Hi Again All
I have a good friend who has a CAP 232 and was alarmed to hear that he is stuffing it full of weight to bring the CG forward. I feel that this could induce early stalling, to which the CAP is susceptible at the best of times
Please could anyone out there tell me where the CG is on a 232 - in terms of say, Percentage chord at wing root.
The chap bought this superb model (65 inch span, maybe a Flair) from a swapmeet in England.
Thanks and Best Regards
David Evans