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US-2003-07-07 : Landing Gear - Main Landing Gear Wheel Tie-Bolt Nuts - Inspection / Replacement

Number US-2003-07-07
Issued by United States of America  United States of America
Issue date 2003-04-03
Effective date 2003-05-08
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • TEXTRON AVIATION INC.
    • BAe/BH/DH/HS.125
      • BAe.125 Series 800A
      • BAe.125 Series 800B
      • BH.125 Series 400A
      • DH.125 Series 1A
      • DH.125 Series 1A-522
      • DH.125 Series 1A/R-522
      • DH.125 Series 1A/S-522
      • DH.125 Series 3A
      • DH.125 Series 3A/R
      • DH.125 Series 3A/RA
      • DH.125 Series 400A
      • HS.125 Series 1B
      • HS.125 Series 1B-522
      • HS.125 Series 1B/R-522
      • HS.125 Series 1B/S-522
      • HS.125 Series 3B
      • HS.125 Series 3B/R
      • HS.125 Series 3B/RA
      • HS.125 Series 3B/RB
      • HS.125 Series 3B/RC
      • HS.125 Series 400B
      • HS.125 Series 400B/1
      • HS.125 Series 401B
      • HS.125 Series 403A(C)
      • HS.125 Series 403B
      • HS.125 Series F3B
      • HS.125 Series F3B/RA
      • HS.125 Series F400B
      • HS.125 Series F403B
    • Hawker
      • Hawker 800
      • Hawker 800XP
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Raytheon SB 32-3522, dated September 2002. Copies may be obtained from Raytheon Aircraft Company, Department 62, PO Box 85, Wichita, Kansas 67201-0085.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu

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