Beech E-55
STCs that may be installed · 343
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 ('1152732')
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 ('1152732')
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 SA1471CEInstallation of flap and aileron seals per Smith Speed Conversions, Inc. Drawing List 1004 stamped FAA Approved on February 5, 1979, or later.STC SA1472CEInstallation of elevator tail cone fairing per Smith Speed Conversions, Inc. Drawing List No. 1005 stamped FAA Approved on February 5, 1979, or later.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 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 SA09222SCInstallation of B-1112 air/oil separator in accordance with J.V.E., Inc. Drawing List DL-8800, Revision 3, dated 03/14/96, Installation Manual BOS-AO1, Revision A, dated 01/22/96, or later FAA approved revisions.STC SA197NWInstallation of Clark three- light gear position indicator system.STC SA2871WEInstallation of right and left hand cockpit side windows in accordance with FAA sealed Beryl D Shannon Aviation Specialties, Inc. Drawing List DLB-1301.STC SA02676CHInstallation of left and right hand fuselage external doublers per attached FAA Approved Model List (AML) No SA02676CH, issued June 8, 2011, or later FAA approved revision.STC SA02561CH-DInstallation of the Hartzell propeller model PHC-C3YF-2UF/FC7391D(B) and PHC-J3YF-2UF/FC7391D(B) propellers in accordance with installation instructions INST_102210 dated October 22, 2010, or later FAA Approved revisions.STC SA00670SEReplacement of certain Goodrich pneumatic deicer boots in accordance with SMR Technologies, Inc. Installation Instructions as listed on AML No. SA00670SE.STC SA00616ATInstallation of McCauley Propeller Model 3AF32C504/82NEA, on Beechcraft Models 95-C55, 95-C55A, D55, D55A, E55, & E55A and McCauley Propeller Model, 3AF32C512/82NEA, on Beechcraft Models 58 & 58A, per Colemill Enterprises Installations Instructions dated November 11, 1994, or later FAA Approved Revision.STC SA1762SOInstall two Teledyne Continental Motors model IO-550-C engines, Hartzell or McCauley propellers, nose cowling (P/N 74000-1) per Colemill Enterprises, Inc. Dwg. No. 74000, Initial Release dated October 29, 1984, and winglets (P/N 66000-50 and -51) per Colemill Enterprises Dwg. No. 66000, Initial Release dated October 29, 1984, in accordance with Colemill Enterprises, Inc. Installation Instructions for Modification of Beechcraft Models: C55, D55, E55, and 58 , dated September 14, 1984, or later FAA approved revision of this document or either drawing.STC SA2103SOInstallation of auxiliary fuel wing tips and winglets in accordance with Colemill Enterprises Installations Instruction for Modification of Beechcraft Baron Model 55 and 58 Aux Fuel Tank Installation revised July 28, 1986 and Colemill Enterprises Drawing No. 7800 Rev. A dated July 28, 1986. Colemill Enterprises Airplane Flight Manual Supplement dated April 28, 1987, is required with this installation.STC SA2997SOInstallation of McCauley propeller governor.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 ST02819NYInstallation of 4-blade propeller MTV-14-D-C-F/CF188-30gSTC SA00290BOInstallation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXXSTC SA02110CHInstallation of a Time Trac Data RecorderSTC SA02293AKInstallation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).STC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.STC SA10960SCInstallation of a built-in oxygen system installedSTC SA4172NMInstallation of Aviation Development oil filter.STC SA00523AT-DInstallation of replacement fuel cell assembliesSTC SA00730AT-DInstallation of replacement fuel cell assembliesSTC SA01149ATInstallation of left hand side and right hand side box section fuel assemblies on Beech BE-58's, and left hand side and right hand side Auxiliary tank fuel cell assemblies on Beech BE-55's. (58TC ALL S/N'S)STC SA01204ATInstallation of left-hand side and right-hand side main fuel tank fuel cell assemblies.STC SA00723AT-DInstallation of replacement fuel cell assembliesSTC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA01834CHInstallation of the High Intensity Discharge Light Assembly Kit.STC SA593CHInstall Champion SlickSTART magneto booster system.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeSTC SA01033WIReplacement of original outboard main landing gear doors with a one-piece monolithic machined metal door.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA00609DEInstallation of a nose whell shimmy damperSTC SA01205WI-DInstallation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.STC SA01105WI-DInstallation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).STC SA917EAInstallation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail, P/N 30-0555-( ).STC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.STC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.STC SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA01170NYInstallation of NPX138N-XXX FM Transceiver.STC SA02172CHInstallation of aluminum elevator skins in place of magnesium elevator skins.STC ST01468CHInstallation of various SMR Technologies electrical propeller deicer models.STC SA486GLInstallation of a Shadin Co. fuel flow indicating system.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA01663SEInstallation of Turbo Charger System.STC SA00729SEInstallation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760, Revision -, dated 7/20/99, or later FAA approved revision.
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