Document ID: chunk:federal_register_of_legislation:F2006B02937:body:0
Version: federal_register_of_legislation:F2006B02937
Segment Type: other
Provision Reference: 
Character Range: 0–814

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Boeing 737 Series Aeroplanes

AD/B737/38 Fuselage Lap Joints BS259 to BS1016 5/90

 Applicability: Line number 001 to 291 inclusive.

            Requirement: Action in accordance with the technical requirements of FAA AD 89-09-03, paras A to D.

            Note: Incorporation of the repairs/modifications in this Directive partially terminate the requirements of AD/B373/37.

 Compliance: In accordance with the Requirement Document.

            Background: This Directive requires terminating action for parts of AD/B737/37. This is in recognition that inspection procedures alone may not ensure an adequate level of structural integrity at the skin splices.