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AD 88-19-03 R1 SUPERSEDED

Bulkhead
WARNING: This AD has been superseded and is no longer active. Replaced by: 2004-05-10. Refer to the superseding AD(s) for current requirements.
Key Information
AD Number 88-19-03 R1 Status Superseded
Effective Date April 13, 1990 Issue Date Not specified
Docket Number 89-NM-156-AD Amendment 39-6532
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) 767 Series (all)
Related Airworthiness Directives
Superseded By 2004-05-10
Regulatory Text

88-19-03 R1 BOEING: Amendment 39-6001 as revised by Amendment 39-6532. Docket No. 89-NM-156-AD.\n \n\tApplicability: Model 767 series airplanes, line numbers 001 through 175, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent a condition that could lead to depressurization of the airplane, accomplish the following: \n\n\tA.\tPrior to the accumulation of 6,000 flight cycles or within the next 1,000 flight cycles after September 26, 1988, (effective date of Amendment 39-6001), whichever occurs later, unless accomplished within the last 5,000 flight cycles, and thereafter at intervals not to exceed 6,000 flight cycles, perform a detailed visual inspection of the aft side of the entire body station 1582 pressure bulkhead for damage (as defined in the Structural Repair Manual) and cracking, in accordance with Boeing Service Bulletin 767-53-0026, dated November 19, 1987, or Revision 1, dated March 16, 1989. \n\n\tB.\tPriorto the accumulation of 25,000 flight cycles, and thereafter at intervals not to exceed 6,000 flight cycles, perform an eddy current inspection of the body station 1582 pressure bulkhead, in accordance with paragraph C. of the Accomplishment Instructions of Boeing Service Bulletin 767-53-0026, Revision 1, dated March 16, 1989. \n\n\tC.\tRepair all damage and cracking prior to further flight in accordance with NOTE 4 in the Accomplishment Instructions of Boeing Service Bulletin 767-53-0026, Revision 1, dated March 16, 1989. \n\n\tD.\tFor the purpose of complying with this AD, the number of flight cycles may be determined to equal the number of pressurization cycles where the cabin pressure differential was equal to or greater than 2.0 PSI. \n\n\tE.\tAn alternate means 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, FAA, Northwest Mountain Region. \n\n\tNOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment, and then send it to the Manager, Seattle Aircraft Certification Office. \n\n\tF.\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. \n\n\tAll persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis AD revises AD 88-19-03, Amendment 39-6001. \n\tThis amendment (39-6532, AD 88-19-03 R1) becomes effective on April 13, 1990.