Supplemental type certificates
49,117 STCs, most recently changed first. Search by what an STC changes, its holder or a model.
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SELECT stc_number, description, holder, status, status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' ORDER BY status_date DESC NULLS LAST, stc_number
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STC ST02938NYMaster Data List, Document Number 8175-MDL Revision O, dated March 11, 2011 and seat installation drawing 8175-2522-2190, Revision I, dated March 11, 2011.
Configuration B: Installation of Executive Interior and Satellite Television Antenna in accordance with BaySys Technologies, LLC Master Data List, Document Number 8175-MDL Revision O, dated March 11, 2011 and seat installation drawing 8175-2522-2199, Revision I, dated March 11, 2011.
Configuration A and B:
The following BaySys Technologies documents are required for this installation:
a. Airplane Flight Manual Supplement, document number 8175-AFMS Revision IR, FAA approved March 14, 2011.
b. The aircraft must be maintained in accordance with Instructions for Continued Airworthiness, document number 8175-ICA, Revision F, dated November 4, 2010, and Maintenance Manual Supplement, document number 8175-MMS Revision A, dated October 29, 2010.
(See Continuation Sheet 2 of 2)STC SR02130SEInstallation of a Supplemental Lighting System, manufactured and installedSTC ST02010SEInstallation of a Thrane & Thrane AVIATOR 300 (Aero-SB Lite) system with Master Data List document AM0225-DL02, Revision D, dated May 24, 2011, or latest FAA-approved revision.STC ST02971CH-DInstallation of Aft VOR/LOC-LSR and Marker Beacon Antennas in accordance with Jet Aviation Index List 41-395G001, Rev NC dated May 28, 2011 or later FAA approved revision.STC SA02848CHInstallation of Wipaire Model 7000 Amphibious FloatsSTC SA02958NYInstallation of propeller MTV-27-1-E-C-F-R(P)/CFR225-55f in accordance with MT Propeller Installation Instruction Doc. No. E-1879, Original Issue, dated October 25, 2010. The following MT Propeller documents are required with this installation:
EASA Approved Airplane Flight Manual Supplement Doc. No. E-1878, Original Issue, dated October 25, 2010 and Instruction for Continued Airworthiness Doc. No. E-1880, Original Issue, dated October 25, 2010.STC ST02318NYInstallation of seating configurations on upper deck of B747-400 Boeing Converted Special Freighter in accordance with Clipper Aviation, Inc., Master Data List CLI-2006-003, Revision D, dated May 23, 2011.STC SA00561DEInstallation of an access panel in the engine baffle piece for the purpose of easing the installation and removal of the oil filter.STC SE00584DEInstallation of modified Oil Filter Adapter, an increased opening pressure spring for filter bypass, and modified filter stud.STC ST01298CH-DInstallation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II).STC SA00730DEInstallation of a monorail sunvisor system in accordance with Drawing List 1970000-DL, Revision D, dated April 8, 2011, FAA approved May 24, 2011, or later FAA approved revision.STC SR01631LAInstallation of starter/generator.STC ST03919ATInstallation of L-3 FA2100CVR Cockpit Voice Recorder in accordance with Chippewa Aerospace Master Drawing List (MDL) No. B747-2371-0001, Rev. 3, Dated December 19, 2010, or later FAA approved revision.STC ST03864ATInstallation of a cabin interiorSTC ST03870ATInstallation of A cabin interior on a Bombardier Model BD-700-lAl 0, SIN 9347, for a total of 14 passengers. This interior is installed in accordance with Savannah Air Center MDL, XRS9347-MDL-2500001, Rev. A, dated August 06, 2010, or later FAA approved revision.STC SA4942SWInstallation of Vortex control wing tip in accordance with Frakes Aviation Drawing No. FA-7042 dated 11/24/82, or later FAA approved revision.STC SB02969CHReplace Balony Kubicek Basket/Burner system and fuel tanks with the Aerostar International Basket Model RB12, S/N RB12-122; the Aerostar International Burner Model HP III Triple, S/N 3014; Aerostar International Model V-18 fuel tank, S/N 00227 and Model V-23 fuel tanks, S/Ns 00061, 00062, and 00063. The Aerostar International Basket/Burner is installed via the standard Balony Kubicek carabiner (snaplink) attachments as specified in the FAA Approved Balloon Flight Manual Supplement dated May 17, 2011.STC SB02970CHReplace