Airworthiness directives › 2019-23-06
AD 2019-23-06 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 Requirements Bulletin 757-53A0112 RB, dated November 16, 2018.
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) through (4) of this AD: Except as specified by paragraph (h) of this AD, at the applicable times specified in the “Compliance” paragraph of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018. Note 1 to paragraphs (g)(1) through (4): Guidance for accomplishing the actions required by this AD can be found in Boeing Alert Service Bulletin 757-53A0112, dated November 16, 2018, which is referred to in Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018. Note 2 to paragraphs (g)(1) through (4): Accomplishing certain repairs required by this AD might affect AD 2018-06-07, Amendment 39-19227 (83 FR 13398, March 29, 2018) (“AD 2018-06-07”), and necessitate requesting an alternative method of compliance (AMOC) to AD 2018-06-07. (2) For airplanes on which Aviation Partners Boeing (APB) blended or scimitar blended winglets are installed in accordance with Supplemental Type Certificate (STC) ST01518SE: Except as specified by paragraph (h) of this AD, at the applicable times specified in paragraph 1.E., “Compliance” of APB Alert Service Bulletin AP757-53-002, Revision 3, dated August 14, 2019, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018. (3) Except as specified by paragraph (h) of this AD: For Group 1 airplanes that have been converted from a passenger to freighter configuration using VT Mobile Aerospace Engineering (MAE) Inc. STC ST03562AT, at the applicable times specified for Group 2 airplanes in the “Compliance” paragraph of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018, do all applicable Group 2 actions, as identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018. (4) Except as specified by paragraph (h) of this AD: For Group 4 airplanes that have been converted from a passenger to freighter configuration using VT MAE Inc. STC ST03562AT, at the applicable times specified for Group 5 airplanes in the “Compliance” paragraph of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018, do all applicable Group 5 actions as identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 757-53A0112 RB, dated November 16, 2018.
Unsafe condition
This AD was prompted by reports of cracks initiating in the fuselage frame web at body station (STA) 1640. The FAA is issuing this AD to address cracks initiating in the fuselage frame web at STA 1640, which, if not detected and corrected, 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