![]() ![]() One might think that the F33A offers a greater range on the aft CG, but it is an illusion because the empty CG location starts out further aft (in my average data it is (81.96 - 79.43) 2.53 inches further aft to begin with whereas the initial aft CG at maximum GW is (86.7 - 84.4) 2.3 inches. ![]() ![]() The aft CG limit on the F33A is located at a fixed value of 86.7 inches whereas the V35B starts at 84.4 inches at max GW (3400) and moves aft to 85.7 inches at 3000 lbs where it remains fixed for weights below that value. The equivalent average numbers for the same year range V tails are: on 49 V35B's with the average CG location of 79.43 inches, empty weight of 2240 lbs, useful load of 1185 lbs. Some of the aircraft in the data have increased maximum GW (usually an IO550 upgrade). It has data on 40 F33A's with the average CG location of 81.96 inches, empty weight of 2329 lbs, useful load of 1113 lbs. I have a spreadsheet that has the W&B data for 234 Bonanza and Baron aircraft organized by model and year. If you require this type of loading, you should be looking at an A36 in the Bonanza line. They rarely run over the Max GW limit, but the aft CG is a challenge with four. It is best to consider them three person airplanes with baggage. Click to expand.The vast majority of V35B and F33A's would be very CG challenged with the cabin load you suggest.
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