AD/RRT-S/10 - HP2 Turbine Disc Locating Sleeve
1AD/RRT-S/10 - HP2 Turbine Disc Locating Sleeve
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/RRT-S/10 - HP2 Turbine Disc Locating Sleeve.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
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 - Spey Series
AD/RRT-S/10 HP2 Turbine Disc Locating Sleeve 13/87 DM
Applicability: Spey 506-14, 506-14A, 506-14D, 511-5W, 511-8, 511-14, 511-14W, 512-14DW, 512-14E, 555-15, 555-15H, 555-15N, 555-15P.
Requirement: Action in accordance with the Requirements of Rolls Royce SB Sp 72-932 Rev 1.
Note: Reference Documents:
- Fokker SB F28/72-6.
2. Netherlands AD Fokker F28 BLA nr. 87-62. Compliance: In accordance with the Requirement Document.
Background: This Directive has been issued to require HP turbine stage 2 disc retaining sleeves to be replaced at cycle lives listed in the Requirement document. This requirement follows advice of an uncontained turbine blade release event which resulted from failure of the subject sleeve.