airworthiness · Rule · Final rule; request for comments. · Published 2003-10-30 · Effective 2003-11-14 · 68 FR 61737
Document
Document number
03-27152
Federal Register citation
68 FR 61737
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce plc Trent 556-61 Turbofan
Publication date
2003-10-30
Effective date
2003-11-14
FAA docket
Docket No. 2003-NE-42-AD
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Rolls-Royce (RR) plc RB211 Trent 556-61 turbofan engines. This AD requires a gauge inspection of the space between the high pressure (HP) fuel tubes adaptor face and seals, and a gauge inspection of the space between the fuel flow transmitter and seals, for evidence of permanent distortion of the face of the fuel tube connecting flanges, and replacement of parts if necessary. This AD is prompted by a report of fuel leaking from the engine fan cowl during an aircraft taxi. We are issuing this AD to prevent in-flight fuel leaks, which could result in an engine fire.