Document ID: chunk:federal_register_of_legislation:F2007L01560:body:0:p2
Version: federal_register_of_legislation:F2007L01560
Segment Type: other
Provision Reference: 
Character Range: 2900–3563

shock absorber for evidence of slippage at the intersection of the tube and fork assembly, and a dye check of the weld area on the fork assembly.

             Amendment 1 required the same inspection requirements by a different inspection method, but required incorporation of an improved nose landing gear fork kit anytime a crack is found; and added additional aircraft to applicability.

             Amendment 2 is issued to correct an error in Requirement 3, where Part III of the referenced Beech MSB should have been Part II.  This error flowed from related FAA AD 2004-23-02.

David Punshon
Delegate of the Civil Aviation Safety Authority

9 May 2007