Airworthiness directives › 2019-24-16
AD 2019-24-16 Airworthiness Directives; Embraer S.A. Airplanes
Models named: ERJ 190-100 STD, -100 LR, -100 ECJ, -100 IGW, ERJ 190-200 STD, -200 LR, -200 IGW. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Embraer S.A. Model ERJ 190-100 STD, -100 LR, -100 ECJ, and -100 IGW airplanes; and Model ERJ 190-200 STD, -200 LR, and -200 IGW airplanes; certificated in any category; serial numbers 19000002, 19000004, 19000006 through 19000213 inclusive, 19000215 through 19000276 inclusive, 19000278 through 19000466 inclusive, 19000468 through 19000525 inclusive, and 19000527 through 19000758 inclusive.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
This paragraph restates the requirements of paragraph (i) of AD 2017-16-08, with no changes. For airplanes having serial numbers 19000002, 19000004, 19000006 through 19000213 inclusive, 19000215 through 19000276 inclusive, 19000278 through 19000466 inclusive, 19000468 through 19000525 inclusive, and 19000527 through 19000696 inclusive, do the revision required by paragraph (g)(1) or (2) of this AD, as applicable. (1) For Model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-200 STD, ERJ 190-200 LR, and ERJ 190-200 IGW airplanes: Within 90 days after October 11, 2017 (the effective date of AD 2017-16-08), revise the existing maintenance or inspection program, as applicable, to incorporate the tasks specified in Part 2—Airworthiness Limitation Inspections—Structures, of Appendix A—Airworthiness Limitations (AL), of the EMBRAER 190/195 Maintenance Review Board Report, MRB-1928, Revision 9, dated August 14, 2015 (“MRB-1928, Revision 9”); EMBRAER MRB—Temporary Revision 9-1, dated October 27, 2015, to Part 2—Airworthiness Limitation Inspections—Structures, and Part 4—Life Limited Items, of Appendix A—Airworthiness Limitations (AL), of MRB-1928, Revision 9; and EMBRAER MRB—Temporary Revision 9-3, dated October 27, 2015, to Part 2—Airworthiness Limitation Inspections—Structures, of Appendix A—Airworthiness Limitations (AL), of MRB-1928, Revision 9; with the thresholds and intervals stated in these documents. The initial compliance times for the tasks are at the later of the times specified in paragraphs (g)(1)(i) and (ii) of this AD. (i) Within the applicable times specified in MRB-1928, Revision 9; EMBRAER MRB—Temporary Revision 9-1, dated October 27, 2015, to Part 2—Airworthiness Limitation Inspections—Structures, and Part 4—Life Limited Items, of Appendix A—Airworthiness Limitations (AL), of MRB-1928, Revision 9; and EMBRAER MRB—Temporary Revision 9-3, dated October 27, 2015, to Part 2—Airworthiness Limitation Inspections—Structures, of Appendix A—Airworthiness Limitations (AL), of MRB-1928, Revision 9. Where tasks are listed in both MRB-1928, Revision 9, and a temporary revision, the compliance times in the temporary revision take precedence. (ii) Within 90 days or 600 flight cycles after October 11, 2017 (the effective date of AD 2017-16-08), whichever occurs later. (2) For Model ERJ 190-100 ECJ airplanes: Within 90 days after October 11, 2017 (the effective date of AD 2017-16-08), revise the maintenance or inspection program, as applicable, to incorporate the tasks specified in Part 1—Certification Maintenance Requirements, Part 2—Airworthiness Limitation Inspections—Structures, Part 3—Fuel System Limitation Items, and Part 4—Life Limited Items, of Appendix A— Airworthiness Limitations (AL), of the EMBRAER Lineage 1000/1000E Maintenance Planning Guide, MPG-2928, Revision 4, dated July 14, 2014; EMBRAER MPG—Temporary Revision 4-2, dated February 13, 2015; and EMBRAER MPG—Temporary Revision 4-3, dated October 30, 2015; with the thresholds and intervals stated in these documents. The initial compliance times for the tasks are at the later of the times specified in paragraphs (g)(2)(i) and (ii) of this AD. (i) Within the applicable times specified in Part 1, Certification Maintenance Requirements, Part 2, Airworthiness Limitation Inspections—Structures, Part 3, Fuel System Limitation Items, and Part 4, Life Limited Items, of Appendix A—Airworthiness Limitations (AL), of the EMBRAER Lineage 1000/1000E Maintenance Planning Guide, MPG-2928, Revision 4, dated July 14, 2014; EMBRAER MPG—Temporary Revision 4-2, dated February 13, 2015; and EMBRAER MPG—Temporary Revision 4-3, dated October 30, 2015. Where tasks are listed in both MPG-2928, Revision 4, and a temporary revision, the compliance times in the temporary revision take precedence. (ii) Within 90 days or 600 flight cycles after October 11, 2017 (the effective date AD 2017-16-08), whichever occurs later.
Unsafe condition
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address fatigue cracking of structural components and to address failure of certain system components, which could result in reduced structural integrity and system reliability of the airplane.
Affected ADs
This AD replaces AD 2017-16-08, Amendment 39-18985 (82 FR 42021, September 6, 2017) (“AD 2017-16-08”).
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1