I am a candidate for a CPL using a Cessna Cutlass 172RG. The requirement is for the applicant to demonstrate that the weight and CG will be within operating limits for all phases of flight. This is where things get tricky as the POH has no mention of the CG shift when the gear is retracted back behind the aft baggage compartment.
Clearly their is a shift, but how much is unknown (at least to me, my instructor and the maintenance technician). I spoke with a DPE, and we are guessing that the CG cart is altered to show the aft most CG with gear down, but the actual performance limitations of the aircraft allow for the CG to be aft of the charts limits of 46.5" - but this is our best guess and assumption not something we have been able to confirm in any documentation.
So - any thoughts?
Edit/Post thought - now that I've been (over) thinking this for a day, it dawned on me that the 172RG's nose wheel retractes forward of the aircrafts center of gravity and is farther forward relative to the aft of CG of the main gear. Is it possible that the forward movement of e nose gear moment is equal to the moment of the aft main gear moment?
Either way, I would love to see something in writing if it exists.
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