Cessna 402C - Page 127

SECTiON 5
PERfORMANCE
ACCELERATE STOP OIST ANCE
I
CONDITIONS:
1. 2700 RPM and 39.0 Inches Hg. Manifold Pressure
Before Brake Release.
2. Mixtures - CHECK Fuel Flows In the White Arc.
3. Wing Flaps - UP.
4. Cowl Flaps - OPEN.
5. Level. Hard Surface, Dry Runway.
6. Engine Failure at Engine Failure Speed.
7. Idle Power and Maximum Effective Braking After
Engine Failure.
NOTE:
1. If full power is applied
without brakes set. dis-
tances apply from point
where full power is applied.
2. Decrease distance 3% for
each 5 knots headwind.
3. Increase distance 13% for
each 5 knots tailwind.
ENGINE
TOTAL DISTANCE - FEET
FAILURE
PRESSURE
WEIGHT - SPEED -
ALTITUDE - -20°C -10°C O'C
+10
o
C
+20
o
C +30
o
C
+40
o
C
POUNDS KIAS
FEET
_4°F
+14
o
F
32°F
+50
o
F
+68
o
F
+86
o
F
+104
o
F
6850
95
Sea Level 3010
3200 3400
3620 3860 4110
4440
1000 3150
3350 3570
3800 4040 4360
4660
2000
3300
3510 3740
3980 4290 4580
4900
3000 3460
3680 3920 4220 4500 4810
5150
4000 3630
3870 4150 4430
4730
5050
5420
5000 3810
4090 4360
4650 4970 5320
5700
6000
4020
4290
4580
4890 5220 5590
6010
7000 4220
4510 4810 5140 5500 5890
6330
8000 4440
4740
5060 5410
5790 6210
6680
9000 4660
4980
5330
5700 6100 6550
7060
10 000 4910
5250 5610 6010
6440
6920
7460
6500
92
Sea Level 2680 2850 3020
3210 3420 3640
3890
1000 2800
2980
3170
3370 3590 3820
4130
2000 2940
3120 3320 3530
3760 4060 4340
3000
3080
3270 3480
3710 3990 4260
4560
4000 3230
3430
3660
3930 4190 4480
4790
5000 3380
3600 3870 4130
4400
4710
5040
6000 3550
3810 4060 4340 4630 4950
5310
7000 3750
4000 4270 4560
48]0
5220
5600
8000 3940
4210 4490 4800 5130 5500
5900
9000 4140
4420 4720 5050
5410
5800
6230
10,000
4360
4660 4980
5320 5700
6120
6580
6000
89
Sea Level 2240
2380
2530
2680 2850 3030
3230
1000 2350
2490 2650 2810 2990 3180
3390
2000 2460
2610 2780
2950 3140 3340 3560
3000
2570
2740 2910
3090 3290
3510
3780
4000 2700
2870
3050
3250 3460 3720
3970
5000 2830
3010 3210 3410 3660 3910
4180
6000 2970
3160 3370 3610 3850 4110
4400
7000
3120
3320 3560 3800
4050 4330 4630
8000 3280
3510
3740
3990 4260 4550
4880
9000 3460
3690 3940 4200
4490
4800 5150
10 000 3640
3880 4140 4420 4730 5060
5430
5500 89
Sea
Level
1870
1980
2100
2220 2350 2490 2650
1000 1950
2070 2190 2320
2460
2610
2770
2000 2040 2170 2300
2430
2580
2740 2910
3000 2140
2270
2410
2550 2710 2870 3080
4000
2240
2380
2520
2670 2840 3040 3230
5000 2350
2490 2640 2810 3000
3190
3390
6000
2460
2610 2770 2960 3150 3350 3560
7000 2580 2740 2930 3UO 3300 3520
3740
8000 2710
2890
3070
3260 3470 3690 3940
9000 2850 3030 3230
3430
3650 3880
4140
10.000 3000
3190
3390
3610 3840 4090 4360
5000 89
Sea
Level 1520 1610 1710 1800 1910 2020
2130
1000 1590
1690 1780 1890 1990
2IlO 2230
2000 1670 1760 1870 1970 2090 2210
2330
3000 1740
1840
1950
2070
2180 2310
2470
4000 1820
1930
2040
2160 2290 2440 2580
5000
1910
2020 2140 2270 2410 2550
2710
6000 2000
2120
2240
2390 2530 2680
2840
7000 2100
2220
2360
2500 2650 2810
2980
8000 2200
2340 2480 2620
2780 2950
3120
9000 2310
2450 2600
2750 2920 3090
3280
10,000
2420
2570
2730
2890
3060 3250
3450
F,gure 5-11
1 November 1979