reporte de aceptación de certificado tipo · s/a - embraer are in compliance with the icao annexes...

Unidad Administrativa Especial de Aeronáutica Civil REPORTE DE ACEPTACIÓN DE CERTIFICADO DE TIPO

(Type Certificate Acceptance Report)

GSAC-4.0-8-02 Versión: 01 26/05/2009

Reporte de Aceptación de Certificado Tipo

Type Certificate Acceptance Report

No. ANAC No. 8505 and TCDS No.EA-8505-07 Noviembre2004 EMBRAER: EMB-120

EMB-120RT EMB-120ER EMB-120FC EMB-120QC



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TABLA DE CONTENIDO (TABLE OF CONTENTS)

RESUMEN (SUMMARY) 3 1. INTRODUCCIÓN (INTRODUCTION) 3 2. DETALLES DE CERTIFICACIÓN DE TIPO OACI (ICAO TYPE CERTIFICATE DETAILS) 4 3. DETALLES DE ACEPTACIÓN DE TIPO (TYPE ACCEPTANCE DETAILS) 4 4. REQUERIMIENTOS DE LOS R.A.C. PARTE 9A (COLOMBIAN R.A.C. PART 9TH DATA REQUIREMENTS) 5 5. REQUERIMIENTOS ADICIONALES DE LOS R.A.C. PARTE 4

TA

(ADDITIONAL COLOMBIAN REQUIREMENTS R.A.C. PART 4TH) 8

APENDICE 1 - LISTA DE CHEQUEO DE AERONAVES (APPENDIX 1 – AIRCRAFT CHECK LIST) 10 APENDICE 2 - ADJUNTOS (APPENDIX 2 - ATTACHMENTS) 14



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RESUMEN (SUMMARY) La aceptación de Tipo Colombiana ha sido otorgada para los modelos EMB-120, EMB-120RT, EMB-120ER, EMB-120FC y EMB-120QC, de la Empresa Brasileira de Aeronáutica S/A EMBRAER, basados en el Certificado Tipo ANAC No. 8505 y TCDS No.EA-8505-07 de Noviembre 2004. La aplicabilidad es para los modelos EMB-120, EMB-120RT, EMB-120ER, EMB-120FC y EMB-120QC, los cuales son elegibles para la emisión de un certificado de Aeronavegabilidad estándar de acuerdo con los Reglamentos Aeronáuticos Colombianos RAC numeral 4.4.1.8., esta aceptación estará sujeta a cualquier requerimiento excepcional operacional que requiera ser cumplido (Ver ítem 5 de este reporte para una revisión del cumplimiento del diseño básico con las reglas operacionales). Colombian Civil Aviation Authority grants Type Certificate Acceptance for the models EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC, of the Empresa Brasileira de Aeronáutica S/A EMBRAER, based on the ANAC Type Certificate No. 8505 and TCDS No.EA-8505-07 de November 2004. Applicability is for the EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC models, which are eligible for the issue of a Standard Airworthiness Certificate according to Colombian Regulations - RAC section 4.4.1.8. This Acceptance is subject to any outstanding Colombian operational requirement. (See item 5 of this report for review of compliance of the basic type design with the operating rules).

1. INTRODUCCIÓN (INTRODUCTION)

Este reporte detalla los aspectos para la aceptación del Certificado Tipo de la ANAC No. 8505 y TCDS No.EA-8505-07, de acuerdo con los RAC Parte 9a literal §9.1 (d) y 9.2.3, con el objeto de emitir un Certificado de Aeronavegabilidad Estándar en Colombia. This report details the basis on which the FAA Type Certificate No. 8505 and TCDS No.EA-8505-07 was accepted, in accordance with the RAC’s, part 9.1 (d) and 9.2.3, in order to issue a Colombian Standard Airworthiness Certificate. Específicamente este reporte está dirigido a: Specifically the report aims to:

(a) Determinar los estándares de diseño del código de aeronavegabilidad asociados al certificado tipo extranjero para la aceptación de este modelo de aeronave en Colombia.

(a) State Design standards of the airworthiness code related to the foreign Type Certificate for the acceptance of this aircraft model in Colombia.

(b) Identificar cualquier condición especial, (b) Identify any special condition, Safety



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nivel equivalente de seguridad o excepción aplicable al modelo cubierto por el Certificado Tipo.

Equivalent Level, or applicable exception to a model covered by the Type Certificate.

(c) Establecer cualquier requerimiento adicional que deba ser cumplido, antes de emitir el Certificado de Aeronavegabilidad Estándar en Colombia.

