Sennheiser SI 234 - ANNEXE 802 Operations Instructions download pdf (Page 295)

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DA 42 NG AFM Performance

Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 5 - 25

5.3.9 TIME, FUEL AND DISTANCE TO CLIMB'

Conditions:'

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

- Flaps .............................. UP'

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

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

NOTE'

Distances shown are based on zero wind. Fuel for start, taxi'

and take-off not included. Add 10% to the time, fuel and'

distance for each 10° C (12° F) increase in OAT.'

Example:'

OAT at take-off ....................... 11°C (52°F)'

Airfield pressure altitude ................ 2000 ft (1200 m)'

Initial climb weight..................... 1900 kg (4189 lb)'

OAT at cruise ........................ -17° C (2° F)'

Cruise altitude........................ 16000 ft (4900 m)'

Time, fuel and distance to climb at airfield: 2 min, 0.5 US gal and 3 NM (1)'

Time, fuel and distance to climb at cruise: 14 min, 3.8 US gal and 24 NM (2)'

Subtract (1) from (2) to obtain time, fuel and distance to climb from airfield to cruise:'

Time to cruise altitude: 14 min - 2 min = 12 min'

Fuel to cruise altitude: 3.8 US gal - 0.5 US gal = 3.3 US gal'

Distance to cruise altitude: 24 NM - 3 NM = 21 NM'

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Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 295

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