Source: https://www.federalregister.gov/articles/2011/12/29/2011-33279/airworthiness-directives-empresa-brasileira-de-aeronautica-sa-embraer-airplanes
Timestamp: 2015-07-30 23:06:42
Document Index: 705974352

Matched Legal Cases: ['§ 39', 'art 2', 'art 2', 'art 2', 'art 2', 'art 2', 'art 2']

Federal Register | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Airplanes
-81897 (4 pages)
Shorter URL: https://federalregister.gov/a/2011-33279 Related Topics
Restatement of Requirements of AD 2010-11-13, Amendment39-16318 (75 FR 30284, June 1, 2010):
For service information identified in this proposed AD, contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), Technical Publications Section (PC 060), Av. Brigadeiro Faria Lima, 2170-Putim-12227-901 São Jose dos Campos-SP-BRASIL; telephone +55 12 3927-5852 or +55 12 3309-0732; fax +55 12 3927-7546;email: distrib@embraer.com.br; Internet: http://www.flyembraer.com. You may review copies of the referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call (425) 227-1221.
Cindy Ashforth, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 227-2768; fax(425) 227-1320.
Since we issued AD 2010-11-13, Amendment 39-16318 (75 FR 30284,June 1, 2010): The Agência Nacional de Aviação Civil (ANAC), which is the aviation authority for Brazil, has issued Brazilian Airworthiness Directive 2011-04-01, datedMay 5, 2011 (referred to after this as “the MCAI”), to correct an unsafe condition for the specified products. The MCAI states:
2. The FAA amends § 39.13 by removing Amendment 39-16318 (75 FR 30284, June 1, 2010) and adding the following new AD:
This AD supersedes AD 2010-11-13, Amendment 39-16318 (75 FR 30284,June 1, 2010)
Restatement of Requirements of AD 2010-11-13, Amendment39-16318 (75 FR 30284, June 1, 2010): Back to Top
Table 1—Inspection Tasks Back to Top
Ram air turbine compartment, support structure and cutout structure-internal Nose landing gear wheel well metallic structure
53-10-012-0002 53-10-012-0003
53-10-021-0005
Wing stub spar 3 side fitting—internal Wing upper skin panels—external
Fixed trailing edge lower skin panel—external
Fixed trailing edge rib 4A—external
Fixed trailing edge rib 6—internal
57-01-012-001 57-10-010-0002
57-50-002-0002
57-50-005-0003
57-50-005-0004
Wing stub main box lower—internal
57-01-002-003
(h) No Alternative Inspections for Paragraph (g) of This AD Back to Top
(i) Revision of the Maintenance Program Back to Top
Within 60 days after the effective date of this AD: Revise the maintenance program to incorporate the new or revised tasks specified in Part 2—Airworthiness Limitation Inspection (ALI)—Structures, of Appendix A, Airworthiness Limitations of the EMBRAER 170 MRBR MRB-1621, Appendix A, Part 2, Airworthiness Limitations, Revision 7, dated November 11, 2010; and Temporary Revision (TR) 7-1, dated February 11, 2011, to Part 2—Airworthiness Limitation Inspection (ALI)—Structures, of Appendix A, Airworthiness Limitations of the EMBRAER 170 MRBR MRB-1621, Revision 7, dated November 11, 2010, with the initial compliance times and intervals stated in these documents. The initial compliance times for the tasks start from the date of issuance of the original Brazilian airworthiness certificate or the date of issuance of the original Brazilian export certificate of airworthiness of the applicable airplane at the applicable time specified in the tasks, or within 600 flight cycles after revising the maintenance program, whichever occurs later. For certain tasks, the compliance times depend on the pre-modification and post-modification status of the actions specified in the associated service bulletin, as specified in the “Applicability” column of Part 2—Airworthiness Limitation Inspection (ALI)—Structures, of Appendix A, Airworthiness Limitations of the EMBRAER 170 MRBR MRB-1621, Appendix A, Part 2, Airworthiness Limitations, Revision 7, dated November 11, 2010; and Temporary Revision (TR) 7-1, dated February 11, 2011, to Part 2—Airworthiness Limitation Inspection (ALI)—Structures, of Appendix A, Airworthiness Limitations of the EMBRAER 170 MRBR MRB-1621, Revision 7, dated November 11, 2010. For tasks identified in the documents identified in this paragraph, doing the initial task required by this paragraph terminates the requirements of paragraph (g) of this AD for that task. (j) No Alternative Actions Intervals, and/or Critical Design Configuration Control Limitations (CDCCLs) Back to Top