(c) Determine any additional requirement that must be complied before Colombian Airworthiness Certificate be issued

2. DETALLES DE CERTIFICACIÓN DE TIPO OACI (ICAO TYPE

CERTIFICATE DETAILS)

Los modelos EMB-120, EMB-120RT, EMB-120ER, EMB-120FC y EMB-120QC, de la Empresa Brasileira de Aeronáutica S/A - EMBRAER cumplen con los estándares de aeronavegabilidad definidos en los anexos 8 y 16 de OACI, respecto a los requisitos de diseño, requisitos de aeronavegabilidad continuada y de ruido. El fabricante establece que

no existe ninguna diferencia que deba ser evaluada. The models EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC, of the Empresa Brasileira de Aeronáutica S/A - EMBRAER are in compliance with the ICAO annexes 8 and 16 about rules necessaries for the design, continued airworthiness conditions and noise compliance. The manufacturer establishes that there is no difference that should be evaluated.

3. DETALLES DE ACEPTACIÓN DE TIPO (TYPE ACCEPTANCE

DETAILS)

La aplicación para la aceptación del Certificado Tipo de las aeronaves EMB-120, EMB-120RT, EMB-120ER, EMB-120FC y EMB-120QC fue solicitada por el fabricante el día 21 de Diciembre de 2011 y fue aprobada el día 05 de Julio de 2012, basada en el Certificado Tipo de la ANAC No. 8505 y TCDS No.EA-8505-07, e incluye los motores Pratt & Whitney Canada PW118 series aprobados mediante Certificados Tipo FAA No. E20NE. Las hélices Hamilton Sundstrand. 14RF-9 aprobadas mediante Certificado Tipo FAA número P11NE. The application for Colombian type certificate acceptance of the models EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC, was received from the manufacturer, on December 21st, 2011. The Type Acceptance Certificate was approved on July 05th, 2012, based on validation of ANAC Type Certificate No. 8505, and TCDS No.EA-8505-07 that includes Pratt & Whitney Canada engines PW118 series approved under FAA Type Certificate number E20NE. Propeller Hamilton Sundstrand 14RF-9 approved under FAA Type Certificate number P11NE.



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4. REQUERIMIENTOS DE LOS RAC PARTE 9ª (COLOMBIAN RAC

PART 9th DATA REQUIREMENTS)

Los requerimientos establecidos en la parte Novena de los RAC han sido cumplidos y se sustentan en el Certificado Tipo ANAC No. 8505 y TCDS No.EA-8505-07 de Noviembre de 2004 con los siguientes documentos: The Type Data requirements of RAC Part 9 have been satisfied according to the Type Certificate ANAC Type Certificate No. 8505 and TCDS No.EA-8505-07 dated November 2004 with the following documents: (1) Certificados Tipos (Type certificates):

ANAC No. 8505 and TCDS No.EA-8505-07 dated November 2004

FAA No. E20NE Rev. 12, dated September 01, 2008

FAA No. P11NE Rev. 12, dated March 27, 2006

(2) Resumen de los ítems de Certificación (Summary certification item)

DATA PERTINENT TO MODELS: EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC TC 8505 issued on 13 May 1985 in accordance with the following requirements: RBHA 25 Airworthiness Requirements for Aircraft Transport Category -corresponding to FAR 25 of Federal Aviation Administration, including amendment 25-1 through amendment 25- 54 effective 14 October 1980. Airplanes incorporating Embraer Service Bulletin No.120-025-0220 comply with RBHA/FAR 25.811(c)(2)(ii), Amendment 25-79, instead of RBHA/FAR 25.811(e)(3), Amendment 25-54. RBHA 21 - Certification Procedures for Aeronautical Products and Parts, Subpart B. SFAR 27 of Federal Aviation Administration, including amendment 27-1 through 27-5 effective 11 January 1984. Compliance has been shown with section 25.832 of FAR Part 25 amendment 25-56 effective 31 January 1983. Exemption for the RBHA/FAR 25.571(e)(2) has been granted in accordance with CTA letter 310-IFI/84 dated 11 April 1984.An equivalent safety finding has been established to RBHA/FAR 25.783(g)-cargo door. Compliance with the structural requirements for ditching, RBHA/FAR 25.801(b), (c), (d), (e), has been established. Compliance with the ice protection requirements, RBHA/FAR 25.1419, has been established. Noise Standards: - RBHA 36 - Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-12 effective 01 August 1981, applicable to EMB-12 and EMB-12R models. - RBHA 36 - Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-18 effective 18 August 1990, applicable to EMB-120ER model. - RBHA 36 - Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-22 effective 13 October 1999, applicable to EMB-120FC model. - RBHA 36 – Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-24, effective 07 August 2002, applicable to EMB-120QC model.



