Cessna 1971 Super Skymaster - Page 44

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TWIN-ENGINE
MAXIMUM RATE-Of-CLIMB DATA
GROSS
WEIGHT
POUNDS
@S. L. &. 59°F
@5000 FT. &. 41° F
@ 10,000 FT. &. 23°F
@ 15, 000 FT. &. 5°F
@20,000 FT.
&. -12°F
lAS
MPH
RATE
ILBS.
OF OF
CUMB . FUEL
FT./MIN.
1
USED
IAS
MPH
RATE
OF
CUMB
FT./MIN.
FROM
jl,.b,..
FUEL
USED
RATE
lAS OF
MPH CUMB
FT./MIN.
FROM
S.L.
FUEL
USED
IAS
MPH
RATE
OF
CUMB
FT./MIN.
FROM
SoL.
FUEL
USED
IAS
MPH
RATE
OF
CUMB
FT./MI
FROM
~
FUEL
N. USED
4630
4200
3800
114
111
108
HOO
1300
1520
18
18
18
111
108
105
820
1005
1200
35
32
30
108
105
102
545
710
885
55
48
43
105
102
99
26S
4lS
570
83
67
58
--
99
96
---
125
265
-- ... -
101
79
NOTES:
1.
Full throttle, 2800 RPM, flaps and gear uP. mixture at recommended leaning schedule.
2.
Fuel used includes warm-up and take-off allowance.
3.
For hot weather, decrease rate of Climb 30 ft./mi.n~ for each 10°F above standard day temperature for particular altitude.
•
GROSS
WEIGHT
POUNDS
4630
4200
3800
4630
4200
3800
NOTES:
SINGLE-ENGINE
MAXIMUM RATE-Of-CLIMB
DATA
@S. L.
&. 59°F
@2500 FT. &. 50°F @ 5000 FT. &. 41°F @75oo FT. &. 32°F
@ 10, 000 FT. &. 23 OF
RATE
RATE RATE
RATE
RATE
lAS OF IAS OF
lAS OF
IAS OF
lAS
OF
MPH
CUMB MPH CUMB MPH
CUMB
MPH CLIMB
MPH
CUMB
FT./MIN. FT./MIN.
FT./MIN.
FT./MIN.
FT./MlN.
FRONT ENGINE OPERATING - REAR PROPELLER FEATHERED
101 235 100
145 99 55
99
-35
98
-125
99 360 98 265
97 170
97 75 96 -20
98
490
97
390 96
290
96
190
95 90
REAR ENGINE OPERATING
- FRONT PROPELLER FEATHERED
101
!
320
100
225
99 130
99 35
98 -60
99
I
450
98 350
97
25S
97
155
96 55
98
I
590
97 48S
96 385
96 275 95 170
1.
Full.throttle, 2800 RPM, flaps and gear up, mixt)1re at recommended leaning schedule.
2.
For hot weather, deere .... rate of cUmb 15 fl./mIn. for each 10'F above standard day temperature for particular altitude.
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