Using Figure 11.14, verify the ROT you calculated in Problem 19. 7 128965 1 9 8 7

Using Figure 11.14, verify the ROT you calculated in Problem 19.

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7 128965 1 9 8 7 6 5 4 9 19 8 7 6 5 4 3 2 19 8 7 6 5 4 3 2 1 90000 90 9 8 7 6 5 4 80000 80 8 70000 70 7 80 60000 60 6 BANK 50000 50 5 ANGLE FOR 40000 40 4 RATE 3 (70 OF TURN 30000 30 3 2. 4 3. Example: V = 300 kts. = 30 r = 13,800 ft ROT = 2.10/sec 2: 900 008 00 700 009 5 19 8 7 6 5 4 3 2 60 50 20000 20 2 40 10000 10 1 30 9000 9 9 8000 8 8 7000 7 (20 6000 6 6 5000 5 5 S 10 4000 D 4 4 20 Radius of turn, it 3000 2000 ROT Rate of turn, degree 3 3 2 -2 000 1.0 1 900 0.9 9 10 20 800 0.8 8 30 700 0.7 -7 40 50 600 0.6 6 60 Bank angle 500 for 0.5 5 70 turn radius 400 0.4 4 80 300 0.3 3 60 V. True airspeed, kts. 200 0.2 2 1 1987 6 5 4 3 2