Airworthiness directives › 2004-01-02
AD 2004-01-02 Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
Models named: 767-200, -300, -300F series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model 767-200, -300, and -300F series airplanes, as listed in Boeing Alert Service Bulletin 767-54A0102, dated November 8, 2001; certificated in any category.
Compliance
Required as indicated, unless accomplished previously. To prevent loss of the fuse pin of the aft pitch load fitting of the diagonal brace, which could result in increased loads in the wing-to-strut joints and consequent separation of the strut and engine from the wing, accomplish the following: Modification (a) Within 24 months after the effective date of this AD: Modify the aft pitch load fitting of the diagonal brace of the nacelle strut of each wing (including dye penetrant inspections for cracking or damage of the fitting; reworking the fitting if cracking or damage is found; honing, chamfering, measuring, and machining the fitting if no cracking or damage is found; and replacing the bushing and fuse pin with new components) by accomplishing all of the actions specified in paragraphs 3.A. through 3.J. of the Accomplishment Instructions of Boeing Alert Service Bulletin 767-54A0102, dated November 8, 2001. Clarifications to the work required by this paragraph may be used per Boeing Information Notice 767-54A0102 IN 01, dated July 18, 2002; and per Boeing Information Notice 767-54A0102 IN 02, dated August 29, 2002. Alternate sealants are allowed when accomplishing the actions required by paragraphs 3.A. through 3.J. of the service bulletin, per Section 51-20-05, Figure 8, dated August 15, 2002, of the Boeing 767-200, 767-300, and 767-300F Structural Repair Manuals. Any applicable follow-on corrective actions must be done before further flight. Alternative Methods of Compliance (b) In accordance with 14 CFR 39.19, the Manager, Seattle Aircraft Certification Office, FAA, is authorized to approve alternative methods of compliance (AMOCs) for this AD. Incorporation by Reference (c) Unless otherwise specified in this AD, the actions shall be done in accordance with Boeing Alert Service Bulletin 767-54A0102, dated November 8, 2001. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Effective Date (d) This amendment becomes effective on February 13, 2004. Issued in Renton, Washington, on December 29, 2003. Ali Bahrami, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-122 Filed 1-8-04; 8:45 am] BILLING CODE 4910-13-P
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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