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2012
1951
13800
13600
13400
4206
4145
4084
6200
6000
5800
1890
1829
1768
13200
13000
12800
4023
3962
3901
5600
5400
5200
1707
1646
1585
12600
12400
12200
3840
3780
3719
5000
4800
4600
1524
1463
1402
12000
11800
11600
3658
3597
3536
4400
4200
4000
1341
1280
1219
11400
11200
11000
3475
3414
3353
3800
3600
3400
1158
1097
1036
10800
10600
10400
3292
3231
3170
3200
3000
2800
975
914
853
10200
10000
9800
3109
3048
2987
2600
2400
2200
792
732
671
9600
9400
9200
2926
2865
2804
2000
1800
1600
610
549
488
9000
8800
8600
2743
2682
2621
1400
1200
1000
427
366
305
8400
8200
8000
2560
2499
2438
800
600
400
244
183
122
7800
7600
2377
2316
200
0
61
0
4-20 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
AIRSPEED AND MACHMETER CALIBRATION
Figure 4-9
AIRSPEED
CALIBRATION
(PILOT/COPILOT
SYSTEMS)
AIRSPEED
CALIBRATION
(STANDBY
SYSTEM)
MACHMETER
CALIBRATION
(PILOT/COPILOT)
IN FLIGHT ANY GEAR
AND FLAP POSITION
IN FLIGHT ANY GEAR
AND FLAP POSITION
ANY ALTITUDES ANY
FLAP POSITION
KIAS KCAS KIAS KCAS IND
MACH
CAL
MACH
80
90
100
81
91
101
80
90
100
81
91
101
0.400
0.410
0.420
0.402
0.412
0.422
110
120
130
111
121
131
110
120
130
111
121
131
0.430
0.440
0.450
0.432
0.442
0.452
140
150
160
141
151
161
140
150
160
141
151
161
0.460
0.470
0.480
0.462
0.472
0.482
170
180
190
171
181
191
170
180
190
172
182
192
0.490
0.500
0.510
0.492
0.502
0.512
200
210
220
201
211
221
200
210
220
202
212
222
0.520
0.530
0.540
0.522
0.532
0.542
230
240
250
231
241
251
230
240
250
232
242
252
0.550
0.560
0.570
0.552
0.562
0.572
260
263
261
264
260
263
262
265
0.580
0.590
0.600
0.582
0.593
0.603
0.610
0.620
0.630
0.613
0.623
0.633
510FM-00 AA 4-21
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
ALTIMETER POSITION CORRECTION - FEET
PILOT AND COPILOT SYSTEMS
NOTE
Shaded areas are above MMO and are for interpolation only.
Figure 4-10
4-22 AA 510FM-00
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
ALTIMETER POSITION CORRECTION - FEET
STANDBY SYSTEM
NOTE
Shaded areas are above MMO and are for interpolation only.
Figure 4-11
510FM-00 AA 4-23
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
STALL SPEEDS - KCAS
Figure 4-12 (Sheet 1 of 2)*
4-24 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
STANDARD CHARTS
FAA APPROVED
Configuration U.S.
STALL SPEEDS - KCAS
Figure 4-12 (Sheet 2)*
510FM-05 AA 4-25
SECTION IV - PERFORMANCE MODEL 510
STANDARD CHARTS
FAA APPROVED
U.S. Configuration
TAKEOFF THRUST SETTING EXAMPLES
EXAMPLE 1:
Anti-Ice = OFF
a. Indicated RAT = 5°C
b. Pressure Altitude = 2000 FEET
c. N1 = 90.9% RPM (Refer to Figure 4-13)
EXAMPLE 2:
Anti-Ice = ON
a. Indicated RAT = -15°C
b. Pressure Altitude = 4000 FEET
c. N1 = 89.9% RPM (Refer to Figure 4-14)
　
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