CSP
−
E
−
1
Weight and Balance Data
ROTORCRAFT FLIGHT MANUAL
MD 500E
(Model 369E)
Revision 14
6
−
21
FWD C
RH
(+)
LH
(
−
)
STA
124.0
STA
109.2
STA
95.5
STA
78.5
CG OF PASSENGERS
L
+12.0 IN.
+5.2 IN.
−
12.0 IN.
FUEL FILLER
INLET LINE
F03
−
024
KIT WEIGHT = 17.9 LB
KIT CG = 101.4 IN. LONGITUDINAL
−
1.0 IN. LATERAL
Aft Compartment Passenger Weights and Longitudinal Moments
(High Density Seating)
Table 6
−
4. Weight and Loading for 369H90035
−
503 Seating and Belts
for Four Installation (High Density Seating)
Passenger (s)
(lb)
Moment (In. lb),
Fwd position
(Sta 95.5)
Moment (in.−lb),
Aft Position
(Sta 109.2)
150
14,300
16,400
175
16,700
19,100
200
19,100
21,800
225
21,500
24,600
250
23,900
27,300
275
26,300
30,000
300
28,700
32,800
325
31,000
35,500
350
33,400
38,200
375
35,800
41,000
400
38,200
43,700
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