← FAA Federal Register actions

Airworthiness Directives; Rolls-Royce, plc RB211 Trent 700 Series Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 1998-09-16 · Effective 1998-10-01 · 63 FR 49416

Document

Document number
98-24645
Federal Register citation
63 FR 49416
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1998-09-16
Effective date
1998-10-01
FAA docket
Docket No. 98-ANE-10-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Rolls-Royce, plc RB211 Trent 700 series turbofan engines. This action requires repositioning of the oil metering jet up into the oil distributor within the bevel gearshaft, followed by repetitive inspections of the Magnetic Chip Detector (MCD). Evidence of driving bevel gearshaft ball bearing failure requires replacement of the Step Aside Gearbox (SAGB). This amendment is prompted by reports of uncommanded engine rundowns caused by failure of the SAGB driving bevel gearshaft ball bearing due to oil starvation. This causes a loss of drive to the external gearbox and accessories, resulting in an inflight engine shutdown. The actions specified in this AD are intended to prevent inflight engine shutdowns caused by SAGB driving bevel gearshaft ball bearing failure.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown