Listado de Certificados Tipos Suplementarios Aceptados por la Autoridad Aeronáutica

STC N°	AUTORIDAD AERONÁUTICA	MARCA DEL PRODUCTO APLICABLE	MODELO DEL PRODUCTO APLICABLE	DESCRIPCIÓN
10027739	EASA	LET	LET 410 UVP-E / LET 410 UVP-E9	The set of the safaty modifications in order to prepare the alternative mean of the compliance to EASA AD 2008-0104 and EASA AD 2008-0105
10030622	EASA	Aircraft Industries, A.S.	L 410 UVP	The set of the safety modifications in order to prepare the alternativemean of the compliance to the EASA AD 2008-0103
10030991	EASA	LET	L-410 UVP L-410 UVP-E L-410 UVP-E20 CARGO L-410 UVP-E9	Introduction of under wing emergency exits.
10035741	EASA	AGUSTA S.P.A	AW109SP	Installation of In-fhght Entertainment System (lES) (composed by kit P/N KNAV-419 and KNAV-420)
EASA A.S.02498	EASA	Vulcan Air	P68TC OBSERVER/ P68 OBSERVER 2/ P68 OBSERVER/ P68 C-TC/ P68 C/ P68 B/ P68	Instalación de una hélice modelo M7V-12-B-C/CF188-53
EASA.R.S.01461	EASA	AGUSTA S.P.A	AB 139 AW139	Interriors Configuration Vip 131 P/N 6AB1AD009-001.
SA00161BO	FAA	Listado del AML	Listado del AML	Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.
SA00171BO	FAA	Listado del AML	Listado del AML	Installation of Pratt & Whitney Engine Services, Inc. Aircraft Data Acquisition System ADAS+, P/N ADAS-K-010.
SA00276NY	FAA	Cessna Aircraft Company	180 Series 182 Series 185 Series	Reinforcement of wing assemblies and installation of Air Research Technology wing tip extension.
SA00290BO	FAA	Listado del AML	Listado del AML	Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX
SA00748DE	FAA	Hawker Beechcraft Corporation	1900D	Installation of the Rockwell Collins IDS-3000 system with new Primary Flight Displays, Multi-Function Display, Display Control Panels, Audio Panels, and Engine Insturmentation
SA00842WI-D	FAA	Raytheon Aircraft Company	1900D	Installation of Honeywell Mark VI Enhanced Ground proximity Warning System.
SA00871SE	FAA	Cessna Aircraft Company	C206 series	lnstalación de Parasol en Gabina de Mando
SA00887SE	FAA	Cessna Aircraft Company	C206 series	lnstalación de Generadores de Vortex en las Alas, Superficies de Cola y Estabilizador Vertical
SA01340LA	FAA	Listado del AML	Listado del AML	Installation of Sandel Avionies Terrain Awareness and Warning System
SA01452CH	FAA	Learjet Inc.	24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 31, 31A, 35, 35A, 36, 36A, 55, 55B, 55C, 60.	Installation of an air ambulance conversion kit.
SA01473SE	FAA	Listado del AML	Listado del AML	Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde
SA01602SE-D	FAA	Cessna Aircraft Company	441	Group aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with the Master
SA01615SE	FAA	Hawker Beechcraft Corporation	200, 200C, B200, B200C, B200GT B200CGT, 300, and 300LW	Installation of winglets and associated changes in wing and aileron structures and related system changes
SA01668CH	FAA	Raytheon Aircraft Company	Listado del AML	Installation of Hartzell Model PHC-(C,L)3YF-1RF/F8068 three bladed propeller in accordance with D’Shannon Products Installation Instructions as listed on AML No. SA01668CH, or later FAA approved revision.
SA01670SE	FAA	Raytheon Aircraft Company	65-B80, A65, 70, 65-90 65-A90, B90, C90, C90A C90GT, E90	Installation of a GWX 68 Weather Radar
SA01692SE	FAA	Listado del AML	Listado del AML	Installation of a Garmin GMX 200 Multi-Function Display in accordance with Garmin Supplemental Type Certificate Master Data List P/N 005-C0315-00, Revision A, dated July 25, 2006, or later FAA approved revision.
SA01748WI	FAA	Hawker Beechcraft Corporation	100 / A100 / B100 / 200 200C / 200T / B200 / B200T B200CT / C90 / C90A E90 / F90	Installation of Cabin LED Downwash Lighting in accordance with PWI Master Document List, No. MDL6910080, Rev IR, dated April 13, 2014, or later FAA approved revisions.
SA01828SE	FAA	Listado del AML	Listado del AML	Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System in accordance with the Installation Manual for the EDM-960, Report No. 909, Revision NC, dated February 22, 2009 or later FAA-approved revision.
SA01933LA	FAA	Listado del AML	Listado del AML	Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System
SA01968SE-D	FAA	Cessna Aircraft Company	441	Certification of Reduced Vertical Separation Minimum (RVSM) Equipment Installation using a single or
SA02013CH	FAA	Listado del AML	Listado del AML	Installation of Avidyne Corporation Traffic Advisory System (TAS)
SA02015SE-D	FAA	Listado del AML	Listado del AML	Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.
SA02019SE-D	FAA	Listado del AML	Listado del AML	Installation of Garmin GTN 6XX/7XX Navigation System
SA02054SE	FAA	Hawker Beechcraft Corporation	C90A, C90GT, C90GTi	Installation of winglets and related system changes.
