DA 40 NG AFM
Performance
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 5 - 23
5.3.10 TIME, FUEL AND DISTANCE TO CLIMB
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Conditions:
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- Power lever . . . . . . . . . . . . . . . . . . . . . . . . . 92% or max. 2100 RPM
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- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
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- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88 KIAS
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NOTE
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Distances shown are based on zero wind. Fuel for start, taxi
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and take-off not included. Add 5% to the time and fuel and
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10% to the distance for each 10° C (18° F) increase in OAT.
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Example:
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OAT at take-off . . . . . . . . . . . . . . . . . . . . . . . 11°C (52°F)
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Airfield pressure altitude . . . . . . . . . . . . . . . . 2000 ft (1200 m)
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Initial climb weight . . . . . . . . . . . . . . . . . . . . . 1310 kg (2888 lb)
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OAT at cruise . . . . . . . . . . . . . . . . . . . . . . . . -17° C (2° F)
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Cruise altitude . . . . . . . . . . . . . . . . . . . . . . . . 16000 ft (4900 m)
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Time, fuel and distance to climb at airfield: 3 min, 0.4 US gal and 5 NM (1)
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Time, fuel and distance to climb at cruise: 26 min, 3.7 US gal and 43 NM (2)
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Subtract (1) from (2) to obtain time, fuel and distance to climb from airfield to cruise:
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Time to cruise altitude: 26 min - 3 min = 23 min
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Fuel to cruise altitude: 3.7 US gal - 0.4 US gal = 3.3 US gal
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Distance to cruise altitude: 43 NM - 5 NM = 38 NM
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Содержание DA 40 NG
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Страница 2: ...DA 40 NG AFM Introduction Page 0 0a Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Страница 160: ...Normal Operating Procedures DA 40 NG AFM Page 4A 40 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Страница 190: ...Abnormal Operating Procedures DA 40 NG AFM Page 4B 30 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Страница 197: ...DA 40 NG AFM Performance Doc 6 01 15 E Rev 3 01 Jul 2014 Page 5 7 5 3 4 INTERNATIONAL STANDARD ATMOSPHERE...
Страница 240: ...Mass Balance DA 40 NG AFM Page 6 8 Rev 3 01 Jul 2014 Doc 6 01 15 E 6 4 2 LOADING DIAGRAM...
Страница 260: ...DA 40 NG AFM Mass and Balance Doc No 6 01 15 E Rev 3 01 Jul 2014 Page 6 28 Intentionally left blank...
Страница 287: ...DA 40 NG AFM Airplane Description Doc 6 01 15 E Rev 3 01 Jul 2014 Page 7 27 7 9 4 FUEL SYSTEM Standard Tank Schematic...
Страница 288: ...Airplane Description DA 40 NG AFM Page 7 28 Rev 3 01 Jul 2014 Doc 6 01 15 E Long Range Tank Schematic...
Страница 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
Страница 322: ...Handling DA 40 NG AFM Page 8 14 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...