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US-2005-06-13 : [Correction] Wing Spar Centre Web Cutout - Inspection / Repair

Number US-2005-06-13
Issued by United States of America  United States of America
Issue date 2005-03-21
Effective date 2005-05-02
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • M7 AEROSPACE LLC
    • SA226
      • SA226-AT
      • SA226-T
      • SA226-T(B)
      • SA226-TC
    • SA227
      • SA227-AC
      • SA227-AT
      • SA227-BC
      • SA227-CC
      • SA227-DC
      • SA227-TT
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 99-06-02, dated March 10, 1999.
Publication(s) and related information Fairchild Airframe Airworthiness Limitations Manual ST-UN-M001, Rev. No. C-6, or ST-UN-M002, Rev. No. A-6, or ST-UN-M003, Rev. No. 5, as applicable; and Fairchild SA226/227 Series Structural Repair Manual, P/N 27-10054-079 (Rev.28), or P/N 27-10054-127 (Rev.7), as applicable. Copies can be obtained from Field Support Engineering, Fairchild Aircraft, Inc., P.O. Box 790490, San Antonio, Texas 78279-0490.
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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