Weight and
Balance Data
CSP–520N–1
MD 520N (500N) ROTORCRAFT FLIGHT MANUAL
TM
Original
6–3
REFERENCE
DATUM
STA
STA
15.0
+ 15.5
–13.0
STA
73.5
STA
100.0
STA
78.5
CG OF PILOT
CG OF COPILOT/
CARGO COMPARTMENT
STA
124.0
ROTOR CL
0.0
+ 12.2
–12.2
STA
105.0
+0.8
168..8
PASSENGER
STA
71.5
CG OF CENTER
PASSENGER
NOTE: REFERENCE COORDINATES VALID FOR TWO OR THREE PLACE COCKPIT/DUAL OR SINGLE CONTROLS
F05–028
Figure 6–2. Reference Coordinates (Sheet 1 of 2)