SA02153LA	FAA	Listado del AML	Listado del AML	Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System.
SA02153LA-D	FAA	Listado del AML	Listado del AML	Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System.
SA02294CH	FAA	Cessna Aircraft Company	180 / 182 / 185 206 / 207 / 210	Installation of an MT-Propeller MTV-(9 or 15)-D/205-58 or MTV-(9 or 15)-D/210-58 and spinner assembly
SA02722CH	FAA	Hawker Beechcraft Corporation	Listado del AML	Install D’Shannon Products, Ltd. 20-gallon fiberglass auxiliary wing-tip fuel tanks DLB1400, Rev. B dated May 14, 2009, in accordance with Installation Manual KB-1401-1, Rev. A, dated May 14, 2009, or later FAA approved revision.
SA02821CH	FAA	Cessna Aircraft Company	180, 182, 185, 206, 207, 210 SERIES	Installation of Hartzell Propeller Models (P)HC-()3YF-1RF/F8068(B,K)() and/or (P)(HC-()3YF01RF/F7693
SA03302AT	FAA	Cessna Aircraft Company	182Q 182R	Installation of Societé de Motorisations Aéronautiques (SMA) Aircraft Diesel Engine model SR305-230-1 (or SR305-230 converted to model SR305-230-1 )
SA04-122	TCCA	Bombardier	DHC-7-100 / 101 / 102 / 103	lnstalación del sistema EGPWS Honeywell MK Vlll
SA04-128	TCCA	Bombardier	DHC-7	Configuraciones de Antenas para DHC-7
SA09013AC-D	FAA	Twin Commander Aircraft Corporation	680T, 680W, 681, 690, 690A, 690B, 680V	Installation of S-TEC System 65 two axis automatic flight guidance system, Model ST-590.
SA09014AC-D	FAA	Twin Commander Aircraft Corporation	680T, 680W, 681, 690, 690A, 690B, 680V	Installation of S-TEC yaw damper system, Model ST-591.
SA09224AC-D	FAA	Cessna Aircraft Company	172 / 172A / 172B / 172C / 172D / 172F / 172G / 172H 142I / 172K / 172 L	Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-685-20/30.
SA09318AC-D	FAA	Hawker Beechcraft Corporation	Bonanza V35B	Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-747-20/30.
SA09401AC-D	FAA	Cessna Aircraft Company	401 / 401A / 401B 402A / 402B / 402C	Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-853 with Optional Autotrim System.
SA09527AC-D	FAA	Twin Commander Aircraft Corporation	690A	Installation of DFCS 01284 (MAGIC 2100) Autopilot System, Model ST-902
SA09536AC-D	FAA	The New Piper Aircraft, Inc.	PA-31T	Installation of S-TEC 01304 Digital FLight Control System.
SA09544AC-D	FAA	Raytheon Aircraft Company	65-90 / 65-A90 / 65-A90-1 65-A90-4 / B90 / C90 / E90 / H90 / C90A / C90GT	Installation of S-TEC 01304 Digital Flight Control System (DFCS).
SA09636AC-D	FAA	Cessna Aircraft Company	425	Installation of S-TEC 01304 Digital Flight Control System (DFCS), Three Axis Automatic Flight Guidance System Part No. 01304-04-01-007, in accordance with Master Data List 921231, Revision 5, dated 9-14-2004, or later FAA approved revision for Cessna 425. FAA approved Airplane Flight Manual Supplement No. 892135, dated 9-20-2004, or later FAA approved revision is required for Cessna 425 with S-TEC 01304 DFCS.
SA09754SC	FAA	Cessna Aircraft Company	340 / 340A	Installation of RAM Series VII 335 horsepower engines
SA09971SC	FAA	Listado del AML	Listado del AML	Installation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellers
SA09971SC-D	FAA	Listado del AML	Listado del AML	Installation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellers
SA10135SC	FAA	Hawker Beechcraft Corporation	35-C33A, 36, A36, E33A, E33C, F33A,F33C, 535, V35, V35A, V35B	Installation of Hartzell model PHC-C3YF-1RF/F8068 propeller. Must be equipped with Teledyne Continental Motors IO-520-B, IO-520-BA, IO-520-BB, or IO-550-B model engine. ,
SA1024SO	FAA	Twin Commander Aircraft Corporation	690A, 690B	Installation 7of AiResearch TPE331-5-252K engines replacing AiResearch TPE331-5-251K engines.
SA10737SC	FAA	Hawker Beechcraft Corporation	200 / 200C / 200T / 200CT A200 / A200C / A200CT B200 / B200C / B200CT and B200T	Installation of Pratt & Whitney Canada PT6A-61Engines and Hartzell (Raisbeck) HC-D4N3A/D9383K-1 Propellers in accordance with Blackhawk Modifications, Inc. Master Drawing List Document Number 06010050
SA10822SC	FAA	Listado del AML	Listado del AML	Installation of EFD1000 Primary Flight Display
SA1359GL	FAA	Twin Commander Aircraft Corporation	680W, 680, 680V, 681, 685, 690, 690A, 690B, 680T, 520, 560, 560-A	Install winglet wingtips.
SA1381GL	FAA	Twin Commander Aircraft Corporation	680-E / 720 / 560F 680FL(P) / 680FL 680F / 720	Replace standard wing tip assembly with winglet tip assembly.
