Form F - 900 - 04F 

### AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL
– BRAZIL 

## BRAZILIAN AIRWORTHINESS DIRECTIVE AD No.: 2012 - 0 8 - 0 3 Effective Date: 05 Sep . 2012 The following Brazilian Airworthiness Directive (AD), issued by the Agência Nacional de Aviação Civil (ANAC) in accordance with provisions of Chapter IV, Title III of Código Brasileiro de Aeronáutica
- Law No. 7,565 dated 19 December 1986
- and Regulamento Brasileiro d a Aviação Civil (RB AC ) 39, applies to all aircraft registered in the Registro Aeronáutico Brasileiro. No person m ay operate an aircraft to which this AD applies, unless it has previously complied with the requirements established herein.

AD No. 2012 - 0 8 - 0 3 - EMBRAER / 39 - 13 60 . APPLICABILITY: This Airworthiness Directive applies to EMBRAER S.A. model ERJ 190

- 100 ECJ, ERJ 190

- 100 STD, ERJ 190

- 100 LR, ERJ 190

- 100 IGW, ERJ 190

- 100 SR, ERJ 190

- 200 STD, ERJ 190

- 200 LR, and ERJ 190

- 200 IGW airplanes; as identified in Embraer Service Bulletin (SB) 190

- 52

- 0038, Revision 01 and 190LIN

- 52

- 0020, both dated August 01, 2011, as app licable.

CANCELLATION / REVISION: Not applicable. REASON: This AD was prompted by reports of cockpit door falling off the hinges when it is being opened or closed. If not corrected, this condition may cause injury to the occupants.

Since this condition may occur in other airplanes of the same type and affects flight safety, a corrective action is required. Thus, sufficient reason exists to request compliance with this AD in the indicated time limit.

REQUIRED ACTION: Replacement of cockpit door passive lock striker, quick

- release pin and hinges. COMPLIANCE: You are required to do the following actions, unless already accomplished: Replacement of cockpit door passive lock striker, quick - release pin and hinges (a) Within 1500 flight hours after the effective date o f this AD, do the actions required by paragraphs (a)(1) and (a)(2) of this AD. (1) Replace the cockpit door passive lock striker and quick

- release pin according to Part I of the Accomplishment Instructions of Embraer SB 190

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- 0038, Revision 01, or 190LIN

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- 0020, both dated August 01, 2011, as applicable, or further revision approved by the ANAC; and (2) Replace the cockpit door upper and lower hinges in accordance with Part III of the Accomplishment Instructions of Embraer SB 190

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- 0038, Revision 01, or 190L IN

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- 0020, both dated August 01, 2011, as applicable, or further revision approved by the ANAC. Material Incorporated by Reference (b) You must use Embraer SB 190

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- 0038, Revision 01, or 190LIN

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- 0020, both dated August 01, 2011, as applicable, or further r evision approved by the ANAC, to do the actions required by this AD, unless the AD specifies otherwise.CONTINUATION OF AD N o .: 2012 - 0 8 - 0 3 / 39 - 1 3 60 PAGE N o .: 2 / 2

Form F - 900 - 04F Credit for Previous Actions (c) This paragraph provides credit for the actions required by paragraph (a)(1) of this AD, if those actions were performed befo re the effective date of this AD, using Embraer SB 190

- 52

- 0038, dated February 10, 2011. Alternative Means of Compliance (AMOC) (d) A different method or a different compliance time, with the requirements of this AD, may be used if approved by the General Mana ger of the Aeronautical Product Certification Branch (Gerência

Geral de Certificação de Produtos Aeronáuticos

– GGCP).

CONTACT: For additional technical information, contact: National Civil Aviation Agency (ANAC) Aeronautical Products Certification Branc h (GGCP) Av. Cassiano Ricardo, 521, Bloco B, 2 o andar, Parque Residencial Aquarius Fax: 55 (12) 3797

- 2330 12246

- 870

– São José dos Campos

- SP , BRAZIL
. E

- mail: p ac @anac.gov.br APPROVAL: HÉLIO TARQUÍNIO JÚNIOR General Manager GGCP DINO ISHIKURA Airworth iness Superintendent

ANAC
NOTE: Original in Portuguese language signed and available in the files of the Aeronautical Products Certification Branch (GGCP) of the National Civil Aviation Agency (ANAC).