Cessna 402C - Page 139

SECTION 5
PERFORMANCE
RANGE PROFILE
CONDITIONS:
1. Takeoff Weight - 6850 Pounds.
2. Cruise Clumb to Deisred Altitude.
3.
Recommended Lean Fuel Flow.
4. Zero Wind.
5. Standard Day.
NOTE:
1. Range computations include fuel
required for
start, taxi, takeoff,
cruise climb to
altitude, cruise,
descent, and 45 minutes reserve
fuel at the particular
cruise ,power.
2. The distances shown are the sum of
the distances to climb, cruise and
descend.
'.oi,402C
185 KTAS
159
210
KTAS
KTAS
20
KTAS
200
191
158
KTAS
KTAS
177 KTAS
KTAS
/Coo,""
r-
15
w
w
,%
,%
,%
0-
~
'"
191
'"
'"
3
'"
'"
0
0
KTAS
.,
~
KTAS ~
170
'"
153
0
r::
V>
~
<0 -V>
KTAS
..-
KTAS
w
10
'"
=>
r-
;C
183
175
~
KTAS
148 KTAS
""
KTAS
163
w
KTAS
'"
=>
V>
5
V>
w
175
'"
0-
KTAS 168
156
KTAS
KTAS
143 KTAS
I I I
300 350 400 450 500
APPROXIMATE RANGE - NAUTICAL MILES (600 POUNDS USABLE FUEL)
Fi9ure 5-21
52847045