Manufacturer
Rolls-Royce Deutschland
Number
EASA 2022-0252R1
Model(s)
BR700-71715A1-30 and BR700-715B1-30/C1-30
Published Date
Effective Date
Summary
Supersedes but retains requirements of AD 2022-0252, which mandated repetitive fluorescent-penetrant inspections of the front flange scallops of certain LP compressor booster rotors. After a new risk assessment, the updated AD extends the inspection interval to 5,000 engine flight cycles if all parts pass the FPI.
UUID
508