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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STC ST10383SCInstallation of four different interior configuration options in accordance with DRB Aviation Consultants, Inc., Master Data List DL1150M01, Revision C, dated February 16, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Document No. 1150R25C02, Revision IR, dated February 16, 2005, or later FAA approved revision is required.Raytheon Aircraft Services Inc · Feb 16, 2005STC SA4381NMInstallation of Cockpit Sun Visor.Rosen Sunvisor Systems LLC · Feb 15, 2005STC ST03041ATThis is an installation for a Honeywell ARINC 717 Flight Data Acquisition Management System in accordance with General Aerospace Master Drawing List No. GA67-DFDR-MDL, Revision A, dated October 1, 2004, or later FAA approved revisions.General Aerospace Inc · Feb 15, 2005STC ST03042ATHoneywell Aircraft Communication Addressing and Reporting Systems (ACARS).General Aerospace Inc · Feb 15, 2005STC SA01698LAInstallation of interior sidewall/armrest panels per drawing DT1-1-02, Revision B, dated December 6, 2004, and later FAA approved revisions as listed on AML No. SA01698LA.Aviation Design of Camarillo CA · Feb 14, 2005STC SE01805NYInstallation of Fuel Nozzle Adapters using studs and nuts.Atlantic Turbines International Inc. · Feb 14, 2005STC ST00211BOInstallation of Aircell ST 3120 Satellite Transceiver System in accordance with BBAS Master Document List BAS63017004, Revision A, dated February 8, 2005, or later FAA approved revision.Learjet Inc. · Feb 14, 2005STC ST01509SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-MU-0413, Rev. NEW, dated February 4, 2005 or latest FAA approved revision.AeroMech Incorporated · Feb 14, 2005STC ST10297SC-DS/N 103 ONLY: Installation of an executive cabin interior.Gulfstream Aerospace Corporation · Feb 14, 2005STC ST10380SCThe right hand #1 & #2, and left hand #2, #3, #7 & #8 low back wide seats with hidden extendable headrests will be replaced with high back wide seats with exposed flex wing style extendable headrestsLearjet Inc. · Feb 14, 2005STC SA2505NMInstallation of Pheromone aerial application system. (AT-400A RESTRICTED CATEGORY)Herculite Products Inc · Feb 11, 2005STC SA4428NMInstallation of Schweizer Phermone aerial application system model No. P.A.A.S. 82.Herculite Products Inc · Feb 11, 2005STC ST01714LA-DInstallation of a Honeywell MST-67A Transponder Upgrade for Elementary Surveillance Mode S Transponders (Flight ID).Learjet Inc. · Feb 11, 2005STC SR00576DEInstallation of a Roll-on Littler System.Air Methods Corporation · Feb 10, 2005STC SR02057NYUpgrade of the S6135-20600 series main gearbox by replacing input free-wheeling units in accordance with Carson drawing. IFWU INSTL Carson S-61 No. CHI-R-001, no revision, dated 12-15-04 and Carson Installation Instructions Report CHI-R-INSTALL, no revision, dated 12-14-04.Carson Helicopters, Inc · Feb 10, 2005STC SR02055NYInstallation of Fuel Purge Canister to be done in accordance with Transport Canada approved DART Aerospace Ltd. Installation Instructions, IIN-D412-706, Revision A, dated November 30, 2004, or later Transport Canada approved revision.Dart Aerospace Limited · Feb 9, 2005STC SR02056NYInstallation of Helicopter Performance Monitoring System is to be done in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332101, Revision 1, dated July 25, 2003, or later Transport Canada approved revision. Audio option is to be installed in accordance with Aero-Dyne Repair Services Engineering Order (EO) EO332102, dated April 2, 2003, or later Transport Canada approved revisions.Aero-Dyne Repair Services Ltd. · Feb 9, 2005STC ST02054NYInstallation of Fin-Cap Camera System to be completed in accordance with Aero Consulting Services Ltd. Modification Data Summary Number E181000, Revision N/C, or later Transport Canada approved revision.Bombardier Aerospace · Feb 9, 2005STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.Avidyne Corporation · Feb 8, 2005STC SA01981NYInstallation of a Universal Avionics Terrain Awareness Warning System (TAWS).Northrop Grumman Corporation California Microwave Systems · Feb 8, 2005STC ST416CH-DInstallation of a Honeywell Ground Proximity Warning System (GPWS) or Enhanced Ground Proximity Warning System (EGPWS).Gulfstream Aerospace Corporation · Feb 8, 2005STC ST01506SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-BJ400-0412 , Rev. NEW, dated January 28, 2005, or later FAA approved revisions.AeroMech Incorporated · Feb 7, 2005STC SA10351SCInstallation of decorative fiberglass fairing in accordance with Texas Skyways, Inc. Master Drawing No. TSFG-100-1, dated November 18, 2004, or later FAA approved revisions.Texas Skyways Inc · Feb 4, 2005STC SA5810NMInstallation of Flite-Tronics static inverter model No. PC-3Y-500.WECO Aerospace Systems Inc. · Feb 4, 2005STC SH8801SW-DFabrication