Diamond DA 62 - Go-Around Climb Performance

Performance DA 62 AFM
5.3.13 GO-AROUND CLIMB PERFORMANCE
Conditions:
- Power lever . . . . . . . . . . . . . . . . . . . . . . . . . . both MAX
- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LDG
- Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . extended
- Airspeed: . . . . . . . . . . . . . . . . . . . . . . . . . . . . v
REF
The climb performance charts show the rate of climb. The gradient and angle of climb
can be calculated using the following formula:
NOTE
The angles of climb at MSL and ISA condition are:
2.7 ° for Maximum Take-Off Mass (2300 kg/5071 lb)
4.3 ° for 1999 kg/4407 lb
Page 5 - 88 Rev. 0
11-Jan-2019
Doc. No. 11.01.05-E