Normal Operating
Procedures
DA 62 AFM
4A.6.8 CLIMB
Initial Climb Check
1. Landing light. . . . . . . . . . . . . . . . . . . . . . . . . . OFF/as required
2. Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . check UP
3. FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . check UP
4. Fuel pumps LH/RH . . . . . . . . . . . . . . . . . . . . OFF
5. Airspeeds, best rate-of-climb . . . . . . . . . . . . . up to 1999 kg (4407 lb):
87 KIAS
above 1999 kg (4407 lb):
89 KIAS
Airspeeds, as required for en route
(cruise) climb . . . . . . . . . . . . . . . . . . . . . . . . . up to 1999 kg (4407 lb):
93 KIAS
above 1999 kg (4407 lb):
96 KIAS
6. POWER lever. . . . . . . . . . . . . . . . . . . . . . . . . up to 95%
7. Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . as required (ball centered)
8. Annunciations/Engine/System Page . . . . . . . monitor
CAUTION
If the oil temperature and/or coolant temperature reaches the
yellow range during climb, flight should be continued with the
airspeed increased by 10 kts and power reduced by 10%
(reduced climb rate) for better engine cooling.
CONTINUED
Page 4A - 38 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E