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US-2024-20-02 : Fuselage - Aft Fuselage Cant Bulkhead at Certain Stations and Vertical Stabilizer Rear Spar Structure - Inspection

Number US-2024-20-02
Issued by United States of America  United States of America
Issue date 2024-10-15
Effective date 2024-10-21
EASA approval number
ATA Chapter 53
Approval Holder
/ Type Designation
  • BOEING
    • 717
      • 717-200
    • DC-9
      • DC-9-11
      • DC-9-12
      • DC-9-13
      • DC-9-14
      • DC-9-15
      • DC-9-15F
      • DC-9-21
      • DC-9-31
      • DC-9-32
      • DC-9-32F
      • DC-9-33F
      • DC-9-34
      • DC-9-34F
      • DC-9-41
      • DC-9-51
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Boeing Multi Operator Message MOM-MOM-24-0456-01B(R1), dated September 4, 2024. Boeing Multi Operator Message MOM-MOM-24-0457-01B(R1), dated September 4, 2024. For Boeing material identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; website myboeingfleet[dot]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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