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US-2012-16-12 : Nacelles / Pylons - Nacelle Strut - Inspection

Number US-2012-16-12
Issued by United States of America  United States of America
Issue date 2012-09-06
Effective date 2012-09-21
EASA approval number
ATA Chapter 54
Approval Holder
/ Type Designation
  • BOEING
    • 707
      • 707-100
      • 707-100B
      • 707-200
      • 707-300
      • 707-300B
      • 707-300C
      • 707-400
    • 720
      • 720
      • 720B
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information (i) Boeing 707 Alert Service Bulletin A3537, dated January 30, 2012. (ii) Figure 24, Steel Part Surface Inspection (Impedance Plane Display), Subject 51-00-00, Structural–General, of Part 6, Eddy Current, of the Boeing 707/720 Nondestructive Test Manual, Document D6-48023, Revision 120, dated March 15, 2012. The revision level of this document is identified on only the manual revision Transmittal Sheet. For The Boeing Company service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

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