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AD 90-06-12 ACTIVE

Bulkhead Splice Strap
Key Information
AD Number 90-06-12 Status Active
Effective Date April 13, 1990 Issue Date Not specified
Docket Number 89-NM-195-AD Amendment 39-6531
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) 747-100 Series 747-100B Series 747-100B SUD Series 747-200B Series 747-200C Series 747-200F Series 747-300 Series 747-400 Series 747-400D Series 747-400F Series 747SP Series 747SR Series
Regulatory Text

90-06-12 BOEING: Amendment 39-6531. Docket No. 89-NM-195-AD. \n\n\tApplicability: Model 747 series airplanes, line position 676, 679, 685, and 690 through 699, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent cracking of the bulkhead splice strap, accomplish the following: \n\n\tA.\tWithin the next 1,000 flight cycles after the effective date of this AD, perform an interim modification of the body station 1241 bulkhead in accordance with Boeing Service Bulletin 747-53-2299, Revision 1, dated June 29, 1989. \n\n\tB.\tWithin the next 5,000 flight cycles after the effective date of this AD, perform an eddy current inspection for cracks of the splice strap in accordance with Boeing Service Bulletin 747-53-2299, Revision 1, dated June 29, 1989. \n\n\t\t1.\tIf no cracking is found, prior to further flight, perform permanent modification in accordance with Boeing Service Bulletin 747-53-2299, Revision 1, dated June 29, 1989.2.\tIf cracking is found, prior to further flight, repair in accordance with method approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tC.\tAccomplishment of paragraph B., above, within the next 1,000 flight cycles after the effective date of this AD, is an acceptable alternative to the interim modification required by paragraph A., above. \n\n\tD.\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\tE.\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 the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis amendment (39-6531, AD 90-06-12) becomes effective on April 13, 1990.