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F-1996-237 : Fuselage inspection connecting angle between frame 56 and framesupport at stringer 38

Number F-1996-237
Issued by France  France
Issue date 1996-11-02
Effective date 1996-11-02
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A320
      • A320-211
      • A320-212
      • A320-214
      • A320-215
      • A320-216
      • A320-231
      • A320-232
      • A320-233
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information ISB A320-53-1084 R 01 OR MSB A320-53-1011 OR MOD 20941
Remarks ISB to be accomplished before accumulation of 20,000 and every 12,000 flights.