AD/RB211/5 Amdt 2 - Low Pressure Compressor Rotor (Fan) Axial Retention
1AD/RB211/5 Amdt 2 - Low Pressure Compressor Rotor (Fan) Axial Retention
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.