SA2200SW	FAA	Hawker Beechcraft Corporation	A35, B35, C35, D35, E35, F35 G35, H35, J35, K35, M35, 35-33, N35, 35-A33, 35-B33, P35, S35, 35-C33, 35-C33A, E33, F33, V35, V35A, V35B E33A, E33C, 36, A36, F33A F33C, G33.	Installation of Teledyne Continental IO-520-B, -BA, – BB or IO-550-B engine and applicable McCauley Propeller only as listed on STC.
SA2256WE	FAA	Cessna Aircraft Company	C206 series	lnstalación de Borde de Ataque GUFF y Cubiertas de Separación de Alerones en cada Ala
SA236CH	FAA	Twin Commander Aircraft Corporation	690A 690B 690C 690D	INSTALLATION OF ALLIED SIGNAL, INC., (GARRETT) TPE331-10T SERIES ENGINES (-512K, -515K, OR -516K IN THE 690A AND 690B; -511K OR -513K IN THE 690C AND 690D) AND RELATED CHANGES.
SA2513CE	FAA	Cessna Aircraft Company	320F / 320E / 340 340A / 320D	Installation of wing nacelle locker tanks and fuel transfer system.
SA2529WE	FAA	Cessna Aircraft Company	185, 185A, 185B, 185C 185D, 185E, A185E, and A185F Landplane and Floatplane	Installation 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.
SA2586NM	FAA	Listado Maestro de Elegibilidad	Listado Maestro de Elegibilidad	Installation of J.P. Instruments temperature monitoring systems.
SA2698NM-S	FAA	Hawker Beechcraft Corporation	200, A200, B200, B200GT	Installation of a set of Hartzell/Raisbeck Quiet Turbofan Propellers or Swept Turbofan Propellers in accordance with Raisbeck Engineering Drawing List 85-1500
SA2750SW-D	FAA	Listado del AML	Listado del AML	Installation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellers
SA2939NM	FAA	Raytheon Aircraft Company	65-90, 65-A90, B90, C90, C90A, C90GT, E90, C90GTi	Instalación de compartimiento de carga en la nacela del ala
SA3366NM	FAA	Hawker Beechcraft Corporation	200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT, B200GT, B200CGT	Instalación de un sistema de recuperacion de Aire Impacto
SA3519NM	FAA	Hawker Beechcraft Corporation	200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT, B200GT, B200CGT	Instalación de aletas canalizadoras de flujo, placas de metal (strakes) en la parte inferior del fuselaje trasero
SA3593NM	FAA	Hawker Beechcraft Corporation	65-A90, B90, C90, C90A, C90GT, C90GTi, E90	Instalación de Hélices turbofan silenciosa o hélices turbofan hojas de barridos
SA3831NM	FAA	Hawker Beechcraft Corporation	200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT, B200GT, B200CGT	Instalación de bordes de ataque mejorados para incrementar las caracteristicas del comprotamiento en vuelo
SA3861NM	FAA	Twin Commander Aircraft Corporation	690A 690B 690C	INSTALACIÓN DE DOS HÉLICES HARTZELL HC-B3TN-SFLLLTI 0876ANSB-2Q EN LOS AVIONES TWIN COMMANDER EQUIPADOS CON DOS AIRESEARCH MODELO TPE331-S-254K O DOS MODELOS TPE331-10T-511K, -512K, -513K, -515K, O -516K MOTORES DE ACUERDO CON LA FAA COPIA SELLADA DE AERO AIR, INC., LISTA MAESTRA DE DIBUJO Nº AAI-100, REVISIÓN B, DE FECHA 23 DE MAYO DE 1999, O POSTERIORMENTE REVISIONES APROBADAS POR LA FAA
SA4010NM	FAA	Raytheon Aircraft Company	65-90, 65-A90, B90, C90, C90A, C90GT, E90, C90GTi	Instalación de aletas en el fuselaje en la parte inferior
SA4428SW	FAA	Cessna Aircraft Company	172N	For model 172 airplanes with Lycoming O-360 engines per STC SA332GL or STC SA4428SW, modification of standard exhaust system. For model 172 with Lycoming O-360 engines per STC SA647CE or STC SA1324CE, modification of standard exhaust system.
SA4733NM	FAA	Hawker Beechcraft Corporation	300 300LW	Installation of lower aft fuselage strakes.
SA4952NM	FAA	Raytheon Aircraft Company	Beech 100/A100/B100	Installation of main landing gear door system for high flotation gear equipped aircraft.
SA5151NM	FAA	Hawker Beechcraft Corporation	B300 / B300C	Installation of dual aft body strakes.
SA5202SW-D	FAA	Cessna Aircraft Company	182Q 182R T182	Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems.
SA5216SW-D	FAA	Cessna Aircraft Company	U206G / TU206G	Installation of S-TEC System 40/50 single and two axis automatic flight guidance system ST-208-40/50.
SA5789NM	FAA	Raytheon Aircraft Company	Listado del STC	Installation of vortex generators on wing and vertical tail and strakes on engine nacelles.
SA615EA	FAA	Listado del AML	Listado del AML	Installation of Whelen anti- collision strobe light power Systems
SA619GL	FAA	Hawker Beechcraft Corporation	A90 / B90 / C90 / C90A / E90 H90 / 65-A90-1 / 65-A90-4	Install wheels and brakes.
