DCA/ R22/41 Main Rotor Blades – Reduced Retirement Life
Applicability:
All R22 series
Requirement:
To prevent in-flight failure of a main rotor blade caused by fatigue cracking in the
inboard end of the main rotor blades and subsequent loss of the helicopter,
accomplish the following:-
1. For main rotor blades which have been fitted to helicopters performing aerial
mustering operations in Australia for more than 50 hours TIS, the blade retirement life
is reduced to 1500 hours TTIS.
Where used blades have been imported from Australia and it can not be determined
whether or not the blades have been fitted to helicopters performing aerial mustering
operations, the blade retirement life is reduced to 1500 hours TTIS.
2. Main rotor blades retired from service per Australian AD/R22/31 Amdt 7 are not to
be fitted to any helicopter.
Note: MRBs that are removed at less than the time specified in the Airworthiness
Limitations Section of the R22 Maintenance Manual should be retained as future
developments may enable them to be placed back into service.
1. Retire blades at 1500 hours TTIS or within the next 25 hours TIS, whichever is the
later.
2. From 13 August 2003.