Cessna 402C - Page 126

G,~'402C
MODEL
NORMAL TAKEOFF DISTANCE
SECTION 5
PERFORMANCE
CONDITIONS:
1. 2700 RPM and 39 Inches Hg. Manifold Pressure
Before Brake Release.
2. Mixtures - CHECK Fuel Flows In the White Arc.
3. !-ling Flaps ~ UP.
4. Cowl Flaps - GDEN.
5. Level, Hard Surface, Dry Runway.
NOTE;
1. If full pow!!r ;s appl ied without
brakes set, distances apply from
point wf)ere full power is applied.
2. For altitudes of 10,000 feet or less,
decreas~ di stance 3% for each 5 knots
of headwind. For altitudr.s above
10,000 feet, decrease distance by 1%
for each 2 knots of headwind.
3. Increase distarlCe 12% for each 5
knots tailwind.
TAKEOFF
zooe (58°F)
30°C (86°F) 40°C (104°F)
TO 50-
FOOT PRESSURE
TOTAL TOTAL
TOTAL
WEIGHT - OBSTACLE ALTiTUDE- GROUND DISTANCE
GROUND DISTANCE
GROUND
D1STANCE
POUNDS SpEEO- FEET ROLL - TO CLEAR ROLL - TO CLEAR ROLL -
TO CLEAR
KIAS
FEET 50 FEET FEET 50 FEET FEET
50 FEET
5500 89
Sea Level 1120 1430 1220
1560
1330
1720
1000 1180
1500 1290
1650 1410
1810
2000 1250
1590 1360
1740
1490
1910
3000 1330
1670 1450
1840
1510
2050
4000 1410
1770 1550 1970 1700
2170
5000 1520
1890 1650 2080
1810
2290
6000
1610 2000 1750 2200 1920
2430
7000 1700
2UO
1860
2320
2030
2570
8000
1810
2230 1970 2460
2160
2730
9000 1920
2370 2100 2610
2300
2900
10,000 2040 2510 2230 2770 2440 3080
11,000 2170
2560 2370 2940 2600 3280
12,000 2310
2830 2530 3130 2770
3490
13,000 2550
3160 2790 3520 3070 3970
14,000 2720
3370 2980 3760 3270
4250
15,000 2900
3590 3180
4010
3490
4560
5000
89
Sea Level 900
1190
980
1290
1060
1410
1000
960 1250 1030
1360
1120
1490
2000
1010 1310 1090
1430
1180
1570
3000
1070 1380 1160
1510
1270
1570
4000
1130 1450
1240 1610 1340
1770
5000
1210 1550 1310
1690
1420
1850
6000
1280
1530 1390
1790
1500
1970
7000
1350 1720
1470 1890 1590
2080
8000
1430 1820 1550
1990
1680
2200
9000
1520
1920 1640 2110 1780
2330
10,000 1610 2030 1740
2230 1890
2470
11,000 1700
2150 1850
2350
2000
2620
12,000 1810
2280 1960
2510
2130
2790
13,000 1980
2530 2150 2810 2330
3150
14,000
2100 2590 2280
2990 2480
3370
15,000 2230
2860 2420
3180
2530
3600
Figure 5-10 (Sheet 4 of 4)
1 November 1979
Revision 4 - 1 December 1983
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5-23