Weight and Balance
Pilot's Flight Manual
6-6.1
BA SIC WEIGHT
WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
WEIGHT (AS WEIGHED)
1123
100.9
113290
.4
429
T
H
G
I
E
W
S
U
L
P
R
U
S
MISSING EQUIP MENT WEIGHT
4.0
93.3
373
13
52
)
D
E
R
E
V
I
L
E
D
(
T
H
G
I
E
W
C
I
S
A
B
L
A
T
O
T
1127
100.9
113663
.4
481
LAT ERAL CENTER OF GRAV ITY
+ 0.4
G
N
I
D
A
O
L
D
R
A
W
R
O
F
T
S
O
M
WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
T
H
G
I
E
W
C
I
S
A
B
1127
100.9
113663
.4
481
T
O
L
I
P
170
83.2
14144 -13.8
-2346
L
E
U
F
E
L
B
A
E
S
U
0
108.5
0
R
E
T
N
E
C
,
R
E
G
N
E
S
S
A
P
170
80.0
13600
.75
128
H
R
,
R
E
G
N
E
S
S
A
P
170
83.2
14144 13.8
2346
TO TAL GROSS WEIGHT
1637
95.0
155551
.4
609
AP PROVED FOR WARD LIMIT 95 INCHES
MOST AFT LOADING
WEIGHT
(LB)
LONG.
ARM
(IN.)
LONG.
MO MENT
(IN.-LB)
LAT.
ARM
(IN.)
LAT.
MO MENT
(IN.-LB)
T
H
G
I
E
W
C
I
S
A
B
1127
100.9
113663
.4
481
T
O
L
I
P
170
83.2
14144 -13.8
-2346
).
L
A
G
E
L
B
A
E
S
U
5
.
2
3
(
L
L
U
F
,
L
E
U
F
195
108.5
21158 17.4
3393
TO TAL GROSS WEIGHT
1492
99.8
148965
1.0
1528
S
E
H
C
N
I
1
0
1
T
I
M
I
L
T
F
A
D
E
V
O
R
P
P
A
Sam ple based on sin gle 33 gal lon fuel tank
F
e
r
u
g
i
6-4. Sam e
l
p Weight and Bal ance Worksheet (Sheet 3 of 3)
Reissued:
CG OF FUEL AT STA 108.5 - S/N 1743, 1744, 1746 AND
T
N
E
U
Q
E
S
B
U
S
This Document contains technical data subject to EAR. See WARNING and classifications on first page.
SCHWEIZER
Model 269C Helicopter
CSP Book 1 CSP-C-1.indd 137
8/4/19 12:46 PM
Содержание S300C 269C
Страница 19: ...CSP Book 1 CSP C 1 indd 19 8 4 19 12 45 PM ...
