ORLI
Č
AN M-8 EAGLE
PILOT'S OPERATING
REVISION NO. 05
DATE OF ISSUE: MAY 02,
WEIGHT AND BALANCE
PAGE
OF
63
67
3.
WEIGHT AND BALANCE RECORD OF THE AIRCRAFT
AIRCRAFT
ENGINE
PROPELLER
TYPE
M8-EAGLE
ROTAX 912 ULS 2
SR 200
SERIAL NUMBER
2022001
9 573 673
1900921
𝐿
𝐴
[
𝑖𝑛
]
= 28,82
𝐿
𝐴𝑅
[
𝑖𝑛
]
=
𝐿
𝐴
−
𝐶
𝐶
[
𝑖𝑛
]
= 1,46
𝐵
𝑆𝐴𝑇
[
𝑖𝑛
]
=
47,36
𝐿
𝑃
[
𝑖𝑛
]
= 66,73
C.G. POSITION CALCULATION
C.G. CALCULATION
WEIGHT CALCULATION
𝐺
𝑃
×
𝐿
𝑃
𝑋
𝑇
[
𝑖𝑛
]
𝑋
𝑇
[
𝑖𝑛
] =
𝐿
𝐴𝑅
−
𝐺
𝑋
𝑇
[%] =
𝑏
×
100
𝐺
𝐶𝐸𝐿𝐾
=
𝐺
𝑃
+
𝐺
𝐻𝐿
𝐶𝐸𝐿𝐾
𝑆𝐴𝑇
CRE
W
[LB]
FUEL
[GAL]
BAG.
[LB]
NOSE
WHEE
L
𝑮
𝑷
[
𝒍𝒃
]
MAIN
GEAR
𝑮
𝑯𝑳
[
𝒍𝒃
]
TOTA
L
WEIG
HT
𝑮
𝑪𝑬𝑳𝑲
[
𝒍
𝒃
]
C.G. FROM REFERENCE
PLANE
𝑿
𝑻
+
𝑪
[
𝒊𝒏
]
𝑿
𝑻
[%]
0
0
0
158,3
643,9
802,2
15,65
29,96
0
0
33
149,5
685,7
835,3
16,87
32,55
132
0
0
177,7
756,8
934,5
16,13
30,98
132
3
0
180,6
772,4
953
16,17
31,07
220
0
0
187,2
835
1022,2
16,
6
32
396
0
0
210,4
989,6
1200
17,12
33,07
396
13,
2
0
226,4
1052,9
1279,3
17,
0
32,8
Summary of Contents for M-8 EAGLE 2022
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