Safety Publications Tool

US-2003-08-52 : Engine - Compressor Variable Geometry - Rigging

Number US-2003-08-52
Issued by United States of America  United States of America
Issue date 2004-05-16
Effective date 2003-06-02
EASA approval number
ATA Chapter 72
Approval Holder
/ Type Designation
  • GENERAL ELECTRIC
    • CT7-9
      • CT7-9B
Revision Not applicable
Correction This Final Rule AD replaces FAA Emergency AD 2003-08-52, issued on April 15, 2003, which contained the requirements of this AD.
Supersedure None
Publication(s) and related information GE Aircraft Engines CT7-TP Alert SB 72-A0328, Revision 1, dated April 8, 2003. For a copy of this service information, contact GE Aircraft Engines Customer Support Center, M/D 285, 1 Neumann Way, Evendale, OH 45215, telephone (513) 552-3272, fax (513) 552-3329, email GEAE.csc[at]ae.ge.com.
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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