Diamond Aircraft DV 20 E - Page 144

Performance DV 20 E AFM
Page 5 - 24 Rev. 2 22-Mar-2022 Doc. No. 4.01.25-E
Gradient
ROC fpm
TAS KTAS
[%] .
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 098
5.3.10 GO-AROUND CLIMB PERFORMANCE
Conditions:
- Throttle............................. MAX
- Propeller speed lever .................. HIGH
- Flaps .............................. LDG
- Airspeed: ........................... v
REF
(56 KIAS)
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:
4.5° for Maximum Take-Off Mass (800 kg / 1764 lb).