and installation of Simplex Model 301 fire attack system.Simplex Manufacturing Company · Feb 4, 2005STC ST01496SECockpit Sun Visor installation in accordance with Federal Aviation Administration (FAA) approved Rosen Sunvisor Systems Drawing List 1570000-DL, Revision E, dated December 28, 2004, or later FAA approved revision.Rosen Sunvisor Systems LLC · Feb 4, 2005STC ST01505SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Hawker Siddeley DH.125 Series 400A, Serial Number NA742 only. Non-Group (Individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM).AeroMech Incorporated · Feb 4, 2005STC ST02045CH-DInstallation of an Aft Lavatory with shower.Gulfstream Aerospace Corporation · Feb 3, 2005STC ST10379SCInstallation of a Universal Avionics Systems Multi-Function Display.Aircraft Systems & Mfg · Feb 3, 2005STC ST10377SCInstallation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS) upgrade.Aircraft Systems & Mfg · Feb 2, 2005STC ST10378SCInstallation of a Universal Avionics Systems Multi-Function Display.Aircraft Systems & Mfg · Feb 2, 2005STC ST01502SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Dassault Mystere-Falcon 20-D5, Serial Number 202 only. Non-Group (individual) aircraft approval for Reduced Vertical Separation Minimum (RVSM).AeroMech Incorporated · Feb 1, 2005STC ST01740LAInstallation of ACSS T2CASAviation Communication and Surveillance Systems (ACSS) LLC · Feb 1, 2005STC ST02053NYInterior installation in accordance with Transport Canada approved Cascade Engineering Order 3410 Rev. Nil, dated January 13, 2005, or later Transport Canada approved revisions.Cascade Aerospace Inc. · Jan 31, 2005STC SA01301WIInstallation of Jacobs R-755B2 or R-755B2M engine modified for fuel injection in accordance with STC SE01288WI, J.P. Instruments Fuel Flow meter in accordance with STC SA00432SE, and electric fuel boost pump. Data required: (1) Radial Engines Master Drawing List Report REL1003-13, Revision (IR), dated October 4, 2004, (2) Radial Engines Limited Instruction for Continued Airworthiness Report REL1003-12, Revision (IR), dated October 4, 2004, and (3) FAA Approved Airplane Flight Manual Supplement REL1003-5, Revision (IR), dated January 21, 2005 or later FAA Approved revisions to (1), (2), or (3).Radial Engines Ltd · Jan 27, 2005STC SA02078CHInstallation of a Hartzell Propeller Inc. 75 diameter three-blade propeller model (P)HC-C3YF-1RF/F7392 with A-2295-1(P) spinner or model (P)HC-G3YF-1RF/F7392 with C-4582-(P) spinner on a Cessna R172K (Hawk XP) Landplane aircraftHartzell Propeller Inc · Jan 27, 2005STC ST01500SEDescriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Raytheon Model HS125-700A Serial No. NA0322. Divian and PSU assembly installation.TCA AIR LLC · Jan 25, 2005STC ST01501SEInstallation of Air Traffic Control Mode S Transponders with Elementary/Enhanced Surveillance in Boeing 767-200 airplanes in accordance with Northwest Aerospace Technologies, Inc. (NAT) Master Drawing List N0221-D10, Revision A, dated December 16, 2004, or later Federal Aviation Administration (FAA) approved revisions.Northwest Aerospace Technologies Inc · Jan 25, 2005STC SA01175WIInstallation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS).Duncan Aviation Inc · Jan 24, 2005STC SA01176WIInstallation of Collins TCAS-4000 Traffic Alert and Collision Avoidance System (TCAS-II).Duncan Aviation Inc · Jan 24, 2005STC ST01128CH-DInstallation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system.Garrett Aviation Services · Jan 22, 2005STC ST01382SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM). Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Learjet Model 31, Serial Numbers 033, 033A, 033C, and 033D only.AeroMech Incorporated · Jan 21, 2005STC ST01498SEDescriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to Learjet Model 55, Serial Number 085 only.AeroMech Incorporated · Jan 21, 2005STC ST01707LAInstallation of ACSS T2CASACSS (Aviation Communication and Surveillance Syst · Jan 21, 2005STC ST10294SC-DInstallation of cockpit center pedestal extension.Gulfstream Aerospace Corporation · Jan 21, 2005STC ST10295SC-DS/Ns 52 and up ONLY: Installation of 3rd Collins FMS 6100 Flight Management System.Gulfstream Aerospace Corporation · Jan 21, 2005STC ST10296SC-DS/N 102 ONLY: Installation of an executive cabin interior.Gulfstream Aerospace Corporation · Jan 21, 2005STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.Electronics International Inc. · Jan 20, 2005STC ST00795ATApproval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data pertaining to this modification are considered inadequate for duplication in other aircraft.This approval is limited to the installation in the Boeing 727-200, (Serial Number 20938 only).Structural Integrity Engineering · Jan 20, 2005STC ST01043ATApproval of increased operating weights.Structural Integrity Engineering · Jan 20, 2005