208_load_sheet 208 Load Sheet

C208_Load_Sheet C208_Load_Sheet

User Manual: 208_load_sheet

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Copyright RSV Aviation March 2005
CESSNA 208B WEIGHT AND BALANCE SHEET FEMALE 1 CHILD FEMALE Certified correct
MALE 0 1 2 3 MALE 0 1 2 Signature
0 0 150 300 450 0 77 227 377 Name
DATE / / A/C REG 1 190 340 490 1 267 417 Notes
FLIGHT NO SECTOR TO 2 380 530 2 457
ACFT OEW ARM INDEX 3 570 2 CHILD FEMALE Formulas:
PAX WEIGHTS (lbs) MALE 0 1
MALE 190 0 154 304
WEIGHT ARM INDEX FEMALE 150 1 344
(lbs) (ins) lb.-in./1000 CHILD 77 3 CHILD 450
OPERATING EMPTY WEIGHT
lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs
USABLE FUEL (2224lbs) 204.8 77 150 154 190 227 231 267 300 304 340 344 377 380 417 450 457 490 530 570
ROW
1 (seats 1-3) 173.9 ⇒-3 -5 -6 -7 -8 -8 -10 -11 -11 -12 -12 -14 -14 -15 -16 -17 -18 -19 -21
2 (seats 4-6) 209.9 ⇒3 5 6 7 8 8 10 11 11 12 12 13 14 15 16 16 18 19 20
3 (seats 7-9) 245.9 ⇒8 16 17 20 24 25 29 32 33 37 37 41 41 45 49 49 53 57 61
4 (seats 10-12) 281.9 ⇒14 27 28 34 41 42 48 54 55 61 62 68 68 75 81 82 88 95 102
lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs lbs
CARGO (pod location) 15 30 45 60 75 90 105 120 135 150 165 180 195 210 230 250 270 280 310
ZONE
A (230lbs) 132.4 ⇒-2 -4 -5 -7 -9 -11 -13 -14 -16 -18 -20 -21 -23 -25 -27
B (310lbs) 182.1 ⇒0 -1 -1 -1 -1 -2 -2 -2 -3 -3 -3 -4 -4 -4 -5 -5 -5 -6 -6
C (270lbs) 233.4 ⇒1 2 4 5 6 7 9 10 11 12 14 15 16 17 19 21 22
D (280lbs) 287.6 ⇒3 6 9 11 14 17 20 23 26 29 32 34 37 40 44 48 52 54
RAMP WEIGHT (8785lbs)
FUEL ALLWANCE START/TAXI 35 206.1 -1
TAKE OFF WEIGHT (8750lbs)
FUEL BURN OFF 205.1
LANDING WEIGHT (8500lbs)
ADJUSTMENT
ADJUSTED TAKEOFF WEIGHT
ADJUSTED LANDING WEIGHT
FUEL INDICES
WT INDEX WT INDEX WT INDEX
50 1 800 21 1550 38
100 3 850 22 1600 39
150 4 900 23 1650 40
200 5 950 24 1700 41
250 7 1000 25 1750 42
300 8 1050 27 1800 44
350 9 1100 28 1850 45
400 10 1150 29 1900 46
450 12 1200 30 1950 47
500 13 1250 31 2000 48
550 14 1300 33 2050 49
600 16 1350 34 2100 50
650 17 1400 35 2150 51
700 18 1450 36 2200 52
750 19 1500 37 2224 53
Index = (arm-192)*wgt/500
Acft index = (arm – 192)*wgt/500 +500 (ie. Index +500)
% mac =( 500/wgt(index-500)+14.43 )/0.664
C of G = 500/wgt (index-500) +192

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