Safety Publications Tool

F-1997-010R1 : Engine - Low Pressure Turbine Rotor Stub Shafts and Conical Supports - Life Limits

Number F-1997-010R1
Issued by France  France
Issue date 1997-02-26
Effective date 1997-03-08
EASA approval number
ATA Chapter 05, 72
Approval Holder
/ Type Designation
  • CFM INTERNATIONAL
    • CFM56-2
      • CFM56-2
      • CFM56-2A
      • CFM56-2B
    • CFM56-3
      • CFM56-3
      • CFM56-3B
      • CFM56-3C
    • CFM56-5
      • CFM56-5
      • CFM56-5-A1/F
Revision This Revision 1 replaces the original DGAC France AD 97-010(B) dated January 02, 1997.
Correction Not applicable
Supersedure None
Publication(s) and related information CFM International CFM 56-2 No.72-728 Revision 2, dated December 21, 1994, CFM 56-2A SB No.72-338 dated November 25, 1993, CFM 56-2B SB No.72-476 dated December 7, 1993, and CFM 56-3 /-3B /-3C SB No.72-695 dated November 25, 1993 (or later approved revisions); and Chapter 05 of the applicable engine shop manual (CFM 56-2 CFMI-TP.SM.4, CFM 56-2A /-2B CFMI-TP.SM.6, CFM 56-3 CFMITP.SM-5, and CFM 56-5 CFMI-TP.SM.7).
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu