Listado de Certificados Tipos Suplementarios Aceptados por la Autoridad Aeronáutica
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 |
