Newbie W&B questions
Posted: Sun Jul 23, 2017 6:57 am
Proud new owner of a '48 170. I was working up W&B scenarios, and it appears this plane has a very far forward CG.
Current documentation shows Empty Weight is 1379.86 with CG at 37.96.
The last time it was weighed (before P. Ponk gear and some avionics changes) it was left main 645, right main 645, tail 100, for an empty weight of 1383 and CG 37.91.
Using Bruce's spreadsheet, I put in myself (186) and my instructor (170), and with 33.5 gallons of fuel, we are out of forward CG limit (especially when accounting for my short legs). We put a case of oil in the baggage compartment, and with half fuel, we were just inside the CG envelope. The airplane felt very nose heavy. Indeed, when my instructor flew it solo, he had trouble getting the tailwheel to stick down on pavement, said it felt bouncy.
I've read quite a few threads here, and it seems like on the last weighing, the tail was actually a bit lighter than most.
First question is it common to need ballast to correct forward CG? I would need 100lbs in the baggae compartment to get the CG towards the middle of the envelope where I'd like it. We plan to reweigh the plane, to make sure the numbers are all correct, but the way it handles seems to be consistent with far forward CG. So I am wondering if there's an actual issue that needs to be corrected.
Second, related question. The plane has a 12.5 gallon aux tank installed in the left wing. I think I have all the records, and the 337 and log book state that a flight test would be performed to determine unusable fuel, but I can't find a record of that. I assume the arm for this is +45, but how can I figure out the additional unusable fuel?
TIA.
Current documentation shows Empty Weight is 1379.86 with CG at 37.96.
The last time it was weighed (before P. Ponk gear and some avionics changes) it was left main 645, right main 645, tail 100, for an empty weight of 1383 and CG 37.91.
Using Bruce's spreadsheet, I put in myself (186) and my instructor (170), and with 33.5 gallons of fuel, we are out of forward CG limit (especially when accounting for my short legs). We put a case of oil in the baggage compartment, and with half fuel, we were just inside the CG envelope. The airplane felt very nose heavy. Indeed, when my instructor flew it solo, he had trouble getting the tailwheel to stick down on pavement, said it felt bouncy.
I've read quite a few threads here, and it seems like on the last weighing, the tail was actually a bit lighter than most.
First question is it common to need ballast to correct forward CG? I would need 100lbs in the baggae compartment to get the CG towards the middle of the envelope where I'd like it. We plan to reweigh the plane, to make sure the numbers are all correct, but the way it handles seems to be consistent with far forward CG. So I am wondering if there's an actual issue that needs to be corrected.
Second, related question. The plane has a 12.5 gallon aux tank installed in the left wing. I think I have all the records, and the 337 and log book state that a flight test would be performed to determine unusable fuel, but I can't find a record of that. I assume the arm for this is +45, but how can I figure out the additional unusable fuel?
TIA.