AD 92-12-03

Active

Fuselage Frames Inspection

Key Information
92-12-03
Active
July 23, 1992
Not specified
91-NM-79-AD
39-8263
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
727-100 Series 727-100C Series 727-200 Series 727-200F Series 727 Series 727C Series
Regulatory Text

92-12-03 BOEING: Amendment 39-8263. Docket No. 91-NM-70-AD. Supersedes AD 90-06-16, Amendment 39-6545.\n\n\tApplicability: Model 727 airplanes, certificated in any category.\n\n\tCompliance: Required as indicated, unless accomplished previously.\n\n\tTo prevent cracking in the fuselage aft lower lobe frames between body stations (BS) 950 and BS 1166, accomplish the following:\n\n\t(a)\tConduct a detailed visual inspection of the fuselage frames in accordance with Part I of the Accomplishment Instructions of Boeing Alert Service Bulletin 727-53A0195, dated May 4, 1989; or Revision 1, dated September 19, 1991; prior to the time specified in subparagraph (a)(1) or (a)(2) of this AD, whichever occurs first.\n\n\t\t(1)\tPrior to the time specified in subparagraph (a)(1)(i) or (a)(1)(ii) of this AD, whichever occurs later:\n\n\t\t\t(i)\tWithin the next 3,000 flight cycles or 15 months after April 24, 1990 (the effective date of AD 90-06-16, Amendment 39-6545), whichever occurs first; or\n\n\t\t\t(ii)\tPrior to the accumulation of 40,000 flight cycles.\n\n\t\t(2)\tPrior to the time specified in subparagraph (a)(2)(i) or (a)(2)(ii) of this AD, whichever occurs later:\n\n\t\t\t(i)\tWithin the next 3,000 flight cycles or 24 months after the effective date of this AD, whichever occurs first; or\n\n\t\t\t(ii)\tPrior to the accumulation of 28,000 flight cycles.\n\n\t(b)\tRepeat the inspection required by paragraph (a) of this AD at intervals not to exceed 4,000 flight cycles or 36 months, whichever occurs first.\n\n\t(c)\tIf any cracks are detected, repair prior to further flight, in accordance with Part I of the Accomplishment Instructions of Boeing Alert Service Bulletin 727-53A0195, dated May 4, 1989; or Revision 1, dated September 19, 1991. Skin repairs must be accomplished in accordance with Section 53-30-3 of the Boeing 727 Structural Repair Manual.\n\n\t(d)\tAccomplishment of repairs in accordance with Boeing Alert Service Bulletin 727-53A0195, dated May 4, 1989; or Revision 1, dated September 19, 1991; constitutes terminating action for the inspections required by paragraphs (a) and (b) of this AD for the repaired areas only.\n\n\t(e)\tAccomplish the preventive modification in accordance with Part I, Paragraph B., of the Accomplishment Instructions of Boeing Alert Service Bulletin 727-53A0195, Revision 1, dated September 19, 1991, prior to the time specified in subparagraph (e)(1) or (e)(2) of this AD, whichever occurs later:\n\n\t\t(1)\tWithin the next 7,500 flight cycles or 45 months after the effective date of this AD, whichever occurs first; or\n\n\t\t(2)\tPrior to the accumulation of 47,500 flight cycles.\n\n\t(f)\tAccomplishment of the preventive modification required by paragraph (e) of this AD constitutes terminating action for the inspections required by this AD for the modified area only.\n\n\t(g)\tAn alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO.\n\n\t(h)\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.\n\n\t(i)\tThe inspections, repairs, and modifications shall be done in accordance with Boeing Alert Service Bulletin 727-53A0195, dated May 4, 1989; or Boeing Alert Service Bulletin 727-53A0195, Revision 1, dated September 19, 1991. 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. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC.\n\n\t(j)\tThis amendment becomes effective on July 23, 1992.

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References
--- - Part 39
FAA Documents