Piedmont Aviation NovfS - Page 2
Friday, Octobor 26, 1945»
Baggage 50 lbs, / 54 Am
Baggage 100 lbs. Arm / 85
Fuol capacity 76 gals Am / 34
Oil capacity 6 1/2 gals. Am *-34
Max. gross v/oight 4150 lbs.
C. G. Limits 16.3 and 26,7
Max, Except tako-off HP 275
Front wheels are locatod on an am of
/4
TfEIGHT AHD BALANCE REPORT
Not Wciight (lbs)
Left Front TOiool 1359
Right Front 'liVhoel 1359
Tail Vi/hoel 229
2947"
Distance botrraon front whool contor lino and tailwhocl axlo 207 3/4"
Empty C G Location from front VT-hool contor lino 16,14
Empty C G Location from datum 16,14 / 4,00 = 20,14
CG 20.14
'ront v'fliools
—207
CALCULATION OF C G FORWARD EXTREIffi
Aircraft EIT
Pilot and Passongor
Fuol (min) 22 11/12 gals
Oil 6,5 gals
C.G Forward Extromo 19,278 or 19,28
Vft, (lbs)
2947,00
340,00
137,50
48,75
3473.25
Arm (in,)
20,14
13,50
34,00
-34,00
Moment (in.lbt
59352.58
4590.00
4675.00
-1657,50
66960,08
CALCULATION OF C G AFT EKTREIIE
Aircraft El/T
Pilot
Passongors (3) roar
Fuol 54 gals.
Oil 6.5 gals
Baggage
Baggage
C G Aft Extromo 26,385 or 26,39
2947.00 20.14 59352,58
ITO.OO 13.50 2295,00
510.00 53,50 27285,00
324.25 34,00 11024.50
48,75 -34.00 - 1657.50
100.00 85,00 8500,00
50.00 54,00 2700,00
4150.00 109499.58
Both C G Extremes are v/ithin the limits. If you have trouble with this problem
do not hesitate to ask mo to clarify it for you.