Diamond DA 62 - Cruise Performance

DA 62 AFM Performance
5.3.11 CRUISE PERFORMANCE
Conditions:
- Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
- Landing gear . . . . . . . . . . . . . . . . . . . . . . . . retracted
- Weight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . up to1999 kg/above 1999 kg
For conversion of OAT to delta-ISA temperatures refer to Chapter 5.3.3 - INTERNATIONAL
STANDARD ATMOSPHERE.
Doc. No. 11.01.05-E Rev. 0
11-Jan-2019
Page 5 - 59