Operation
DA 40 NG AFM
Limitations
2.14 FUEL
' Approved fuel grades: |
JET A (ASTM D 1655), |
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JET A-1 (ASTM D 1655), |
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TS-1 (GOST 10227-86), |
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and blends of the above listed fuel grades. |
NOTE
A minimum cetane number of 37 determined acc. to
EN ISO 5165/ASTM D613 is recommended.
NOTE
Use only uncontaminated fuel from reliable sources.
Standard Tank Configuration: |
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Total fuel quantity |
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2 x 15.0 US gal (2 x 56.8 liter) |
Usable fuel |
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2 x 14.0 US gal (2 x 53.0 liter) |
Long Range Tank (if installed) Configuration :
Total fuel quantity |
: 2 x 20.5 US gal (2 x 77.6 liter) |
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Usable fuel |
: 2 x 19.5 US gal (2 x 73.8 liter) |
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Max. indicated fuel quantity |
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14 US gal (53 liter) per tank |
Max. permissible difference |
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between right and left tank |
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9 US gal (approx. 34 liter) |
CAUTION
If an indicator shows 14 US gal, then 19.5 US gal must be assumed for the calculation of the difference between right and left tank.
Page 2 - 24 |
Rev. 2 |
15-Jun-2011 |
EASA |
Doc. # 6.01.15-E |
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approved |
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DA 40 NG AFM
Operation
Limitations
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:
VO = 113 KIAS (ABOVE 1180 KG / 2601 LB)
VO = 108 KIAS (ABOVE 1080 KG / 2381 LB TO 1180 KG / 2601 LB)
VO = 101 KIAS (UP TO 1080 KG / 2381 LB )
'
On the Instrument Panel, Next to the Fuel Quantity Indication:
Long Range Tank (if installed):
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
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
EASA |
Page 2 - 25 |
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approved |
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Operation
DA 40 NG AFM
Limitations
Next to Each of the Two Fuel Filler Necks:
WARNING
APPROVED FUEL
JET-A1
or see Airplane Flight Manual
Next to the Essential Bus Switch:
Ess. Bus NOT for normal operation. See AFM.
Page 2 - 26 |
Rev. 1 |
15-Mar-2011 |
EASA |
Doc. # 6.01.15-E |
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approved |
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DA 40 NG AFM
Operation
Limitations
In the Cowling, on the Door for the Oil Filler Neck:
OIL
SHELL HELIX
ULTRA 5W30
or see Airplane
Flight Manual
Next to the Flap Selector Switch:
max. 
110 KIAS
max.
98 KIAS
On the Fuel Valve:
FUEL VALVE
NORMAL EMERGENCY
CAUTION: INTERMITTENT USE
ONLY (SEE AFM)
'
OFF
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
EASA |
Page 2 - 27 |
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approved |
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Operation
DA 40 NG AFM
Limitations
Next to the Baggage Compartment:
Max. |
30 kg/ |
66 lb |
Baggage Tube Compartment:
Max. 5 kg/ 11 lb
Baggage Tray (if OÄM 40-164 installed, extended baggage compartment):
Page 2 - 28 |
Rev. 1 |
15-Mar-2011 |
EASA |
Doc. # 6.01.15-E |
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approved |
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DA 40 NG AFM
Operation
Limitations
COCKPIT BAGGAGE |
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BAGGAGE |
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COMPARTMENT |
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EXTENSION |
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MAX. 45 kg [100 lb] |
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MAX. 18 kg [40 lb] |
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ARM: 3.89 m [153.1”] |
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ARM: 4.54 m [178.7”] |
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MAX. BAGGAGE TOTAL (COCKPIT BAGGAGE
COMPARTMENT & EXTENSION): 45 kg [100 lb]
CAUTION: OBSERVE WEIGHT AND BALANCE LIMITATIONS
SEE AIRPLANE FLIGHT MANUAL CHAPTER 6
' If Short Baggage Extension (OÄM 40-331) is carried out:
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Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
EASA |
Page 2 - 29 |
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approved |
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Operation
DA 40 NG AFM
Limitations
On the Left Sidewall, Next to the Instrument Panel:
Alternate Static
OPEN 
CLOSED
If Alternate Static is open
Emergency Window and
Cockpit Vent must be closed
Beside the Door Locking Device:
EMERGENCY EXIT:
The keylock must be unlocked during flight
' On Fuel Cooler Inlet Baffle (if installed):
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' On the Instrument Panel:
Remove at Outside Temperatures above 20 °C / 68 °F
______ NO SMOKING ______
Page 2 - 30 |
Rev. 1 |
15-Mar-2011 |
EASA |
Doc. # 6.01.15-E |
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approved |
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