CTHIn ForceLegislation
AD/RB211/6 Amdt 4 - Low Pressure Compressor Rotor (Fan) Axial Retention
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AD/RB211/6 Amdt 4 - 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/RB211/6
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.