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Number Description ISSUE DATE

A120-DV-53 Engineering Basic Data B March 26, 1992

120-DV-15 Compliance Checklist F May 8, 1992

ISSUE PAPER A-19 Cargo Door Venting 1 August 7, 1985

TD0756IB-T-A-1 ELOS 1 May 05, 2010

TD0756IB-T-A-2 ELOS 1 May 05, 2010

3722 Exemption 1 May 22, 1983

(3) Documentación técnica del fabricante (Maintenance Manuals, Operating Manuals and Service Instructions)

Series Document Number Issue Date Revision

ALL

Airplane Flight Manual AFM-120/794 Oct 18, 2007 71

Operating Manual OM-120BAS/625 Sep 10, 2008 47

Wiring Manual WM-120ASA/709 Mar 01, 2012 30

Aircraft Maintenance Manual MM-120/1459 Mar 28, 2012 30

Aircraft Illustrated Parts

Catalogue IPC-120/1752 Jan 17, 2012 26

Structural Repair Manual SR–120/632 Sep 26, 2011 50

5. REQUERIMIENTOS ADICIONALES DE LOS RAC PARTE 4ª

(ADDITIONAL COLOMBIAN REQUIREMENTS RAC PART 4TH

)

A continuación se listan los requerimientos de aeronavegabilidad adicionales para la emisión de un certificado de aeronavegabilidad estándar, definidos en el capítulo II de la Parte Cuarta, “Requisitos generales de aeronavegabilidad” y Novena de los RAC. Compliance with the requirements for the expedition of a Standard Airworthiness Certificate, to operate in General Aviation, is according with RAC’s regulations inside its part IV, Chapters II, Rules.



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Norma (Rule)

Descripción del requerimiento ( Description)

4.2.2.3.

AERONAVES CIVILES MOTORIZADAS CON CERTIFICADO DE AERONAVEGABILIDAD ESTÁNDAR DE LA REPÚBLICA DE COLOMBIA (REQUISITOS DE INSTRUMENTOS Y EQUIPO) CIVILIAN ENGINE POWERED AIRCRAFT WITH COLOMBIAN STANDARD AIRWORTHINESS CERTIFICATE (INSTRUMENT AND EQUIPMENT REQUIREMENTS)

4.2.2.4.

TRANSMISOR LOCALIZADOR DE EMERGENCIA (ELT) Uno (fijo), transmisor de dos frecuencias (121.5 y 406.0 MHz). TSO – C126 EMERGENCY LOCATOR TRANSMITER (ELT) One (fixed) 2 frequencies transmitter (121.5 and 406.0 MHz). TSO – C126

4.2.2.5 LUCES DE AERONAVES AIRCRAFT’S LIGHTS

4.2.2.7 INSTRUMENTOS Y EQUIPOS INOPERATIVOS INOPERATIVE EQUIPMENTS AND INSTRUMENTS

4.2.2.8 USO DE TRANSPONDER ATC ATC TRANSPONDER RIGHT USE

4.2.2.10 SISTEMA DE ALERTA DE ALTITUD – Un sistema ALTITUDE ALERT SYSTEM – One system

4.2.2.14 SEÑALAMIENTO DE LAS ZONAS DE PENETRACION DEL FUSELAJE

4.5.6.26 REGISTRADORES DE DATOS DE VUELO (FDR) – Un sistema. TSO – C124A FLIGHT DATA RECORDER (FDR) – One system. TSO – C124A

4.5.6.33 REQUERIMIENTO DEL EQUIPO DE RADAR METEOROLOGICO – Un sistema WEATHER RADAR EQUIPMENT REQUERIMENTS – One system

4.5.6.34 GRABADORES DE VOZ EN LA CABINA DE MANDO (CVR) – Un sitema TSO – C123A COCKPIT VOICE RECORDER (CVR) – One system TSO – C123A

4.5.6.36 SISTEMA ALERTA DE TRAFICO Y ADVERTENCIA DE COLISION (ACAS II) – Un sistema TSO – C119 AIRBORNE COLLISION AVOIDANCE SYSTEM (ACAS II) – One system. TSO – C119

4.5.6.38

SISTEMA DE ADVERTENCIA Y ALERTA DEL TERRENO (TAWS) – Un sistama TSO – C151 TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) – One system. TSO – C151

9.2.3 literal d) 4

PLACAS: IDIOMA ESPAÑOL O ESPAÑOL E INGLES PLACARDS: SPANISH OR ENGLISH AND SPANISH

Type Validation Operational Limitations: All indicated in the following documents:

