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US-2002-15-04 : Engine - Centrifugal Compressor Impellers - Revised Cycle Count / Inspection / Marking

Number US-2002-15-04
Issued by United States of America  United States of America
Issue date 2002-08-06
Effective date 2002-09-10
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • HONEYWELL INTERNATIONAL INC.
    • T5313
      • T5313B
    • T5317
      • T5317A
      • T5317A-1
      • T5317B
      • T5317BCV
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Textron Lycoming SB T5313B/17-0052, Revision 2, dated December 16, 1993; AlliedSignal, Inc. SB T53-L-13B/D-0108, Revision 1, dated November 22, 1999; SB T53-L-13B-0108, Revision 1, dated November 22, 1999; SB T53-L-703-0108, Revision 1, dated November 22, 1999; SB T53-L-13B-0020, Revision 3, dated October 25, 2001; SB T53-L-13B/D-0020, Revision 1, dated April 25, 2001; SB T53-L-703-0020, Revision 1, dated April 25, 2001; or SB T531B/17-0020, Revision 6, dated May 2, 2001. For a copy of this service information, contact Honeywell International, Inc., Attn: Data Distribution, M/S 64-3/2101-201, P.O. Box 29003, Phoenix, AZ 85038-9003, telephone: (602) 365-2493; fax: (602) 365-5577.
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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