Cessna 172 P - Maximum Rate of Climb; Time, Fuel, and Distance to Climb

WEIGHT
LBS
2400
PRESS
ALT
FT
S.L.
2000
4000
6000
8000
10000
12000
CLIMB
SPEED
KIAS
76
75
74
73
72
71
70
-20°
805
695
590
485
380
275
175
0°
745
640
535
430
330
225
125
20°
685
580
480
375
275
175
- - -
40°
625
525
420
320
220
- - -
- - -
RATE OF CLIMB - FPM
MAXIMUM RATE OF CLIMB
CONDITIONS:
Flaps Up
Full Throttle
NOTE:
Mixture leaned above 3000
feet for maximum RPM:
Figure 5-5. Maximum Rate of Climb
2400 S.L.
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
11000
12000
15
13
11
9
7
5
3
1
-1
-3
-5
-7
-9
76
76
75
75
74
74
73
72
72
71
71
70
70
700
655
610
560
515
470
425
375
330
285
240
190
145
0
1
3
5
7
9
11
14
17
20
24
29
35
0.0
0.3
0.6
1.0
1.4
1.7
2.2
2.6
3.1
3.6
4.2
4.9
5.8
0
2
4
6
9
11
14
18
22
26
32
38
47
WEIGHT
LBS
PRESSURE
ALTITUDE
FT
TEMP
°C
CLIMB
SPEED
KIAS
RATE OF
CLIMB
FPM
FROM SEA LEVEL
TIME
MIN
FUEL USED
GALLONS
DISTANCE
NM
Figure 5-6. Time, Fuel, and Distance to Climb
CONDITIONS:
Flaps Up
Full Throttle
Standard Temperature
NOTES:
1. Add 1.1 gallons of fuel
for engine start, taxi and
takeoff allowance.
2. Mixture leaned above
3000 feet for maximum RPM.
3. Increase time, fuel and
distance by 10% for each 10°C
above standard temp.
4. Distances shown are based
on zero wind.
TIME, FUEL AND DIATNCE TO CLIMB
MAXIMUM RATE OF CLIMB
FLIGHT SIMULATION USE ONLY
PERFORMANCE
PAGE 7
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