Operation
DA 40 NG AFM
Limitations
2.10 MANEUVERING LOAD FACTORS
WARNING
The table below shows structural limitations. Exceeding the maximum load factors will lead to an overstressing of the airplane.
CAUTION
Intentional negative g-maneuvers are not permitted.
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at vO |
at vNE |
with flaps in T/O |
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or LDG position |
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Positive |
3.8 |
3.8 |
2.0 |
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Negative |
-1.52 |
0 |
0 |
Page 2 - 18 |
Rev. 1 |
15-Mar-2011 |
EASA |
Doc. # 6.01.15-E |
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DA 40 NG AFM
Operation
Limitations
2.11 OPERATING ALTITUDE
The maximum operating altitude is 16,400 ft (5,000 m) pressure altitude.
2.12 FLIGHT CREW
Minimum crew |
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1 |
(one person) |
Maximum number of occupants : |
4 |
(four persons) |
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Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
EASA |
Page 2 - 19 |
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Operation
DA 40 NG AFM
Limitations
2.13 KINDS OF OPERATION
Provided that national operational requirements are met, the following kinds of operation are approved:
•Daytime flights according to Visual Flight Rules (VFR)
•With the appropriate equipment: night flights according to Visual Flight Rules
(NVFR)
•With the appropriate equipment: flights according to Instrument Flight Rules (IFR)
•Take-off and landing on paved surfaces
•Take-off and landing on unpaved surfaces
Flights into known or forecast icing conditions are prohibited.
Flights into known thunderstorms are prohibited.
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Minimum Operational Equipment (Serviceable) |
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The following table lists the minimum serviceable equipment required by JAR-23. Additional |
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minimum equipment for the intended operation may be required by national operating |
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rules and also depends on the route to be flown. |
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NOTE |
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Many of the items of minimum equipment listed in the |
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following table are integrated in the G1000 (if installed). |
Page 2 - 20 |
Rev. 1 |
15-Mar-2011 |
EASA |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
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Operation |
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Limitations |
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For daytime VFR |
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In addition |
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In addition |
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flights |
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for night VFR flights |
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for IFR flights |
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Flight & |
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Airspeed indicator |
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Vertical speed |
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Second airspeed |
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naviga- |
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Altimeter |
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indicator (VSI) |
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indicator (on PFD |
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tion |
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Magnetic compass |
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Attitude gyro |
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and backup, if |
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Turn & bank indicator |
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G1000 is installed) |
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pilot in command |
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Directional gyro |
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Second altimeter |
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VHF radio (COM) |
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Second attitude |
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VOR receiver |
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gyro (on PFD and |
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Transponder (XPDR) |
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backup, if G1000 is |
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GPS receiver (part of |
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installed) |
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G1000, if installed) |
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Second VHF radio |
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Second headset (if |
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(COM) |
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PM 1000 intercom is |
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VOR-LOC-GP |
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installed) |
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receiver |
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Second GPS |
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receiver (part of |
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G1000, if installed) |
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
EASA |
Page 2 - 21 |
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approved |
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Operation
DA 40 NG AFM
Limitations
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For daytime VFR |
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In addition |
In addition |
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flights |
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for night VFR flights |
for IFR flights |
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Engine |
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Fuel qty. |
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Ammeter |
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instru- |
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Oil press. |
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Voltmeter |
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Oil temp. |
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Coolant temp. |
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Coolant level |
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indicator |
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Gearbox temp. |
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Load |
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Prop. RPM |
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• Fuel temp. left & |
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right tank |
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Fuel flow |
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Fuel pressure |
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warning |
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ECU A/B Caution |
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ENGINE Caution |
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(if White Wire |
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annunciator panel |
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is installed) |
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Lighting |
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Position lights |
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Strobe lights (anti |
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collision lights) |
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Landing light |
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Instrument lighting |
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Flood light |
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Flashlight |
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Page 2 - 22 |
Rev. 1 |
15-Mar-2011 |
EASA |
Doc. # 6.01.15-E |
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approved |
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DA 40 NG AFM |
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Operation |
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Limitations |
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For daytime VFR |
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In addition |
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In addition |
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flights |
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for night VFR flights |
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for IFR flights |
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Other |
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Stall warning system |
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Pitot heating system |
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• Emergency battery |
opera- |
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Alternate means for |
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Alternate static valve |
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(for backup attitude |
tional |
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fuel quantity |
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gyro and flood light) |
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mini- |
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mum |
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indication (see |
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equip- |
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Section 7.9) |
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ment |
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Safety belts for each |
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occupied seat |
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Airplane Flight |
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Manual |
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NOTE
A list of approved equipment can be found in Chapter 6.
Engine Systems and Equipment
All engine systems and equipment must be functional prior to airplane take-off. Any engine system or equipment failure must be corrected before next flight.
Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
EASA |
Page 2 - 23 |
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approved |
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