Sennheiser SI 234 - ANNEXE 802 Operations Instructions download pdf (Page 287)

100

101

DA 42 NG AFM Performance

Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 17

Gradient

ROC fpm

TAS KTAS

[%] .

[]



098

5.3.7 CLIMB PERFORMANCE (ALL ENGINES OPERATING)

Conditions:

- Power lever ......................... both 92%

- Flaps .............................. UP or APP

- Landing gear ........................ retracted

- Airspeed ............................ v

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 (1900 kg / 4189 lb) with a power

setting of 100% at MSL and ISA conditions:

- 1337 ft/min (6.8 m/s) with flaps UP

- 1267 ft/min (6.4 m/s) with flaps APP

NOTE'

If MÄM 42-678 is installed, the rate of climb at MTOM'

(1999 kg / 4407 lb) with a power setting of 100% at MSL'

and ISA conditions:'

- 1243 ft/min (6.3 m/s) with flaps UP'

- 1183 ft/min (6.0 m/s) with flaps APP'

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Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 287

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