Performance
DA 40 NG AFM
Page 5 - 26
Rev. 3
01-Jul-2014
Doc. # 6.01.15-E
5.3.11 CRUISE PERFORMANCE
%
NOTE
For operation without wheel fairings a performance reduction
of 4% TAS at all power settings must be expected.
Conditions:
%
-
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
%
-
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . retracted
%
-
Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1310 kg (2888 lb)
%
%
For conversion of OAT to delta-ISA temperatures refer to Chapter 5.3.3 - INTERNATIONAL
%
STANDARD ATMOSPHERE.
%
%
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...