Balony Kubicek Basket/Burner system and fuel tanks with the Aerostar International Basket Model RB12, S/N RB12-105; the Aerostar International Burner Model HP III Triple, S/N 3004; Aerostar International Model V-18 fuel tank, S/N 96021 and Model V-23 fuel tanks, S/Ns 95012, 95016, and 95018. The Aerostar International Basket/Burner is installed via the standard Balony Kubicek carabiner (snaplink) attachments as specified in the FAA Approved Balloon Flight Manual Supplement dated May 18, 2011.STC ST04211AT-DInstallation of Dual AN/ARC-210(V) Talon VruHF Airborne RadiosSTC SB02968CHReplace the Cameron Balloons US burner, and fuel tanks with Cameron Balloons Ltd. (EASA TCDS BA.013)(Thunder & Colt (B2EU) and (B3EU)) Stratus double burner via standard burner frame gimbal block and tank straps.STC SB02972CHReplace the Lindstrand Balloons Ltd Basket/Burner system with the Aerostar International Basket, Part Number 51620, S/N CWS-3139, and the Aerostar International Burner, Part Number 52350, S/N HP3D-3645. Replace the Lindstrand Balloons Ltd fuel tanks with the Aerostar International Model V-18 Fuel Tanks, Part Number 53037, S/Ns 96052 and 96055. The Aerostar International Basket/Burner is installed via the standard Lindstrand Balloons carabiner (snaplink) attachments.STC SR00311BOInstallation of Hydraulic Pack System including a hydraulic pump connected to the auxiliary pad of the onboard Lycoming engine in accordance with Firefly Inc. Master Document List, Document No. FFI-10000MDL, dated March 29, 2011, or later FAA-approved revision.STC SA2529WEInstallation of twelve (12) gallon auxiliary fuel tank in each wing,
inboard of tip in accordance with FAA sealed Flint Aero Drawing List No. MDL FA-180, no Revision,
dated December 18, 1981, or later FAA approved revision, or Flint Aero Master Drawing List
No. 15171821, Revision IR , dated may 18, 2006, or later FAA approved revision.STC ST00541SEInstallation of a Pratt & Whitney PT6A-34 engine rated at 560 HP, 2200 RPM, or as an option, a Pratt & Whitney PT6A-35 engine rated at 560 HP, 2190 RPM, or as an option, a Pratt & Whitney PT6A-21 engine rated at 550 HP, 2200 RPM, and an eligible propeller from Table 1, Page 3 and associated hardware in accordance with Rocket Engineering Master Drawing List 560.00.000, Revision AP, dated September 14, 2007, or later approved revision.STC ST02984NYInstallation of Cockpit Floor Mounted Push to Talk Switch in accordance with ACS-NAI Ltd Modification Data Summary Number G987000 Revision N/C, dated March 4, 2011, or later Transport Canada approved revision.STC ST02985NYInstallation of a Honeywell CAS 66A TCAS 1 Installation on a Learjet inc. Model 31, in accordance with Bombardier Aerospace Master Drawing List BAS31010032 Revision NC, dated September 12, 2007, or later approved revision.STC ST02987NYInstallation of a secondary power source to each EFB unit (pilot/co-pilot) in the cockpit, in accordance with ACS-NAI Modification Data Summary, document number G918000 Revision N/C, dated December 22, 2010, or later Transport Canada approved revision.STC SA02112AKFabrication and installation of Stabilizer Jack-Screw Actuator in accordance with North Pacific Welding Drawing Number C-0712500, dated March 31, 2000 and Cessna Skywagon 180 and 185 Series Service Manual; or McFarlane Aviation, Inc., Drawing 1111-1, revision original, dated June 1, 2010 or later FAA approved revisions.STC SA02113AKFabrication and installation of Stabilizer Jack-Screw Actuator in accordance with North Pacific Welding Drawing Number C-0712500, dated March 31, 2000 and Cessna Skywagon 180 and 185 Series Service Manual; or McFarlane Aviation, Inc., Drawing 1111-1, revision original, dated June 1, 2010 or later FAA approved revisions.STC SA02161AKFabrication and installation of Stabilizer Jack-Screw Actuator in accordance with North Pacific Welding Drawing Number C-0712500, dated March 31, 2000 and Cessna 100 Series 1962 and prior Service Manual, dated February 1, 1962; or McFarlane Aviation, Inc., Drawing 1111-1, revision original, dated June 1, 2010 or later FAA approved revisions.STC ST00063MCInstallation of Universal Avionics Dual UNS-1Espw upgradeSTC ST02128SEInstallation of a new premium economy class seat arrangement for Delta Air Lines A330-300 aircraft in accordance with Northwest Aerospace Technologies, Inc. (NAT) Master Drawing List