SA63GL	FAA	Cessna Aircraft Company	C206 Series	lnstalación de Ruedas Principales y Frenos Marca Clevelan
SA685AL	FAA	Cessna Aircraft Company	C206 Series	lnstalación Hélices Marca Hartzell, Modelos PHC-J3YF-IRF/ F8468A-8R, PHC-J3YF-1RF/ F8468A-6R, (P) HC-C3YF-1RF/F8468A-8R, O PHC-C3YF-1RF/F8468A-6R
SA8036NM	FAA	Cessna Aircraft Company	185, 185A, 185B, 185C, 185D, 185E, A185E, A185F	Installation of a wing tip fuel tank 28/30 US gallon; increase wing span approximately four feet and
SA8842SW	FAA	Cessna Aircraft Company	180 Series 182 Series	Installation of a Teledyne Continental O-470-U engine as an alternate to Teledyne Continental models O-470-K, L, R, and S.
SA8908SW-D	FAA	Cessna Aircraft Company	335 340 340A	Installation of S-TEC System 55 Two Axis automatic flight guidance system, Model ST-575, with optional autotrim system.
SA8RM	FAA	Cessna Aircraft Company	402C	Installation of a vapor cycle air-conditioning system in accordance with FAA sealed Drawing List No. 40-002 dated February 28, 1973, or DL-40, Revision AB, dated February 23, 1995, or DL-40-2, Revision S, dated January 30, 1995, or later FAA approved revision.
SA9210SC-D	FAA	Hawker Beechcraft Corporation	300	Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS)
SA950CE	FAA	Cessna Aircraft Company	182, 182A, B, C, D, E F, G, H, J, K, L, M, N P, Q, R182, TR182 T182, 182R, 182S 182T, and T182T	Installation of STOL kits (wing leading edge cuffs, drooped tips, stall fences and aileron gap seals).
SE0004EN	FAA	Pratt & Whitney	st02883	lnstructiorrs for continued Airworthiness
SE000EN	FAA	Pratt & Whitney	PT6A-11 / 11AG / 15AG 21 / 27 / 25 / 110 / 112	lnstructiorrs for continued Airworthiness
SE09104SC	FAA	Teledyne Continental Motors	TSIO-520 NB	Modification of Teledyne Continental Motors Model TSIO-520-NB engine in accordance with RAM Drawing No. 1776, Revision E, dated 05/25/1999, or later FAA aproved revision. Maximun continuous power is 335 HP at 2700 RPM and 38.0 inches Hg manifold pressure.
SE3630SW-D	FAA	Teledyne Continental Motors	TSIO-520-SERIES	Engine modiflcations in accordance with RAM Aircraft, Limited Partnership Drawing No. 1157, Rev. AG, dated April 21,2005, or later FAA approved revísion.
SE4327SW	FAA	Teledyne Continental Motors	TSIO-520 NB	Increase all operation power rating to 325 horse power (HP) at 40 inches of manifold pressure (MP)
SH1392SO	FAA	Bell Helicopter Textron	206A / 206B	Instalación de Skid alto en el tren de aterrizaje
SH1447SO	FAA	Bell Helicopter Textron	206A / 206B / 206L / 206L-1 206L-3 / 206L-4 / 407	Installation baggage floor protector
SH1664SO	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Instalación de ventanas y parabrisas
SH1990SO	FAA	Bell Helicopter Textron	206A / 206B / 206L / 206L-1 206L-3 / 206L-4 / 407	Manufacture of Automatic door opener kits in accordance with Aeronautical accessories, Inc. Drawing List Report No. AA-86001, no revisión, dated May 13, 1986, or later FAA aproved revisions, and installation per “Installation Instructions” listed in that report.
SH199OSO	FAA	Bell Helicopter Textron	206A / 206B / 206L / 206L-1 206L-3 / 206L-4 / 407	Manufacture of Automatic door opener kits in accordance with Aeronautical accessories, Inc. Drawing List Report No. AA-86001, no revisión, dated May 13, 1986, or later FAA aproved revisions, and installation per “Installation Instructions” listed in that report.
SH2073SO	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Instalacion del sistema restrictor de hombros
SH2616SO	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Instalación de consola inferior
SH3110S0	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Instalación de Puerta de Compartimiento de Carga
SH3298SO	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Instalación de la tapicería interior
SH3585SW	FAA	Bell Helicopter Textron	206B / 206L 206L-1 / 206L-3	Intallation of freon air conditioner – belt – driven
SH5685SW	FAA	Bell Helicopter Textron	206B / 206L 206L-1 / 206L-3 / 206L-4	Instalación de parabrisas inferior
SH577SW	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Instalación de ventanas de la tripulaciÓn
SH5850SW	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Intallation of Helix-Plex chin Bubble
SR00044AT	FAA	Bell Helicopter Textron	206A / 206B / 206L 206L-1 / 206L-3 / 206L-4	Reeirrplazo de la puerta de la batería
SR00060DE	FAA	AGUSTA S.P.A	A109A, A109AII, A109C, A109K2, A109E	Installation of Belt-Driven Vapor Cycle Air Conditioning System Kit P/N A109-00-011 with dual condenser blower configuration
SR00409SE	FAA	McDonnell Douglas Helicopter Co. (Hughes)	369A, 369H, 369D, 369E, 369FF, 500N, and 600N	Rapid removal door system hinges, installed in accordance with Certified Technology Installation Instructions CT9602-1, Revision C, dated January 1, 2000, or later FAA approved revision and manufactured in accordance with Certified Technology Drawing List CT9602, Revision E, dated January 10, 2000, or later FAA approved revision.
