Rolls-Royce 1004227 Automobile User Manual


 
EPRI Proprietary Licensed Material
RB 211 Maintenance Scope
B-11
RN 5017 – Log Book Cyclic Life Information
RN 5024 – HP Turbine Blade Check Procedure
RN 5033 – Fatigue failures of Compressor, turbine rotor blades and stator vanes
RN 5039 – Inspection standard for HP turbine blades
OIA 005 – HPT blades for thermal cracking
MOD 1167 – Single life bolts
Dimensionally inspect the Panel Support and Rotor Disc Location.
In conjunction with the OEM and Customer, review the HP turbine creep life.
Consign HP turbine blades for weld repair of the outer shroud abutment and non-abutment
faces to MOD 1130 & 1131 Sermaloy ‘J’ Coating.
Overhaul process HP Turbine Disc and front rear cones.
Inspect rear bearing track and seals.
Inspect all rotating seals.
Visually inspect all Remaining Components.
Rebuild and rebalance the HP Turbine Rotor as per standard procedures.
Nozzle Case and Nozzle Vanes HP (Section 1081)
Detail Strip, Clean and Inspect.
Embody the following:
RN 5012 – Acceptance standard of the cooling tube in HP NGV’s.
RN 5022 – Restricted usage of Nimonic 80A fasteners.
RN 5033 – Fatigue failures of compressor, turbine rotor blades and stator vanes.
OIA 043 – Revised HP Turbine honeycomb seal clearances.
Inspect the HP Seal Segments, repair and renew the Honeycomb seals as necessary.
Consign the HP NGV’s for repair, as required, and re-protection with Sermaloy ‘J’ coating in
accordance with MOD 1110.
Rebuild the HP Nozzle cases as per standard procedures.
Attachment Parts and Fittings Combustion Liners (Section 1088)
Detail Strip, Clean and Inspect.
Attachment Fittings Combustion Outer Case (Section 1089)
Detail Strip, Clean and Inspect.