N0371-D10, Revision B, dated April 4, 2011 or later Federal Aviation Administration (FAA) approved revisions.STC SB02966CHReplace the Lindstrand Balloons Ltd Basket/Burner system with the Aerostar International Basket, Part Number 13860, S/N CW3131, and the Aerostar International Burner, Part Number 17395, S/N HP2D-3230. Replace the Lindstrand Balloons Ltd fuel tanks with the Aerostar International Model H-20 Fuel Tanks, Part Number 07752, S/Ns H-211 and H-217. The Aerostar International Basket/Burner is installed via the standard Lindstrand Balloons carabiner (snaplink) attachments.STC SB02965CHReplace the Lindstrand Balloons Ltd Basket/Burner system with the Aerostar International Basket, Part Number 53030, S/N RWSW-127, and the Aerostar International Burner, Part Number 52350, S/N HP3D-3053. Replace the Lindstrand Balloons Ltd fuel tanks with the Aerostar International Model H-20 Fuel Tanks, Part Number 07752, S/N H-95057 and Model V-18 Fuel Tanks, Part Number 53037, S/N 95047. The Aerostar International Basket/Burner is installed via the standard Lindstrand Balloons carabiner (snaplink) attachments.STC SA00553ATInstallation of either a Hartzell model PHC-J3YF-1RF/F7691() or PHC-J3YF-1RF/F8468A() -6R propeller and associated spinner assembly in accordance either Bonaire Aviation Company Propeller Installation Instructions in Cessna 201 Series Aircraft (Continental IO-520L Powered) dated June 1, 1994, or later FAA approved revision; or John Jewell Aircraft, Inc. Cessna 210 Hartzell PHC-J3YF-1RF/F7691 or PHC-J3YF-1RF/F8468A SA00553AT Installation Manual dated March 1, 2011, or later FAA approved revision.STC SA02985CHInstallation of a Cool Start System in accordance with Installation Instructions , Revision A, dated April 14, 2011, or later FAA Approved revision.STC SA2700SWInstallation of geared elevator tab according to Drawing FA-7023, Revision F, dated 11/28/77, Sheets 1 through 3; E.O. s FA-7023G dated 1/23/78; FA-7023H (6 sheets) dated 3/24/78, or later FAA approved revision.STC SA2747SWInstallation of lockable, full swivel tail wheel per Drawing FA7027H, dated 5/11/78, or later FAA approved revision.STC SA3522SWRemoval of the three degree offset from the vertical stabilizer, addition of the airfoil shape to the top of the horizontal stabilizer, and move of the turbine aft by 13 inches in accordance with Drawing Numbers 7061, 7062, 7063, and Drawing List No. 70001 revised 10/10/85.STC SA3528SWInstallation of airfoiled horizontal stabilizer and straightening of the vertical fin in accordance with Frakes Drawing List 70002 dated 10/31/85, or later FAA approved revision.STC SA4003SWAddition of servo-tabs to upper ailerons according to Drawing FA 7039, Sheets 1 and 2, dated 5/15/79, or later FAA approved revision.STC SA4035SWManufacture and installation of Frakes Aviation PN FA 7040-2 Cockpit Air Inlet Scoop according to Drawing FA 7040 dated 8/10/79 and Installation Instructions.STC SA4941SWInstall two additional 17 gallon fuel tanks in each upper wing in accordance with Frakes Aviation Drawing Number 7045.STC SA4959SWRevised engine inlet air filtration and intake geometry with PT6A-34 engine installed per STC SA3238WE in accordance with Frakes Aviation Drawing FA 7502, Sheets 1 through 10, dated 3/8/83.STC SA5590SWFrakes engine cowling, air inlet and filtration system and engine bleed air cockpit heater.STC SA7415SWInstallation of a cockpit bleed air heaterSTC SA8763SWInstallation of an improved cowling, air inlet and filtration systemSTC SA8764SWInstallation of an improved cowling, air inlet and filtration system on Model AT-502 in accordance with Frakes Aviation, drawing list FA 7900B,Rev B, dated 11-30-93.STC SB02995CHReplace the Cameron Balloons Ltd. fuel tanks with Cameron Balloons US 15 or 20 gallon fuel tanks, part numbers CB2901, CBUS1060, and CB2903 (built under Type Certificate (TC) B2GL).STC ST01623WI-DInstallation of Rockwell Collins, Inc. Pro Line Fusion Integrated Modular Avionics (IMA) system, with right side cockpit (copilot) primary flight displays and controls only, in accordance with:
(1) Master Drawing List RCA-0211-001, Revision -, dated March 9, 2011,
(2) Airplane Flight Manual Supplement RCA-0214, Revision -, dated March 8, 2011,
(3) Instructions for Continued Airworthiness RCA-0248, Revision -, dated March 8, 2011,
or later FAA approved revisions to (1), (2), and (3).