Cessna Hawk XP - Rate of Climb; Time, Fuel, and Distance to Climb

SECTION 5
PERFORMANCE
CONDITIONS:
Flaps Up
2600
RPM
Full Throttle
Mixture Set at Placard Fuel Flow
Cowl Flap
Open
RA TE OF CLIMB
[MAXIMUM
CESSNA
MODEL R172K
MIXTURE SETTING
PRESS ALT
GPH
S.L.
16
4000
14
8000
12
12,000
10
-
WEIGHT
PRESS
CLIMB
RATE
OF CLIMB - FPM
LBS
2550
I
,,,
- 14
ALT
FT
S.L.
2000
4000
6000
8000
10,000
12,000
SPEED
KIAS
-20°c
o
0
c
81 . 1040
945
80
925
830
79
810
720
78
695
615
77
585
505
76
480
400
75
370
295
Figure 5-5. Rate of Climb
20°c
40°c
845
750
740
650
635
545
530
445
425
345
320
- - -
220
- - -
CESSNA
MODEL R172K
7
SEC T ION 5
PERFORMANCE
TIME, FUEL, ~ND DISTANCE TO CLIMB
I MAXIMUM RATE OF CLIMB I
CONDITIONS:
flaps Up
2600 RPM
Full Throttle
Mixture
Set at Placard Fuel Flow
Cowl Flap
Open
Standa rd Temperature
NOTES :
MIXTURE SETTING
PRESS ALT
GPH
S.L. 16
4000 14
8000
12
12,000
10
1. Add 1.4 gallons of fuel for engine st.art, taxi and takeoff allowance.
2.
Increase time, fuel and distance by 10% for each 10°c above standard temperature.
3. Distances shown are based on zero wind.
PRESSURE
CLIMB
RATE
OF
FROM SEA LEVEL
WEIGHT
ALTITUDE
TEMP
SPEED CLIMB
LBS
FT
oc
KIAS FPM
TIME FUEL USED
DISTANCE
MIN
GALLONS
NM
2550
S.
L. 15
81
870 0
0
0
1000
13
80 825 1
0.3
2
2000
11
80 780
2
0.6
3
3000 9
79
735
4
1.0
5
4000 7
79
690
5
1.3
7
5000 5
79
645 7
1.6
9
6000 3
78
600 8
2.0
11
7000 1
78
555
10
2.4 14
8000
- 1
77
510 12
2.7
16
9000
-3
77 465 14
3.2
19
10,000
- 5
76 420
16
3.6
23
11,000
-7
76
375 19
4.0
26
12 ,000
-9
75
330 22 4.5
31
Figure 5-6. Time, Fuel, and Distance to Climb ( Sheet 1 of 2)
5-15
r \