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The charts in section 5 of the AFM…
Field elevation 2500 feet
Takeoff Weight: 4200 KG
What is the total takeoff distance with Flaps 15?
Distance to climb?
Weight: 4500 kg
From Sea-level to 15,000 feet.
Crusing at 20,000 feet. Aircraft weight 4500 kg.
In the event of an engine failure, with a tailwind of 10 kts, what is the distance you will be able to glide? Using this chart?
When operating in known icing conditions, what is true?