mtv wrote:Gross weight limitations are predicated on a number of parameters, and often have nothing to do with the structural robustness of the airframe. Probably the most common parameters have to do with performance, rather than concern over something breaking.
As to similarities between the 172 and the 172 RG, note that the 172 RG was certified under the Cessna 175/Hawk XP/T-41 Type Certificate, NOT under the Cessna 172 TC.
MTV
Thanx MTV. Performance may be the key factor? But, some types of performance enhancements seems to get better treatment from the FAA than others?
Perhaps RG's were able to demonstrate significantly better climb rates over obstacles on take-off (I'm skeptical about that**), or maybe somewhere else in the flight envelope?
Surprisingly, increased engine power doesn't get similar increases in MGW, since the XP @ 195hp and T-41 @ 210hp got
nothing for their better performance. And I don't believe Stoots Aviation received any MGW increase from the FAA for their recent 210hp IO-390 STC? Wonder why?
Interestingly, in the C177 Cardinal series, when the Cardinal RG came along, it got a whopping 300# increase in MGW to 2800#! Was that because of it's (notoriously slow) retractable gear, or it's increase in horsepower from 180-to-200, or both?
** I find it hard to believe that more horse-power applied throughout the entire take-off roll & climbout, counts for less than a heavier & slowly retracting gear system that only helps after lift-off. And I always seem to be much-much higher than any obstacles, by the time that the gear is eventually "up and locked" in an RG.
Since better or bigger airfoils also increase performance, it would seem logical that Wing-X could demonstrate that in all models of Cessna? But, for some strange reason: there are models that get MGW increases, while others don't, yet, can be imported without a weight increase, and the poor C172 can't even get brought into the country! Weird?
It almost seems to come down to marketing? Cessna just gives away added MGW on their heavier RG's, in order to provide customers with the same useful load, and they have enough "influence" to push it through the FAA?