CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Weight and
Balance Data
Original
6–13
Table 6–4. Internal Cargo Loading
TIE−DOWN LOCATION
RESTRAINT VALUE/POUNDS OF CARGO
TIE−DOWN FUSELAGE
LATERAL
MAIN CABIN
RESTRAINT DIRECTION
BAGGAGE COMPARTMENT
RESTRAINT DIRECTION
TIE DOWN
NUMBER
FUSELAGE
STATION
LATERAL
STATION
FORWARD
LATERAL
LEFT (−)
LATERAL
RIGHT (+)
FORWARD
LATERAL
LEFT (−)
LATERAL
RIGHT (+)
1
156.8
−27.0
220
2
174.9
−25.0
20
40
3
193.0
−25.0
130
20
4
211.1
−25.0
130
40
5
229.2
−27.0
120
220
6
229.2
−11.0
50
240
7
229.2
−8.0
50
240
8
229.2
8.0
50
240
9
229.2
11.0
50
240
10
229.2
27.0
120
220
11
211.1
25.0
130
40
12
193.0
25.0
130
20
13
174.9
25.0
20
40
14
156.8
27.0
220
15
156.8
11.0
240
16
156.8
8.0
240
17
156.8
−8.0
240
18
156.8
−11.0
240
19
232.9
−21.6
90
185
20
251.0
−24.8
120
135
110
21
233.3
0.0
85
85
22
257.9
0.0
20
120
120
23
232.9
21.6
90
185
24
251.0
24.8
120
135
110
25
230.5
−24.6
110
26
230.5
24.6
110
27
269.0
−17.5
105
28
269.0
17.5
105
Summary of Contents for MD900 with PW206E
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