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Wind = 10 KNOTS (HEADWIND)
From Figure 4-57, the Dry Landing Distance is 2000 FEET. VREF = 88 KNOTS, VAPP = 95 KNOTS.
From Figure 7-11, the Wet Landing Distance at VREF = 88 KNOTS is 2750 FEET.
From Figure 7-12, the Wet Landing Distance at VREF+10 KNOTS = 98 KNOTS is 3450 FEET.
7-6 AA 510FM-05
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS UP (WET
RUNWAY OVER A 15 FOOT SCREEN HEIGHT) (ANTI-ICE
OFF)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 7-2. If the runway has a gradient,
adjust V1 and takeoff field length using figure 7-1.
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 7-1*
510FM-06 AH 7-7
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 1 of 15)*
7-8 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 2)*
510FM-06 AH 7-9
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 3)*
7-10 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 4)*
510FM-06 AH 7-11
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 5)*
7-12 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 6)*
510FM-06 AH 7-13
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 7)*
7-14 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 8)*
510FM-06 AH 7-15
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 9)*
7-16 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 10)*
510FM-06 AH 7-17
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 11)*
7-18 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 12)*
510FM-06 AH 7-19
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 13)*
7-20 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 14)*
510FM-06 AH 7-21
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 15)*
7-22 AH 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
TAKEOFF FIELD LENGTH - FEET, FLAPS UP (WET
RUNWAY OVER A 15 FOOT SCREEN HEIGHT) (ANTI-ICE
OFF)
Determine takeoff field length, V1, VR, V2 and VENR from Figure 7-2. If the runway has a gradient,
adjust V1 and takeoff field length using figure 7-1.
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 7-1
510FM-06 AI 7-7.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 1 of 15)
7-8.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 2)
510FM-06 AI 7-9.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 3)
7-10.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 4)
510FM-06 AI 7-11.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 5)
7-12.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 6)
510FM-06 AI 7-13.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 7)
7-14.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 8)
510FM-06 AI 7-15.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 9)
7-16.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 10)
510FM-06 AI 7-17.1
SECTION VII - ADVISORY INFORMATION MODEL 510
U.S. Configuration
Figure 7-2 (Sheet 11)
7-18.1 AI 510FM-06
MODEL 510 SECTION VII - ADVISORY INFORMATION
Configuration U.S.
Figure 7-2 (Sheet 12)
510FM-06 AI 7-19.1
SECTION VII - ADVISORY INFORMATION MODEL 510
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Citation Mustang airplane flight manual 3(31)