SR00551NY	FAA	Bell Helicopter Textron	206A / 206B / 206L / 206L-1 206L-3 / 206L-4 / 407	Instalación de la consola de equipos de aviónica
SR00650NY	FAA	Bell Helicopter Textron	212 / 412 / 412EP / 412CF	Instalación del sistema de deflectores de los eyectores de escape de Alpine Aerotech Ltd
SR00813AT	FAA	Bell Helicopter Textron	206L, 206L-1, 206L-3, 206L-4	Manufacture of Emergency Floatation System Kits
SR00877SE	FAA	MD Helicopters, Inc.	369D, 369E, 369HM, 369HS y 369HE	Instalación de sistema de filtrado de aire en la entrada de la turbina
SR01052AT	FAA	Listado del AML	205A / 205A-1 / 205B / 212 / 412 / 412EP / 412CF / AB412 / AB412EP	Reemplazo de los tubos cruzados del patin del tren de aterrizaje
SR01062LA	FAA	MD Helicopters, Inc.	369A, 369HM, 369D 369HE, 369HS, 369E, 500N	Installation of Aerometals exhaust tailpipe outlet hangar assemblies, P/N 369X8236.
SR01077AT	FAA	Bell Helicopter Textron	407	Manufacture of cargo mirror assembly
SR01394LA	FAA	MD Helicopters, Inc.	369D / 369E / 369F / 369FF 369H / 369HE / 369HM 369HS	Intallation of Aerospace filtration systems intet barrier filter systemin lieu of the engine air particle separator or FOD Acreen
SR01533AT	FAA	Bell Helicopter Textron	206A, 206B	Manufacture of Emergency Flotation System Kit in accordance with Aeronautical, Accessories, Inc. Drawing List Report No. AA-95074, Revision “A”, dated December 29, 1997, and installation per Report AA-95075, Revision “A”, dated December 4, 1997, or later FAA approved revisions.
SR01849AT	FAA	Bell Helicopter Textron	212 / 412 / 412EP	Reemplazo de equipo de reserva de Nitrógeno compuesto ligero
SR02049LA	FAA	Robinson	R44, R44 II	Installation of Apical Industries, Inc. Emergency Float Kits.
SR02249LA	FAA	Bell Helicopter Textron	206B, 206L, 206L-1, 206L-3, 206L-4	Installation of replacement tail rotor blade
SR02518NY	FAA	Bell Helicopter Textron	212, 412	Installation of Caledonian Airborne Systems Ltd CPT-900 Automatically Deployable/Automatic Fixed Emergency Locator Transmitter
SR02964CH	FAA	Bell Helicopter Textron	206A / 206A-1 / 206B 206B -1 / 206L / 206L-1 206L-3 / 206L-4	Install Airwolf Aerospace, LLC Tension-Torsion Strap Assemblies, P/N AA-206-011-154-105/-107
SR09054RC	FAA	Bell Helicopter Textron	206A / 206B	Instalacion de una bateria de sellada de ácido de plomo
SR09192RC	FAA	McDonnell Douglas	600N	Intallation of a cabin window assembly
SR09368RC	FAA	Bell Helicopter Textron	407	Installation of engine inlet barrier filter (IBF) system.
ST00491SE	FAA	The Boeing Company	DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) MD-90-30 DC-9-81 (MD-81)	Installation of the AlliedSignal Enhanced Ground Proximity Warning System.
ST00598WI	FAA	Embraer	EMB-120 / -120RT EMB-120ER EMB-120QC EMB-120FC	Conversion of airplane from a passenger configuration to an all cargo configuration.
ST00608AT	FAA	McDonnell Douglas	DC-9-10 / 20 / 30 / 40 / 50 & 80 Series	Installation of a Trimble TNL 2100T global positioning system.
ST00737SE	FAA	The Boeing Company	727-100 / 727-200	Modification of Boeing Model 727-100 and 727-200 series airplanes accomplished in accordance with Raisbeck Commercial Air Group, Inc., Master Drawing List 99B-1000, Revision A, dated August 30, 1999, or later FAA approved revision.
ST00835CH-D	FAA	Learjet Inc.	Learjet 31 / Learjet 31A Learjet 35 / Learjet 36 Learjet 36A Learjet 35A (C-21A)	Installation of an AlliedSignal Engines TFE731-2C Turbofan Engine.
ST00836CH-D	FAA	Learjet Inc.	31, 31A, 35, 35A, 36, 36A	Installation of Honeywell N1 Digital Electronic Engine Control (DEEC) in accordance with Garrett Aviation Services drawing list DL836 revision ”J” dated June 24, 2005, or later FAA approved revision.
ST00909SE	FAA	Learjet Inc.	45	Installation of emergency medical stretchers and bases, oxygen and electrical systems
ST01499WI-D	FAA	Learjet Inc.	45	Installation of an UNS-1Ew Flight Management System on Learjet Model 45.
ST01829AT	FAA	The Boeing Company	737-100 737-200 737-300 737-400 737-500 737-700	Installation of SAF-T-GLO Aerospace Limited’s photoluminescent floor proximity emergency escape path marked system (FPEEPMS).
ST01932AT	FAA	McDonnell Douglas	DC9-81, -82, -87 & MD-90-30	Installation of SAF-T-GLO Aerospace Limited’s photoluminescent floor proximity emergency escape path marking system (FPEEPMS) in accordancd with SAF-T-GLO MDL Report Number G49-2, Rev C, July 7, 1999, or later FAA-approved revision..
