Cessna 1973 172 - Take-Off Data; Maximum Rate-Of-Climb Data

TAK
TAKE-OFF DISTANCE FROM
E-OFF DA
HARD SURFACE Ri
TA
JNWAY WITH FLAP S UP
GROSS
WEIGHT
POUNDS
IAS
AT 50'
MPH
HEAD
WIND
KNOTS
AT SEA LEVEL & 59°
AT 2500 FT. & 50°F
AT 5000 FT. & 4rF AT 7500 FT. & 32°F
GROSS
WEIGHT
POUNDS
IAS
AT 50'
MPH
HEAD
WIND
KNOTS
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
1100
1255
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
NOTE 3: 1. In
2. F
5C
crease distance 10% for each 25^ above standard temperature for particular altitude.
Dr operation on a dry, grass runway, increase distances (both "ground run" and "total to clear . ,
ft. obstacle") by 1% of the "total to clear 50 ft. obstacle" figure.
MAXIMUM RATE-OF-CLIMB DATA
AT SEA LEVEL £ 59°F
AT 5000 FT. & 41 "F
AT 10,000 FT. &
23''F
AT 15.000 FT. & S-F
GROSS
WEIGHT
POUNDS
IAS
MPH
RATE OF
CLIMB
FT/MIN
GAL.
OF FUEL
USED
IAS
MPH
RATE OF
CLIMB
FT/MIN
FROM
S.L.
FUEL
USED
IAS
MPH
RATE OF
CLIMB
FT/MIN
FROM
S.L.
FUEL
USED
IAS
MPH
RATE OF
CLIMB
FT/MIN
FROM
S.L.
FUEL
USED
2300 90
645
1.0
85
435
2.6
79
230
4.8
73 20
11.5
2000
86
840
1.0
80 610
2,2
74 380 3.6
68
155
6.3
1700
82
1085
1.0 76
825
1.9 70
570
2.9
64
315
4.4
NOTES: 1.
2.
3.
Flaps up, full throttle, mixture leaned for smooth operation above 3000 ft.
Fuel used includes warm up and take-off allowance.
For hot weather, decrease rate of climb 20 ft. /min, for each lO'^F above standard day
temperature for particular altitude.
i> Figure 6-3.