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Refer to figure. (Figure 4.5 CAP 698) Determine the climb limited take-off mas...
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Refer to figure. (Figure 4.5 CAP 698)Determine the climb limited take-off mass, given:Temperature (OAT): 35°CAirport Pressure altitude: 3 000 ftTake off flap setting: 5°A/C air conditions packs: OffEngine anti-icing system: Off
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