ST02221AT	FAA	The Boeing Company	757-200 757-300	Installation of SAF-TO-GLO photoluminescent floor proximity emergency escape with marking system (FPEEPMS).
ST02506AT	FAA	Hawker Beechcraft Corporation	400A	Installation of an Increased Ampere-Hour Recombinant Gas (RG) Lead acid battery.
ST02883AT-D	FAA	Gulfstream Aerospace LP	Gulfstream 200	Installation of Transponder Flight ID.
ST02929AT	FAA	McDonnell Douglas / The Boeing Company	DC-9-30 SERIES DC-9-80 SERIES 757-200 SERIES	Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT).
ST02995AT	FAA	McDonnell Douglas	DC9-81, -82, -87 & MD-90-30	Installation of SAF-T-GLO Aerospace Limited’s photoluminescent floor proximity emergency escape path marking system (FPEEPMS) in accordancd with SAF-T-GLO MDL Report Number G49-2, Rev C, July 7, 1999, or later FAA-approved revision..
ST03154AT-D	FAA	Gulfstream Aerospace LP	1125 Westwind Astra Astra SPX Gulfstream 100	Installation of Concorde Valve Regulated Lead-Acid Main Batteries.
ST03358AT-D	FAA	Gulfstream Aerospace LP	Galaxy / Gulfstream 200	Installation of Universal UNS-1C+ Dual Flight Management System Software.
ST03570AT	FAA	Gulfstream Aerospace LP	Galaxy / Gulfstream 200	Installation of an Auxiliary Power Unit (APU) Surge Control Valve Exhaust Modification.
SR01853NY	FAA	Bell Helicopter Textron	412, 412EP	Instalacion del sistema comunicador de data y posicion Skytrac ISAT-200
SA4366WE	FAA	Cessna Aircraft Company	U206G	Instalacion de tanques para combustible de 14,9 U.S. galones en la punta de los planos
SR09347RC-D	FAA	Bell Helicopter Textron	212, 412, 412EP	Instalacion de un sistema de iluminación para las salidas de emergencia
SA00001CH	FAA	Piper Aircraft Corporation	DC9-81, DC9-82, DC9-87	Install Aero Fabricator Shoulder harness and seat belt assembly
SA8404SW-D	FAA	Beechcraft Corporation	58, 58A	Installation of S-TEC System 55 two axis automatic flight guidance system,Model ST-550,
SE444GL	FAA	Teledyne Continental Motors	TSIO-520-B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -U, -BB, -CE, -EB, -JB, -KB, -LB, -NB, -UB, -VB, -AE, -AF, and LTSIO-520-AE	Instalación de un traductor de flujo de combustible
SA544GL	FAA	Cessna Aircraft Company	320D, 320E, 320F, 340A, 335	Instalacion de Sistema de instalación de flujo de combustible
SR09373RC-D	FAA	Bell Helicopter Textron	412, 412EP	Instalación de un sistema de monitoreo de vibración (BHVM)
SH97-76	TCCA	Bell Helicopter Textron	407	Installation of Locking fuel cap kitin
SA09198AC-D	FAA	Piper Aircraft Corporation	PA-23-250, PA-E23-250	Installation of S-TEC System 55X Two Axis Automatic Flight Guidance System, Model ST-662-1
SA3338SW-D	FAA	Beechcraft Corporation	58P, 58PA, 58TC, 58TCA	Instalacion de sistema de vuelo automatico modelo AK813
SR09248RC	FAA	Bell Helicopter Textron	206A/B, 206L, 206L-1, 206L-3, 206L-4	Instalación de un bearing elastomerico en el rotor de cola
SA4934NM	FAA	Cessna Aircraft Company	340A	Installation of vortex generators on the wing and vertical stabilizer, and 5% take off gross weight increase
SA09330AC-D	FAA	Cessna Aircraft Company	182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N	Modernizacion del sistema de piloto automatico
SA00432SE	FAA	Listado del AML	Listado del AML	Fuel flow transducer installed
SA01769WI	FAA	Beechcraft Corporation	B200GT, B200CGT	Sistema dual de control de vuelo Pro Line Fusion
SA01784WI	FAA	Beechcraft Corporation	B300, B300C	Sistema dual de control de vuelo Pro Line Fusion
SA00352BO	FAA	Listado del AML	Listado del AML	Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP34
SA1372GL	FAA	British Aerospace PLC	Jetstream 3100 Series	Installation of McCauley propellers
SA234CH	FAA	Cessna Aircraft Company	Listado del AML	Installation of Hartzell PHC-C3YF- FC7663D-2R with the associated spinner model C-4558-2P or C-4558-
SA02078CH	FAA	Cessna Aircraft Company	R172K	INSTALLATION OF HARTZELL PHC-C3YF-1RF/F7392 WITH SPINNER A-2295-1(P) OR MODEL PHC-G3YF-1RF/F7392 WITH C-4582-(P)
