Posts Tagged ‘Rolls-Royce’

FAA is superseding an AD on Thrust Reverser Units for Rolls Royce RB211 Engines

Saturday, February 23rd, 2013

The FAA is superseding an existing airworthiness directive (AD) 2013-04-01 for all Rolls-Royce plc (RR) RB211-524 series turbofan engines. That AD currently requires removal and repair of certain thrust reverser units (TRUs) prior to reinstallation. This AD requires the same actions for an expanded population of TRUs and extends the compliance time for repairing certain TRUs. This AD was prompted by additional engineering evaluation of TRUs, as a result of a translating cowl gearbox stubshaft failure and subsequent repair. We are issuing this AD to prevent failure of the attachment rivets, which may result in release of the TRU from the engine.

DATES: This AD is effective March 8, 2013.

default icon2013-04-01.pdf

AD on High pressure turbine for Rolls-Royce Corporation

Friday, September 24th, 2010

AD 2010-19-01 – High pressure turbine on Rolls-Royce Engine AE 3007A

pdf icon2010-19-01.pdf

AD Low- pressure turbine disks Rolls Royce

Monday, August 23rd, 2010

AD 2010-17-12 for Low pressure turbine disks Rolls Royce Deutschland Ltd &

Rolls-Royce TAY 650
Rolls-Royce TAY 651

pdf icon2010-17-12.pdf

AD for Rolls Royce Rear cooling air holes

Monday, August 23rd, 2010

AD 2010-17-10 applies to the following Rolls Royce models

Rolls Royce RB211-22B-02
Rolls Royce RB211-524B4-D-02
Rolls Royce RB211-524D4-19
Rolls Royce RB211-524D4-39
Rolls Royce RB211-524D4-B-19
Rolls Royce RB211-524D4-B-39
Rolls Royce RB211-524D4X-19
Rolls Royce RB211-524D4X-B-19

pdf icon2010-17-10.pdf

AD 2010-17-13 for Rolls Royce Engines

Friday, August 20th, 2010

LPT casings for Rolls-Royce Engines

AD 2010-17-13

Rolls-Royce RB211-524C2-19

Rolls-Royce RB211-524C2-B-19

pdf icon2010-17-13.pdf