Safety Publications Tool

US-2004-03-08 : Fuselage and Engine Pylons Drag Angles - Modification / Forward Engine Beam Shear Web - Inspection / Modification / Repair

Number US-2004-03-08
Issued by United States of America  United States of America
Issue date 2004-02-09
Effective date 2004-03-15
EASA approval number
ATA Chapter 51
Approval Holder
/ Type Designation
  • LEARJET, INC.
    • 31/35/36
      • 31
      • 31A
      • 35
      • 35A
      • 36
      • 36A
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Bombardier SB 31-51-2, dated February 1, 2001; and SB 31-51-3, Revision 1, dated August 2, 2001; or SB 35/36-51-3, dated February 1, 2001; and SB 35/36-51-4, Revision 1, dated August 2, 2001. Copies may be obtained from Learjet, Inc., One Learjet Way, Wichita, Kansas 67209-2942.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

Download attachments: