Document ID: chunk:federal_register_of_legislation:F2006B06566:body:0
Version: federal_register_of_legislation:F2006B06566
Segment Type: other
Provision Reference: 
Character Range: 0–745

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Rolls Royce Turbine Engines - RB211 Series

 AD/RB211/6
 Amdt 4

 Low Pressure Compressor Rotor (Fan) Axial Retention

 9/87

            Applicability: RB211-524 series engines and modules as listed in Rolls Royce SB RB211-72-6576 R7.

 Requirement: Rolls Royce SB RB211-72-6576 Rev 7.

Note: FAA AD 82-12-05 Amdt 39-4398 refers.

Compliance: In accordance with the Requirement Document.

            Background: This Directive has been amended to reflect the manufacturers latest revision to the Requirement Document. This revision amends the engine models and modules effectivity listing.