Weight and
Balance Data
CSP–520N–1
MD 520N (500N) ROTORCRAFT FLIGHT MANUAL
TM
Original
6–4
WL
66.0
ST
A
15.00
WL
22.75
CORNER
PILOT
’S
SEA
T
WL
21.50
ST
A
268.5
JACKING
POINT
ST
A
275.4
BL
0
WL
41.0
ST
A
315
F05–029
ST
A
159.97
ST
A
168.20
ST
A
124.75
CANT
ST
A
129.0
ST
A
132.9
ST
A
137.50
ST
A
146.62
ST
A
155.75
ST
A
174.00
WL
34.50
WL
13.10
JACKING POINT
ST
A
96.89
BL+25.6
WL
0.00
C BEAM L
WL
32.00
WL
1
1.98
WL
38.36
WL
14.19
WL
0.00
ST
A
0.00
ST
A
44.65
ST
A
50.50
ST
A
56.85
ST
A
64.37
ST
A
100.0
1
19.67
ST
A
84.79
CANT
ST
A
78.50
ST
A
90.61
ST
A
96.42
ST
A
102.23
ST
A
108.04
ST
A
1
13.85
ST
A
ST
A
124.00
ST
A
137.50
C L
Figure 6–2. Reference Coordinates (Sheet 2 of 2)