AFM120-794-FAA-SECTION 02 limitations. TYPE CERTIFICATE DATA SHEET Nº EA-8505



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APENDICE 1 - LISTA DE CHEQUEO DE AERONAVES (APPENDIX 1 – AIRCRAFT CHECK LIST)

CERTIFICADO TIPO (Type Certificate ):

ANAC Type Certificate No. 8505 and TCDS No.EA-8505-07 dated November 2004

AERONAVE (Aircraft): EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC,

FABRICANTE (Manufacturer):

Empresa Brasileira de Aeronáutica S/A EMBRAER Av Brigadeiro Faria Lima, 2170 Sao Jose dos Campos, SP - Brasil –CEP 12227-901 Contact: Eduardo Mayrink de Oliveira Airworthiness Engineer [email protected] Office: +55 12 3927 2567 - Mobile: + 55 12 8112 9955 (NEW)

www.embraer.com

PLANTA MOTRIZ (Engine):

Engine: Pratt & Withney PW118 FAA TC No E20NE Propeller: Hamilton Sundstrand 14RF-9 FAA TC No P11NE.

OPERADOR NACIONAL (National Operator):

NACIONAL DE AVIACION

FUNCIONARIO(s) (Team):

EDGAR CADENA ANDRES PARRA

REGULACIONES R.A.C. (R.A.C. Regulation):

Paragraph 9.1. d). Paragraph 9.2.3.

DOCUMENTACION (DOCUMENTS)

CUMPLIMIENTO (DOCUMENTOS REVISADOS)

1. DATOS GENERALES DEL CERTIFICADO TIPO

(Type Certificate Data Sheets):

REVISION ACTUAL (Actual Issue): 32 FECHA DE REVISION (Issue Date): Ene (Jan)28, 2010 \\Bog7\secretariasa\5102-Grupo Tecnico\2012\109 CONCEPTOS TECNICOS - ADMINISTRATIVOS\CONVALIDACIONES DE TC\EMB 120 BRASILIA

NUMERO DE PAX: Maximum of 30 passengers TRIBULATION: 2 (pilot and copilot) for all flight conditions TECHO DE SERVICIO: 9 750m (32 000 ft). WEIGTHS :

Model EMB-120 Model EMB-120RT

Ramp: 11 580 kg Take-off: 11 500 kg Landing: 11 250 kg Zero fuel: 10 900 kg

Model EMB-120ER Model EMB-120QC Model EMB-120FC

Ramp: 12 070 kg Take-off: 11 990 kg Landing: 11 700 kg Zero fuel: 10 900 kg

2. Lista de Chequeo De Conformidad Código De Aeronavegabilidad

EMBRAER COMPLIANCE CHECKLIST SUMMARY REPORT No 120-DV-15 DATED FEBRUARY 26 1985, APPLICABILITY EMB-120

http://www.embraer.com/



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(Compliance Check List airworthiness code):

3. Lista Maestra de Planos (Master Drawing List or Type Build Standard (TBS)):

EMBRAER ENGINEERING BASIC DATA REPORT No 120-DV-53 REVISION B MARCH 26 1992 APPLICABILITY EMB-120

4. NIVELES EQUIVALENTES DE SEGURIDAD (Equivalent Level Of Safety –ELOS)

Number Description Model Date

TD0756IB-T-A-1 Repairs to fatigue critical

structure ALL May 05, 2010

TD0756IB-T-A-2 Sections 26.45, 26.47(d) and

26.47(d)(1) ALL May 05, 2010

5. EXCEPCIONES

(Exceptions)

Exemption No. 3722 for section 25.571(e)(2) of the Federal Aviation Regulations to permit type certification of the Embraer Model EMB-120 without showing that the airplane is capable of successfully completing a flight during which likely structural damage occurs as a result of propeller blade impact.

6. Plano en tres vistas del

conjunto (impreso o copia) (views assembly drawing (Printed or blueprint)):

Ver APENDICE 2 - ADJUNTOS See APPENDIX 2 - ATTACHMENTS

7. Planos de Configuración Interior (Interior configuration Drawings (LOPA):

8. Manual De Operación De La Aeronave (Aircraft Operacional

Pilots Operating Handbook



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Manuals): Document Number Issue Date Revision

