DA 42 NG AFM Performance
Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 41
Gradient
ROC fpm
TAS KTAS
[%] .
[]
[]
098
5.3.12 GO-AROUND CLIMB PERFORMANCE'
Conditions:
- Power lever ......................... both MAX
- Flaps .............................. LDG
- Landing gear ........................ extended
- Airspeed:
Up to 1900 kg (4189 lb) ................ v
REF
= 84 KIAS'
Above 1900 kg (4189 lb) ............... v
REF
= 86 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:
4.7° for Maximum Take-Off Mass (1900 kg / 4189 lb)
5.1° for Maximum Landing Mass (1805 kg / 3979 lb)
If MÄM 42-678 is carried out:
'
3.9° for Maximum Take-Off Mass (1999 kg / 4407 lb)'
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