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US-2008-03-12 : Rudder Pedal Bracket Assemblies - Inspection / Replacement

Number US-2008-03-12
Issued by United States of America  United States of America
Issue date 2008-02-18
Effective date 2008-03-11
EASA approval number
ATA Chapter 27
Approval Holder
/ Type Designation
  • BOEING
    • DC-8
      • DC-8-11
      • DC-8-12
      • DC-8-21
      • DC-8-31
      • DC-8-32
      • DC-8-33
      • DC-8-41
      • DC-8-42
      • DC-8-43
      • DC-8-51
      • DC-8-52
      • DC-8-53
      • DC-8-55
      • DC-8-61
      • DC-8-61F
      • DC-8-62
      • DC-8-62F
      • DC-8-63
      • DC-8-63F
      • DC-8-71
      • DC-8-71F
      • DC-8-72
      • DC-8-72F
      • DC-8-73
      • DC-8-73F
      • DC-8F-54
      • DC-8F-55
    • 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
      • DC-9-81
      • DC-9-82
      • DC-9-83
      • DC-9-87
    • MD-88
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 2006-07-25 dated 11 April 2006.
Publication(s) and related information McDonnell Douglas DC-8 Alert Service Bulletin (ASB) A27-273, Revision 5, dated February 18, 1993, and Boeing ASB DC9-27A307, Revision 7, dated August 29, 2006. Contact Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024), for a copy of this service information.
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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