DA 40 NG AFM
Operating
Limitations
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
EASA
approved
Page 2 - 29
max. usable fuel: 2 x 19.5 US gal
*
Max. indicated fuel quantity: 2 x 14 US gal
*
Refer to AFM to use entire tank capacity
*
Max. difference LH/RH tank: 9 US gal
2.15 LIMITATION PLACARDS
All
limitation
placards relevant for the base DA 40 NG airplane are shown below. A
list of all placards is included in the Airplane Maintenance Manual (Doc. No. 6.02.15),
Chapter 11.
On the Instrument Panel:
THIS AIRPLANE MAY ONLY BE OPERATED IN ACCORDANCE WITH THE
AIRPLANE FLIGHT MANUAL IN THE "NORMAL" CATEGORY IN NON-ICING
CONDITIONS. PROVIDED THAT NATIONAL OPERATIONAL REQUIREMENTS
ARE MET AND THE APPROPRIATE EQUIPMENT IS INSTALLED AND
OPERATIONAL, THIS AIRPLANE IS APPROVED FOR THE FOLLOWING
KINDS OF OPERATION: DAY VFR, NIGHT VFR, IFR. ALL AEROBATIC
MANEUVERS INCLUDING SPINNING ARE PROHIBITED. FOR FURTHER
OPERATIONAL LIMITATIONS REFER TO THE AIRPLANE FLIGHT MANUAL.
OPERATING MANEUVERING SPEED:
V
O
= 113 KIAS (ABOVE 1180 KG / 2601 LB)
V
O
= 108 KIAS (ABOVE 1080 KG / 2381 LB TO 1180 KG / 2601 LB)
V
O
= 101 KIAS (UP TO 1080 KG / 2381 LB )
On the Instrument Panel, Next to the Fuel Quantity Indication:
Long Range Tank (if installed):
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...