SA00428WI	FAA	Cessna Aircraft Company	206,U206,U206A HASTA U206G,P206, P206A HASTA P206E,TP206A HASTA TP206E,TU206A HASTA TU206G	INSTALACION DE HELICES MCCAULEY, MODELO D3A34C402/90DFA-2,-4,-6,-8 Y -10
ST02893AT	FAA	Beechcraft Corporation	400,400A,400XP,400T,MU-300-10	INSTALATION OF A BOOM BEAM TAXI/LANDING LIGHT SYSTEM
SA01728WI	FAA	Cessna Aircraft Company	525/525A (SERIALES 525-360 HASTA 0599 Y 525A-0001 HASTA 0299)	INSTALACION DE UN SISTEMA GARMIN GTN 650/750 MFD
SA8710SW	FAA	Beechcraft Corporation	65-90,65-A90,B90,C90,C90A,C90GT,C90GTI Y E90	INSTALLATION OF A EXHAUST STUB
SA8711SW	FAA	Beechcraft Corporation	F90	INSTALLATION OF A EXHAUST STUB
SA8712SW	FAA	Beechcraft Corporation	99,99A,99A(FACH),A99,A99A,B99,C99,100,A100,A100A	INSTALLATION OF A EXHAUST STUB
SA00343BO	FAA	AML	AML	INSTALACION DE UNA CONFIGURACION SIMPLE O CONFIGURACION DUAL DE AVIDYNE CORPORATION INTEGRATED FLIGHT DISPLAY, MODEL IFD540
ST00881WI-D	FAA	AML	AML	MODIFICACTION OF A TCAS II SYSTEM INSTALLATION CHANGE 7,0 OR CHANGE 7.1)
ST01855CH-D	FAA	Gulfstream Aerospace LP/ISRAEL AIRCRAFT INDUSTRIES	1125w/1124/1124A	Installation of Honeywell N1 Digital Electronic Engine Control
2017S03-25	BRASIL	Embraer	(ERJ-190-100 SR/IGW/LR/STD) (ERJ-190-200-IGW/LR/STD)	Installation of alternative part number radial construction nose ans main tires
SA03525NY	FAA	Beechcraft Corporation	300, 300LW, B300 Y B300C	INSTALACION DE HELICE DE CINCO PALAS MTV-27-1-E-C-F-R(P)/CFR260-62B
SA01296WI	FAA	Cessna Aircraft Company	A185E, A185F	INSTALACION DE HELICES DE TRES PALAS MTV-15-D/210-58
ST01767WI	FAA	Hawker Beechcraft Corporation	400A	INSTALACIÓN DE WINGLETS
SA00729SE	FAA	AML	AML	Installation 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.
SA4943SW-D	FAA	Cessna Aircraft Company	414A	Installation of RAM winglets
ST02502LA	FAA	The Boeing Company	DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) MD-88 MD-90-30	Installation of TDG Aerospace, Inc. Universal Fault Interrupter (UFI)
SA02539CH-D	FAA	Hawker Beechcraft Corporation	B100	Installation of the Hartzell propeller model HC-B4TN-5F/T10173AN(B,K)-12.5.
SE7559SW	FAA	Teledyne Continental Motors	C-75, C-85, C-90, O-200	Install adapter to permit use of a spin-on oil filter.
SE8409SW	FAA	Teledyne Continental Motors	C-125 SERIES; C145 SERIES; O-300 SERIES; GO-300 SERIES; IO-360 SERIES; TSIO-360 SERIES	Installation of P/N CO-300-1 Oil Filter Adaptor with spin-on filter as a replacement for the existing oil screen
SE09356SC	FAA	Teledyne Continental Motors	O-470; IO-470; IO-520; IO-550	Install F & M Enterprises’ Model C6LC, C6LC-S or C6LC-L oil filter adapter for a spin-on oil filter
SE10348SC	FAA	Teledyne Continental Motors	O-470-11; O-470-15	This STC application is to allow replacement of the existing oil filter screen assembly
ST02030LA	FAA	Learjet Inc.	40 / 45	Installation of a Honeywell Automatic Dependent Surveillance Broadcast (ADS-B) Out system
SA02571SE	FAA	AML	AML	Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).
SA01818WI	FAA	AML	AML	Installation of Garmin G5 Electronic Flight Instrument
SA3598NM	FAA	Beechcraft Corporation	AML	Installation of cockpit sunvisor assemblies
SA02121SE	FAA	AML	AML	Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System
ST04021AT-D	FAA	Gulfstream Aerospace	GALAXY / GULFSTREAM 200	Installation of an Automatic Dependent Surveillance Broadcast Out (ADS-B) System
ST00835DE	FAA	AML	AML	Installation of Automatic Dependent Surveillance – Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor
SA02080AK-D	FAA	Cessna Aircraft Company	208B	Instalacion de Deflector de Escape
ST02427LA	FAA	Cessna Aircraft Company	500; 550; S550; 560; 560XL	Installation of Dual Garmin GTN 6XX/7XX Series Global Navigation System with Structural Antenna and
10053659	EASA	AIRBUS	A300, A310, A300-600	Instalación del TCAS 7.1
SA00765DE	FAA	AML	AML	Installation of Automatic Dependent Surveillance – Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor
SA01714WI	FAA	AML	AML	Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.
