c.n
I
t,.)
-TAKE -OFF
DISTAN C E
FLAPS RETRACTED
HARD SURFACE RUNWAY
GROSS
IAS
HEAD
WT.
50 FT.
WIND
LBS.
MPH
KNOTS
0
1600
64
10
20
AT SEA LEVEL
&
59° F.
GROUND
TO CLEAR
TOTAL
RUN
50 FT. OBS
735
1385
500
1035
305
730
AT 2500 FT.
&
50° F.
GROUND
TO CLEAR
TOTAL
RUN
50 FT. OBS
910
1660
630
1250
395
890
AT 5000 FT.
&
4 1 ° F.
TOTAL
GROUND
TO CLEAR
RUN
50 FT. OBS
1115
1985
780
1510
505
1090
AT 7500 FT.
&
32° F.
GROUND
TO CLEAR
TOTAL
RUN
50 FT. OBS
1360
2440
970
1875
640
1375
NOTES: 1 .
Increase the distances 10%for each 35°F. increase in temperature above standard for the pa�ticular allitude.
2 .
For operation on a dry, grass runway, incr�ase distances (both "ground run" and ''total to clear 50 ft. obstacle") by 7% of the
"total to clear 50 ft, obstacle" figure.
-MA X I MUM
RATE-OF-C L I M B
DATA
GROSS
WEIGHT
LBS.
1600
NOTES: 1.
2 .
3.
AT SEA LEVEL
&
59° F.
!AS.MPH
73
RATE
FUEL
CLIMB
USED,
FT.
GAL.
670
o.
6
AT 5000 FT.
&
41° F.
IAS, MPH
FUEL
CLIMB
¥���
FT.
S.L.,GAL.
69
440
1. 6
AT 10000 FT.
&
23° F.
CLIMB
��5�
!AS. MPH
FUEL
S.L.,GAL.
65
220
3. 0
Flaps retracted, full throttle, mixture leaned to smooth operation above 5000 ft.
Fuel used includes warm-up and take-off allowances.
For hot weather, decrease rate of climb 15 ft. /min. for each 10°F above standard day temperature for particular altitude.
-LA N D I N G
DISTAN C·E
FLAPS LOWERED TO 40° - POWER OFF
HARD SURFACE RUNWAY - ZERO WIND
AT SEA LEVEL
&
59° F.
AT 2500 FT.
&
50° F.
AT 5000 FT.
&
4 1 ° F.
GROSS
APPROACH
TOTAL
TOTAL
TOTAL
WEIGHT
SPEED,
GROUND
TO CLEAR
GROUND
TO CLEAR
GROUND
TO CLEAR
LBS.
IAS,MPH
ROLL
50 FT.OBS
ROLL
50 FT. OBS
ROLL
50 FT. OBS
1600
58
445
1075
470
1135
495
1195
NOTES:
1,
Decrease
the
distances shown
by l
0
%fo
r
each
4
knots of headwind
•
•
2 .
Increase the distance by 10% for each 60°F. temperature increase above standard.
AT 7500 FT.
&
32° F.
GROUND
ROLL
520
TOTAL
TO CLEAR
50 FT.OBS
1255
3 .
For operation on a dry, grassy runway, increase distances (both "ground roll" and "total t o clear 5 0 ft. obstacle") by 20%of
the "total to clear 50 ft. obstacle" figure.
Figure
5-3.