Airworthiness directives › 2018-06-07
AD 2018-06-07 Airworthiness Directives; The Boeing Company Airplanes
Models named: 757-200, -200CB, -300 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to The Boeing Company Model 757-200, -200CB, and -300 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
(1) For all airplanes except those identified in paragraphs (g)(2) and (g)(3) of this AD: Do all applicable actions identified as “RC” (required for compliance) in, and in accordance with, the Accomplishment Instructions of Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016; except as provided by paragraphs (h)(1) and (h)(4) of this AD. Do the actions at the applicable times specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016, except as provided by paragraph (h)(2) of this AD. (2) For airplanes on which Aviation Partners Boeing (APB) Alert Service Bulletin AP757-53-001, Revision 1, dated June 21, 2017, blended or scimitar blended winglets are installed in accordance with Supplemental Type Certificate ST01518SE: Do all applicable actions identified as “RC” (required for compliance) in, and in accordance with, the Accomplishment Instructions of APB Alert Service Bulletin AP757-53-001, Revision 1, dated June 21, 2017; and Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016; except as provided by paragraphs (h)(1) and (h)(4) of this AD. Do the actions at the applicable times specified in paragraph 1.E., “Compliance,” of APB Alert Service Bulletin AP757-53-001, Revision 1, dated June 21, 2017, except as provided by paragraph (h)(3) of this AD. (3) For airplanes that have been converted from passenger to freighter configuration in accordance with VT Mobile Aerospace Engineering (VT MAE) Supplemental Type Certificate ST03562AT: Do all applicable actions identified as “RC” in, and in accordance with, the Accomplishment Instructions of Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016; except as provided by paragraphs (h)(1) and (h)(4) of this AD. Do the actions at the applicable times specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016, except as provided by paragraph (h)(2) of this AD. Where Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016, refers to Group 1 airplanes, the tasks identified under Group 2 airplanes must be done instead; where Boeing Alert Service Bulletin 757-53A0108, dated November 14, 2016, refers to Group 4 airplanes, the tasks identified under Group 5 airplanes must be done instead.
Unsafe condition
This AD was prompted by a report of fatigue cracking found in the fuselage frame at station (STA) 1640, which severed the inner chord and web. We are issuing this AD to detect and correct cracking of the fuselage frame at STA 1640, which could result in reduced structural integrity of the airplane.
Affected ADs
None.
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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