ON-wing AMM & SRM use
Hi,
Hopefully this is an easy question for someone to answer: -
An aircraft (my question is for the A319/320/321 with V2500 specifically) comes in for an A or C check with no scheduled engine removal planned. When inspecting the nacelle regions of the aircraft (AIC, FCDs, T/R, CNA etc) the main useable document is the AMM, containing all insp/chck tasks, off-wing repairs etc. My question is, what dictates when the vendor SRM (structural repair manual) is used? This also contains field repairs & allowable damage limits.
I’m completely confused on when & how the SRM is used so any input would be most appreciated.
Thanks.