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U.S. Configuration
Figure 7-4 (Sheet 13)
7-36.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-4 (Sheet 14)
510FM-06 AI 7-37.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-4 (Sheet 15)
7-38.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS 15°
(WET RUNWAY OVER A 15 FOOT SCREEN HEIGHT)
(ANTI-ICE OFF)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 7-6. If the runway has a gradient,
adjust V1 and takeoff field length using Figure 7-5.
If the required distance is greater than the available distance, the airplane weight must be reduced
until distance required is less than or equal to distance available.
Figure 7-5
510FM-06 AA 7-39
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 1 of 15)*
7-40 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 2)*
510FM-05 AA 7-41
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 3)*
7-42 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 4)*
510FM-05 AA 7-43
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 5)*
7-44 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 6)*
510FM-05 AA 7-45
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 7)*
7-46 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 8)*
510FM-05 AA 7-47
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 9)*
7-48 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 10)*
510FM-05 AA 7-49
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 11)*
7-50 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 12)*
510FM-05 AA 7-51
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 13)*
7-52 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-6 (Sheet 14)*
510FM-05 AA 7-53
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-6 (Sheet 15)*
7-54 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS 15°
(WET RUNWAY OVER A 15 FOOT SCREEN HEIGHT)
(ANTI-ICE ON)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 7-8. If the runway has a gradient,
adjust V1 and takeoff field length using Figure 7-7.
If the required distance is greater than the available distance, the airplane weight must be reduced
until distance required is less than or equal to distance available.
Figure 7-7
510FM-06 AA 7-55
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-8 (Sheet 1 of 15)*
7-56 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-8 (Sheet 2)*
510FM-05 AA 7-57
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-8 (Sheet 3)*
7-58 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-8 (Sheet 4)*
510FM-05 AA 7-59
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-8 (Sheet 5)*
7-60 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-8 (Sheet 6)*
510FM-05 AA 7-61
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-8 (Sheet 7)*
7-62 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-8 (Sheet 8)*
510FM-05 AA 7-63
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-8 (Sheet 9)*
7-64 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-8 (Sheet 10)*
510FM-05 AA 7-65
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-8 (Sheet 11)*
7-66 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-8 (Sheet 12)*
510FM-05 AA 7-67
SECTION VII - ADVISORY INFORMATION MODEL 510
　
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本文鏈接地址：Citation Mustang airplane flight manual 3(33)