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US-2004-26-04 : [Correction] Low Pressure Turbine-to-Exhaust Case Bolts and Nuts - Replacement / High Pressure Turbine Containment Hardware - Installation

Number US-2004-26-04
Issued by United States of America  United States of America
Issue date 2005-01-24
Effective date 2005-02-09
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • PRATT & WHITNEY
    • JT8D Series 200
      • JT8D-209
      • JT8D-217
      • JT8D-217A
      • JT8D-217C
      • JT8D-219
Revision Not applicable
Correction This AD was republished to correct a compliance time in Table 1 of the AD. In all other respects, the original document remains the same.
Supersedure This AD supersedes FAA AD 99-22-14, dated October 29, 1999.
Publication(s) and related information PW ASB No. JT8D A6346, dated September 10, 1998, or Revision 1, dated April 23, 1999, or Revision 2, dated December 1, 1999, or Revision 3, dated May 21, 2004. For a copy of this service information, contact Pratt & Whitney, 400 Main St., East Hartford, CT 06108; telephone (860) 565-7700; fax (860) 565-1605.
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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