SA2000CE	FAA	Cessna Aircraft Company	182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P	“Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index a nd leaded automotive gasoline, 88 minimum antiknock index (RON + MON)/2”
SE1997CE	FAA	CONTINENTAL	O-470-A, -E, -J, -K, -L, -R, -S,	Addition of following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON+MON)/2”
SA11222DS	FAA	AML	AML	Installation of automatic dependent surveillance- broadcast( ADS-B) Out
ST02230SE	FAA	AML	AML	The installation of dual Garmin GTX-33ES Mode-S transponders and single or dual Garmin GTN 650/750 panel mounted navigation and global positioning system (GPS) units, or dual Garmin GTX-335R and/or GTX-345R Mode-S transponders and single or dual Garmin GTN 650/750/625/725 panel mounted navigation and GPS units
ST02989AT	FAA	Cessna Aircraft Company	500 / 550 / 501 / 551	Installation of a modified Glareshield
SA2830SO	FAA	Cessna Aircraft Company	AML	Installation of a Teledyne Continental Motors model IO-550F engine along with either a McCauley or Hartzell (various P/N’s) propeller
SA01944CN	FAA	AML (AERONAVES)	AML (AERONAVES)
SA01943CN	FAA	AML (MOTORES)	AML (MOTORES)
SA00352BO	FAA	AML Doc. Nº AVAXP-006, Rev. 01	AML Doc. Nº AVAXP-006, Rev. 01	Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version)
SA04046CH	FAA	AML Nº SA04046CH	AML Nº SA04046CH	Installation of L-3 GENESIS ™ Electronic Standby Instrument System (ESI-500/MAG-500)
SA02283SE	FAA	AML	AML	Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P
ST03424CH	FAA	Beechcraft Corporation Textron Aviation	400 / 400A – 700A / 700B / 800A / 800B / 800XP / 850XP – 500 /550	Certification of Automatic Dependent Surveillance – Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders
ST11144SC	FAA	The Boeing Company	737-300 / 400 / 500	Installation of Extended Squitter Mode S Transponders and GPS Position Source
SA01695SE	FAA	AML	AML	Installation of an antenna
SA01714WI	FAA	AML	AML	Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.
ST0821WI	FAA	AML	AML
ST04340NY	FAA	AML	AML	Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0
ST03273NY	FAA	The Boeing Company	737-300 / 400 / 500	The installation of Dual CMC SBAS Landing System (GLS) with CMA-5024 GLSSU Sensors and Dual CMC CMA-5025 Control Panels
SA02819NY	FAA
10054797	EASA
ST00361BO	FAA	AML	AML	Installation of a Honeywell Primus II (XS-852) ADS-B Out System
SA01933LA-D	FAA	AML	AML	Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System
SA00343BO	FAA	AML	AML	Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release)
SE693GL	FAA	Teledyne Continental Motors		Superseded by STC SE01943CH. Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index.
SA761GL	FAA	Cessna Aircraft Company	172 / 172G / 172F / 172E / 172D / 172C / 172C / 172A / 172B / 172H	Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index.
SA01943CH	FAA
SA01944CH	FAA	AML	AML	Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.
ST01691WI	FAA	Textron Aviation Inc	500 / 550 / 650 / S550	Installation of Garmin GTN Series GPS/Comm/Nav Systems with optional Garmin GDL-69/A XM Weather Data Link, GTX-33 Series Transponders and optional Bendix/King KMR-675 Marker Beacon Receiver
ST11144SC	FAA	The Boeing Company	737-300 / 400 / 500	Installation of Extended Squitter Mode S Transponders and GPS Position Source
SR02124SE	FAA	AML	AML	Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;
ST01821WI	FAA	Beechcraft Corporation	400A	Installation of Garmin G5000 Integrated Flight Deck with GFC 700 Automatic Flight Control System (AFCS)
ST01823WI	FAA	Textron Aviation Inc	500 / 550 / 560/ 560XL / S550	Installation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out
SA01969SE	FAA	AML	AML	Installation of a Mid-Continent MD302 Standby Attitude Module
ST11216DS	FAA	AML	AML	Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft
SA02636SE	FAA	AML	AML	Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.
SA09546AC-D	FAA	Cessna Aircraft Company	441	Installation of S-TEC 01304 Digital Flight Control System (DFCS)
SR02471AK	FAA	AML	AML	Installation of the L-3 Communications NGT -9000/9000R ADS-B System
ST02632LA	FAA	AML	AML	Modification to replace the existing Mode S Transponder system with ACSS NXG-700 GPS Mode S Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS
ST01443CH-D	FAA	Cessna Aircraft Company	650	Installation of ARTEX Emergency Locator Transmitter (ELT) 110-406.
SA02444AK	FAA	AML	AML	Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed
ST11216DS	FAA	AML	AML	Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft
SE2563CE	FAA	Textron Lycoming AVCO Corporation		Leaded and unleaded automotive gasoline, 91 minimum antiknock index (RON+MON) /2 per ASTM spec D-439. Intermixing with aviation gasoline also approved.
SE1931CE	FAA	Textron Lycoming AVCO Corporation		Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index, (RON+MON)/2.
SA1948CE	FAA	Cessna Aircraft Company	172C / 172K / 172A / 172L / 172 / 172I / 172H / 172G / 172F / 172E / 172D / 172B / 172M	Operation on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index(RON+MON) /2 per ASTM Spec. D-439. Intermixing with aviation gasoline also approved.
SA2600CE	FAA	Cessna Aircraft Company	172N / 172P / 172D / 172E / 172F / 172G / 172H / 172I / 172K / 172L / 172M	Operation of airplane on leaded and unleaded automotive gasoline, 91 minimum antiknock index(RON+MON)/2. Intermixing aviation gasoline also approved.
10072022	EASA	AML	AML	EASA Validation of FAA Approved AML Supplemental Type Certificate (STC)No. STC ST02639LA. This AML STC installs an RTCADO 260B Version 2 ADS-BOut compliant ACSS Mode S transponder (NXT-800)