DA 62 AFM Performance
5.3.7 CLIMB PERFORMANCE - TAKE-OFF CLIMB
Conditions:
- Power lever. . . . . . . . . . . . . . . . . . . . . . . . . . both 95%
- Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP or T/O
- Landing gear. . . . . . . . . . . . . . . . . . . . . . . . . retracted
- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . v
Y
The climb performance tables show the rate of climb. The gradient of climb can be
calculated using the following formula:
NOTE
Rate of climb at MTOM (2300 kg/5071 lb) with a power setting
of 100% at MSL and ISA conditions:
- 1075 ft/min (5.5 m/s) with flaps UP
- 1018 ft/min (5.2 m/s) with flaps T/O.
Rate of climb at 1999 kg/4407 lb with a power setting of 100%
at MSL and ISA conditions:
- 1317 ft/min (6.7 m/s) with flaps UP
- 1250 ft/min (6.4 m/s) with flaps T/O.
Doc. No. 11.01.05-E Rev. 0
11-Jan-2019
Page 5 - 35