DA 40 NG AFM
Operating
Limitations
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
EASA
approved
Page 2 - 17
NOTE
In some countries the beginning of a flight is defined by
starting the engine. In those countries a maximum ramp mass
4 kg (9 lb) above the maximum take-off mass is approved.
At the time of lift-off the maximum permitted take-off mass
must not be exceeded.
NOTE
The maximum zero fuel mass is the highest mass with empty
fuel tanks.
Summary of Contents for DA 40 NG
Page 1: ......
Page 2: ...DA 40 NG AFM Introduction Page 0 0a Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Page 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...
Page 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
Page 322: ...Handling DA 40 NG AFM Page 8 14 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
