shannon Aviation Specialties, Inc., drawing B15001, dated May 30, 1977, or later FAA approved revision.STC SA2219WEInstallation of Filtrator Company Engine Crankcase Breather and Vacuum Pump Air-Oil Separator in accordance with the applicable FAA sealed drawing listed on the attached Master Eligibility List Number SA2219WE.Installation of Filtrator Company engine crankcase breather and vacuum pump air-oil separator.STC SA2653WEInstallation of Beryl D Shannon Aviation Specialties Engine Crankcase, Breather, and Vacuum Pump Air-Oil Separator in accordance with the FAA approved drawing lists shown on the attached Master Eligibility List Number MEL-2014 dated November 1, 1976, or later FAA approved drawing lists.STC SA884SOInstallation of exhaust silencers in accordance with Beryl D Shannon installation instructions for Part Number 1010-1 and 1010-2, Rev. A, dated 2-2-76, or for Part Number 1010-3 and 1010-4, Rev. B, dated 2-10-76.
The exhaust silencer is manufactured in accordance with Beryl D Shannon Drawing No. 1010, Rev. B, dated 2-2-76.STC ST00961LAInstallation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated
June 26, 2000, or later FAA approved revisions.STC SA09256SCIncrease in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.STC SA1691GLInstallation of McCauley Propeller Model 3A34C423/90DFA-10 in accordance with D Shannon Drawing No. 533420, Revision C, dated October 26, 1991, or later FAA Approved revision.STC SA197NWInstallation of Clark three- light gear position indicator system.STC SA2870WEInstallation of right and left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB-1301 or later FAA approved revision.STC SA414CHReplace Beech lower cowling access panels with D'Shannon Products part numbers J1101-1 (left hand side)and J1101-2 (right hand side).STC SA4196SWInstallation of one piece windshield according to Blue Star Conversion One Piece Windshield Installation, Rev. 2, dated 3/28/80, or later FAA approved revision.STC SA686CEInstallation of Continental IO-520-B engine derated to power shown in the appropriate Airplane Flight Manual Supplement and Hartzell HC-C3YF-1/8468A-8R (Low 10.0 .2, High 36.0 1.0 Blade Angle Stop at 30 inch Sta.) propeller or McCauley 2A36C23/84B-2 (Low 13.3 , High 29.7 Blade Angle Stop from Ref. Sta. 30) propeller in accordance with AeroStol drawing 3100B, Sheet 1, Rev. B, dated 11/15/75 and 3100, Sheet 2, dated 9/18/75, or later FAA approved revisions, for all of the above Beech model aircraft, except Model G33. For Model 33 installation of the Continental IO-520-BB engine derated to the power shown in the appropriate Airplane Flight Manual Supplement and McCauley 2A36C23/84B-O (Low 13.3 , High 29.7 Blade Angle Stop, Ref. Sta. 30) propeller in accordance with D Shannon Products Drawing G3M2686BB, Rev. 1, dated 2/27/86 (5 sheets), or later FAA approved revisions.
For Model H35 installation of the Continental IO-520-BB engine derated to the power shown in the appropriate Airplane Flight Manual Supplement and McCauley 3A32C406/82NDB-2 propeller in accordance with D Shannon Products Drawing H353A32C406BB Rev. 1, dated 11/25/86 (5 sheets), or later FAA approved revisions.STC SA01165CHInstall cooling air baffle on Raytheon (Beech) aircraft Model H35, J35, K35, M35, N35 and P35 or aircraft Model A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, 35-33, 35-A33, 35-B33, 35-C33, E33, and F33 which are modified by STC SA2660SW, SA5635SW, SA5527SW, SA238GL, SA893WE, or SA2361SW to use Teledyne Continental Motors engine Models IO-470-C, or IO-470-N, in accordance with Castlegar Trust L. L. C. Installation manual as listed on AML No. SA01165CH, or later FAA Approved revisions.STC SA1315WEInstallation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.STC SA01085SEInstallation of BAS, Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE, dated May 13, 2002, or later FAA approved revision.STC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA00290BOInstallation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXXSTC SA01085LAInstallation of the VNS 1000 Voice Navigation System.
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