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US-2008-21-11 : Skin doubler pads and deflectors on low-pressure turbine (LPT) cases - Rework / Installation

Number US-2008-21-11
Issued by United States of America  United States of America
Issue date 2008-10-28
Effective date 2008-11-28
EASA approval number
ATA Chapter 7
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • CF6-80C
      • CF6-80C2A1
      • CF6-80C2A2
      • CF6-80C2A3
      • CF6-80C2A5
      • CF6-80C2A5F
      • CF6-80C2A8
      • CF6-80C2B1
      • CF6-80C2B1F
      • CF6-80C2B1F1
      • CF6-80C2B1F2
      • CF6-80C2B2
      • CF6-80C2B2F
      • CF6-80C2B3F
      • CF6-80C2B4
      • CF6-80C2B4F
      • CF6-80C2B5F
      • CF6-80C2B6
      • CF6-80C2B6F
      • CF6-80C2B6FA
      • CF6-80C2B7F
      • CF6-80C2B8F
      • CF6-80C2D1F
      • CF6-80C2L1F
    • CF6-80E1
      • CF6-80E1A1
      • CF6-80E1A2
      • CF6-80E1A3
      • CF6-80E1A4
      • CF6-80E1A4/B
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information GE Service Bulletin/Repair Document No.: CF6-80C2 S/B 72-1171 Rev.1 CF6-80E1 S/B 72-0303 Rev. 1 Repair Document (RD) 935-314-S4 Rev.4
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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