Cessna 172 - Take-Off Data; Maximum Rate-of-Climb Data

.
TAKE-OFF
DATA
TA~E-OFF DISTANCE FROM HARD SURFACE RUNWAY WITH FLAPS UP
AT SEA LEVEL & 59°F
AT 2500 FT. & 50°F
AT 5000 FT. & 41 .. F
AT 7500 FT. & 32•F
GROSS IAS
HEAD
TOTAL
TOTAL
TOTAL
TOTAL
WEIGHT
AT so• WIND GROUND
TO . CLEAR
GROUND
TO
CLEAR
GROUND
TO CLEAR GROUND
TO CLEAR
POUNDS
MPH
KNOTS
RUN
SO FT OBS
RUN
SO FT OBS RUN 50 FT OBS
RUN
50 FT OBS
.
0
86S 1S2S
1040
1910
12S5
2480
156S
385S
2300
68
10
615
1170
750 148S
920
19SS
1160
3110
20 40S
8SO
50S 1100
630
I
1480
810 2425
'
0
630 1095 75S
1325 905
1625
1120 21SS
2000
63
10
43S
820 S30
lOOS 64S
12SO
810
168S
20
27S 580
340
720 42S
910
59S 12SS
0
43S 780
S20
920
62S 1095
76S
1370
1700
58
10
290
S70
3SS
680
430 820
53S
1040
20
17S
38S 21S
470
270
S7S
34S
. 745
NOTES: 1.
Increase distance 10% for each 25°F above standard temperature for particular altitude.
2.
For operation on a dry, grass runway, increase distances (both "ground run" and "total to clear
1
SO Ct. obstacle") by 7% of the "total to clear SO Ct: obstacle" figure.
~
MAXIMUM . RATE-OF-CLIMB
DATA
AT SEA LEVEL & S9°F
AT 5000 FT. & 41°F
AT 10,000 FT.&: 23•F
AT 15, 000 FT. & s•F
GROSS
RATE OF
GAL.
RATE OF
FROM
RATE OF
FROM
RATE OF
FROM
S.
L.
'
S.L. S.L.
WEIGHT IAS
CLIMB OF FUEL
lAS
CLIMB
FUEL
lAS
CLIMB
FUEL
IAS
CLIMB
FUEL
POUNDS
MPH
FT/MIN USED MPH
FT/MIN
USED
MPH
FT/MIN
USED
MPH FT/MIN
USED
'
2300
91
64S 1. 0
8S
435
2.6
80 ~
230
4.8 73
20
11. s
2000 88
840 1. 0 81
610
2.2
75
380
3.6 68
lSS
6.3
1700
83
108S
1. 0 77 82S 1. 9 70
S70
2. 9
64
31S
4.4
\
NOTES:
1. Flaps up, Cull throttle, mixture leaned for smooth operation above 3000 rt.
2.
Fuel used Includes warm up and take-of! allowance.
3. For hot weather , decreas ·e rate of climb 20 ft. /min. for each 10°F above standard day
.
' temperature !or particular altitude .
Figure 6-3.