Airplane Flight Manual AFM-120/794 Oct 18, 2007 71

Operating Manual OM-120BAS/625 Sep 10, 2008 47

Wiring Manual WM-120ASA/709 Mar 01, 2012 30

9. Manual de Cableado ( Wiring Manual): Wiring Manual WM-120ASA/709

Mar 01, 2012

30

10. MANUAL DE MANTENIMIENTO (Maintenance Manual):

Aircraft Maintenance Manual MM-120/1459

Mar 28, 2012

30

11. CATALOGO ILUSTRADO DE PARTES (Illustrated Parts Catalogue):

Aircraft Illustrated Parts

Catalogue IPC-120/1752 Jan 17, 2012 26

12. BOLETINES DE SERVICIO,

( Service Bulletins):

Service Bulletins www.flyembraer.com

13. DIRECTIVAS DE AERONAVEGABILIDAD (Airworthiness Directives):

PAGINA WEB ANAC : http://www.anac.gov.br/

14. CERTIFICACION DE RUIDO (Noise Compliance):

See POH Section 4-26

15. OTROS (Others RVSM, PBN, IFR, etc):

RVSM. Not applicable. The airplane is certificated in the transport category, in the following conditions, both day and night, when the appropriate equipment and instruments required by the airworthiness and operating regulations are approved, installed and in an operable condition: Visual (VFR); Instrument (IFR) and Icing Conditions. (See AFM)

16. BASES DE CERTIFICACIÓN (Certification Bases) :

DATA PERTINENT TO MODELS: EMB-120, EMB-120RT, EMB-120ER, EMB-120FC and EMB-120QC TC 8505 issued on 13 May 1985 in accordance with the following requirements: RBHA 25 Airworthiness Requirements for Aircraft Transport Category -corresponding to FAR 25 of Federal Aviation Administration, including amendment 25-1 through amendment 25- 54 effective 14 October 1980. Airplanes incorporating Embraer Service Bulletin No.120-025-0220 comply with RBHA/FAR 25.811(c)(2)(ii), Amendment 25-79, instead of RBHA/FAR 25.811(e)(3), Amendment 25-54. RBHA 21 - Certification Procedures for Aeronautical Products and Parts, Subpart B. SFAR 27 of Federal Aviation Administration, including amendment 27-1 through 27-5 effective 11 January 1984. Compliance has been shown with section 25.832 of FAR Part 25 amendment 25-56 effective 31 January 1983. Exemption for the RBHA/FAR 25.571(e)(2) has been granted in accordance with CTA letter 310-IFI/84 dated 11 April 1984.An equivalent safety finding has been established to RBHA/FAR 25.783(g)-cargo door. Compliance with the structural requirements for ditching, RBHA/FAR 25.801(b), (c), (d), (e), has been established. Compliance with the ice protection requirements, RBHA/FAR 25.1419, has been established. Noise Standards: - RBHA 36 - Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-12 effective 01 August 1981, applicable to EMB-12 and EMB-12R models. - RBHA 36 - Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-18 effective 18 August 1990, applicable to EMB-120ER model. - RBHA 36 - Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-22 effective 13 October 1999, applicable to EMB-120FC model. - RBHA 36 – Noise Standard - Type Certification – corresponding to FAR Part 36 of Federal Aviation Administration, including amendment 36-1 through 36-24, effective 07 August 2002, applicable to EMB-120QC model.

http://www.flyembraer.com/

http://www.anac.gov.br/



GSAC-4.0-8-02 Versión: 01 26/05/2009

APENDICE 2 - ADJUNTOS (APPENDIX 2 - ATTACHMENTS) Los siguientes documentos son adjuntos de este informe: The following documents are attached to this report:

Copia del Certificado de homologación de tipo de ANAC, Numero 8505 Copy of ANAC Type Homologation Certificate, Number 8505.

Copia de la Hoja de Datos del Certificado Tipo para el motor Numero E-20NE (Pratt & Whitney Canada Engines). Copy of TCCA Engine Type Certificate Data Sheet, Number E20NE (Pratt & Whitney Canada Engines).

Copia de la Hoja de Datos del Certificado Tipo para la hélices número P11NE (Hamilton Sundstrand 14RF-9). Copy of TCCA Propeller Type Certificate Data Sheet, Number P11NE (Hamilton Sundstrand 14RF-9).

Otros: Vista planos en 3 dimensiones.

(Other): Airplane Drawing Three Views.

Firmas (Signatures)

…………………………............... Andres E. Parra Catama Inspector de Seguridad Aérea (UAEAC – Air Safety Inspector)

Dated: July 5, 2012

……………………….............. Edgar L. Cadena Cañón Jefe de Grupo Técnico (UAEAC- Technical Group Chief)



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GSAC-4.0-8-02 Versión: 01 26/05/2009

Airplane Drawing Three Views.

reporte de aceptación de certificado tipo · s/a - embraer are in compliance with the icao annexes...

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