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US-2002-08-06 : [Correction] Horizontal Stabilizer Pivot Fitting Attachment bolts - Inspection

Number US-2002-08-06
Issued by United States of America  United States of America
Issue date 2002-05-31
Effective date 2002-05-03
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • BOEING
    • 777
      • 777-200
      • 777-300
Revision Not applicable
Correction This AD was re-published to correct the requirements by adding an option to allow operators a 30-day grace period for submission of the report required by paragraph (d) of the AD. This correction is prompted by communication received from the manufacturer that the current requirements of the AD could put operators out of compliance.
Supersedure None
Publication(s) and related information Boeing Alert SB 777-55A0013, dated December 19, 2001, or Revision 1, dated January 31, 2002. For a copy of this service information, contact Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-2207.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu