Document ID: chunk:federal_register_of_legislation:F2006B06565:body:0
Version: federal_register_of_legislation:F2006B06565
Segment Type: other
Provision Reference: 
Character Range: 0–755

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/RB211/5
 Amdt 2

      Low Pressure Compressor Rotor (Fan) Axial Retention

 1/83

Applicability: RB211-22B-02, RB211-524B-02, RB211-524B2-19, RB211-524B2-39, RB211-
524C2-19 engines and modules as specified in SB No. RB211-72-6574, Rev. 6.

 Document: Rolls Royce SB No. RB211-72-6574, Rev. 6.

            Note: FAA AD No. 82-12-05, Amdt. 39-4398 refers.

 Compliance: In accordance with the requirement document.

            Background:  This Directive is amended in order to reference the latest revision to the manufacturer's requirement document.