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Cessna 402C - Page 146

Cessna 402C
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SECTION
5
PERFORMANCE
NORMAL
LANDING
DISTANCE
CONDITIONS:
1.
Throttles
IDLE.
2.
Landing Gear -
DOWN.
3.
Wing
Flaps -
45°.
4.
Cowl
Fl
aps -
CLOSE.
5.
Level,
Hard
Surface
Runway.
6.
Maximu~
::ffect;ve
Braking.
NOTE:
1.
If
necessary
to
land with wing
flap~
UP,
the
approach speed
should
be
increased
above
the
normal approach speed
by
13
knots.
Expect
total
landing
distance
to
increase
by
35%.
2.
For
altitudes
of
10,000
feet
or
less,
decrease
distance
by
3%
for
each 5 klIOts headwind. For
altitudes
above
10,000
fe"t,
decrease
the
total
landing
distance
by
1%
for
each 2 knots of headwind.
3. For
operations
with
tailwinds
up
to
10
blots,
increase
total
distances
by
14%
for
each 5
knots
wind.
20°C (68°F) 30°C (86°F)
40°C
(l04°F)
SPEED
AT
TOTAL
TOTAL TOTAL
50-FOOT
PRESSURE
GROUND
DISTANCE
GROUND
DISTANCE
GROUND
DISTANCE
WEIGHT
-
OBSTACLE
ALTITUDE
ROLL
-
TO
CLEAR
ROLL
-
TO
CLEAR
ROLL
-
TO
CLEAR
POUNDS
KIAS
-
FEET
FEET
50
FEET
FEET
50
FEET FEET
50
FEET
5500 83 Sea Level 670
2100
690 2120
710
2140
1000
690 2120
720
2150
740
2170
2000
720 2150 740
2170
770 2200
3000
740
2170
770
2200 790 2220
4000 770 2200 800
2230
820 2250
5000
800
2230
830
2260
860
2290
6000 830
2260
860
2290 890
2320
7000
860
2290
890
2320
920 2350
8000
900
2330
930
2360
960
2390
9000
930 2360 960
2390
990
2420
10,000
970
2400
1000
2430
1030
2460
11,000
10lD
2440 1040
2470
1070
2500
12,000
1050
2480
1080
2510 1120
2550
13,000
1090
2520
1130
2560
1160
2590
14,000
1130
2560
1170
2600
1210
2640
15,000 1180
2610
1220
2650 1260
2690
5000 83 sea Level 540 2100 560
2120 580
2130
1000
560
2120
580 2140
600
2150
2000
580
2140
600
2160 620
2180
3000
600 2160
620
2180
640
2200
4000 630
2180
650 2200 670
2220
5000
650 2210 670
2230
690
2250
6000 680 2230 700
2250
720
2280
7000 700 2260 720
2280
750 2300
8000
730 2280 750
2310
780 2330
9000
760
2310
780 2340
810
2360
10,OCO
790 2340 810 2370 840 2390
11,000
820 2370 840
2400
870
2430
12,000
850 2400 880 2430
910
2460
13,000
880
2440
910 2470 940 2500
14,000
920
2470
950
2510
980 2540
15,000
960 2510 990
2540 1020
2580
Figure 5-25 (Sheet 4 of 4)
I
I
1
November
1979
Revision 4 - 1
December
1983
5-43/5-44