Safety Publications Tool

US-91-12-10 : Wings - Spar Attachment - Modification

Number US-91-12-10
Issued by United States of America  United States of America
Issue date 1991-07-15
Effective date 1991-07-15
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • TEXTRON AVIATION INC.
    • 200 (Super King Air)
      • B200
      • B200C
      • B200T
    • 300 (Super King Air)
      • 300
      • 300LW
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Beech Kit No. 101-4050. For a copy of this service information, contact the Beech Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085. For aeroplanes making use of the AMOC (see attached and Remarks below), the following documents must be used: Beechcraft Super King Air 200 Series Maintenance Manual, P/N 101-590010-19 Revision A40, December 21, 1995, Section 4-00-00, Airworthiness Limitations (or later FAA approved revision); or Beech Super King Air 300 and 300LW Maintenance Manual P/N 101-590097-9 Revision A23 November 11 , 1995, Section 4-00-00, Airworthiness Limitations (or later FAA approved revision).
Remarks FAA recently [23 February 2018] approved the attached AMOC (Ref. 7K0-18-00734) that meets the criteria of ED Decision 2004/04/CF and the FAA/EASA Bilateral Agreement, which means this AMOC is considered 'approved by EASA' and can be used for affected aroplanes under EASA jurisdiction. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu