Safety Publications Tool

US-2006-01-05 : Engine - Reduced Life Limits for Parts

Number US-2006-01-05
Issued by United States of America  United States of America
Issue date 2006-01-12
Effective date 2006-02-16
EASA approval number
ATA Chapter 05, 72
Approval Holder
/ Type Designation
  • HONEYWELL INTERNATIONAL INC.
    • T5309
      • T5309A
      • T5309B
      • T5309C
    • T5311
      • T5311A
      • T5311B
    • T5313
      • T5313B
    • T5317
      • T5317A
      • T5317A-1
      • T5317B
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes FAA AD 87-12-05 dated 8 June 1987.
Publication(s) and related information Lycoming SB No. 0002, Revision 2, dated March 6, 1989; Honeywell International Inc. SB No. T5313B/17-0020, Revision 7, dated November 21, 2002; SB No. T5313B-0125, dated March 15, 2001, or SB No. T5317-0125, dated March 15, 2001. 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 for a copy of this service information.
Remarks The military variants of the T53 engines are not eligible for installation on civil helicopters in Europe. Enquiries 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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