Cessna 172 Skyhawk - Take-off and Climb Performance

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TAKE-OFF DATA
TAKE-OFF DISTANCE FR O M H A R D SU R FA C E RUNWAY WITH FLAPS UP
GROSS
WEIGHT
POUNDS
IAS AT 50'
MPH
HEAD
WIND
KNOTS
AT SEA LEVEL & 59°
AT 2500 FT. & 50°F
AT 5000 FT. & 41"F
AT 7500 FT. & 32°F
GROUND
RUN
TOTAL TO
CLEAR 50 FT
OBS
GROUND
RUN
TOTAL TO
CLEAR 50 FT
OBS
GROUND
RUN
TOTAL TO
CLEAR 50 FT
OBS
GROUND
RUN
TOTAL TO
CLEAR 50 FT
OBS
2300
68
0 10 20
865 615 405
1525 1170 850
1040 750
505
1910 1485 4100
1295 920
630
2480 1955 1480
1565 1160
810
3855 3110 2425
2000
63
0 10 20
630 435 275
1095 820 580
755 530 340
1325 1005 720
905 645 425
1625 1250 910
1120 810
595
2155 1685 1255
1700
58
0 10 20
435 290 175
780 570 385
520 355 215
920 680 470
625 430 270
1095 820
575
765 535 345
1370 1040 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 50 ft. obstacle") by 7% of the "total to clear 50 ft. obstacle" figure.
MAXIMUM RATE-OF-CLIMB DATA
GROSS
WEIGHT
POUNDS
AT SEA LEVEL & 59°F
AT 5000 FT. Si 41°F
AT 10,000 FT. & 23°F
AT 15.000 FT. & 5"F
LAS MPH
RATE OF
CLIMB
FT/MIN
GAL. OF
FUEL
USED
LAS MPH
RATE OF
CLIMB
FT/MLN
FROM
S.L. FUEL
USED
LAS MPH
RATE OF
CLIMB
FT/MIN
FROM
S.L.
FUEL
USED
IAS MPH
RATE OF
CLIMB
FT/MIN
FROM S.L.
FUEL
USED
2300
82
645
1.0
81
435
2.6
79
230
4.8
78
22
11.5
2000
79
840
1.0
78
610
2.2
76
380
3.6
75
155
6.3
1700
77
1085
1.0
76
825
1.9
73
570
2.9
72
315
4.4
NOTES: 1. Flaps up, full throttle, mixture leaned for smooth operation above 3000 ft. 2. Fuel used includes warm up and take-off
allowance. 3. For hot weather, decrease rate of climb 20 ft./min. for each IO°F above standard day temperature for particular altitude.
Figure 6-3.
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