Operating Limitations |
DA 42 NG AFM |
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2.10 MANEUVERING LOAD FACTORS
NOTE
The tables below show structural limitations. The load factor limits for the engine must also be observed. Refer to the corresponding Operation Manual for the engine.
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at vO |
at vNE |
with flaps in APP |
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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 |
-1.52 |
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WARNING
Exceeding the maximum structural load factors will lead to overstressing of the airplane.
CAUTION
Intentional negative g- maneuvers are not permitted.
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EASA |
Doc. No. 7.01.15-E |
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DA 42 NG AFM |
Operating Limitations |
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2.11 OPERATING ALTITUDE
The maximum operating altitude is 18,000 ft (5,486 m) pressure altitude.
2.12 FLIGHT CREW
Minimum crew |
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1 (one person) |
Maximum number of occupants |
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4 (four persons) |
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 grass surfaces
Flights into known or forecast thunderstorms are prohibited.
Minimum Operational Equipment (Serviceable)
The following table lists the minimum serviceable equipment required by JAR-23. Additional minimum equipment for the intended operation may be required by national operating rules and also depends on the route to be flown.
EASA
Doc. No. 7.01.15-E Rev. 1 18-Feb-2009 Page 2 - 21 approved
Operating Limitations |
DA 42 NG AFM |
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NOTE
Many of the items of minimum equipment listed in the following table are integrated in the G1000.
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for daytime |
in addition for |
in addition for |
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VFR flights |
night VFR flights |
IFR flights |
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Flight & |
* airspeed indicator |
* vertical speed |
* second airspeed |
navigation |
(on G1000 PFD or |
indicator (VSI) |
indicator (both, on |
instruments |
backup) |
* attitude gyro |
G1000 PFD and |
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backup) |
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* altimeter (on G1000 |
(artificial horizon; on |
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PFD or backup) |
G1000 PFD or |
* second altimeter |
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* magnetic compass |
backup) |
(both, on G1000 |
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* turn & bank |
PFD and backup) |
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* 1 headset, used by |
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indicator (on G1000 |
* second attitude |
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pilot in command |
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PFD) |
gyro (both, on |
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* directional gyro |
G1000 PFD and |
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backup) |
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* VHF radio (COM) |
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* second VHF radio |
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with speaker and |
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(COM) |
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microphone |
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* VOR-LOC-GP |
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* VOR receiver |
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receiver |
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* transponder |
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* second GPS |
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(XPDR), mode A |
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receiver (part of |
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and mode C |
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G1000) |
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* GPS receiver (part |
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of G1000) |
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18-Feb-2009 |
EASA |
Doc. No. 7.01.15-E |
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DA 42 NG AFM |
Operating Limitations |
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for daytime |
in addition for |
in addition for |
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VFR flights |
night VFR flights |
IFR flights |
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Engine |
* fuel qty. (2x) |
* ammeter |
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instruments |
* oil press. (2x) |
* voltmeter |
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* oil temp. (2x) |
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* coolant temp. (2x) |
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* coolant level |
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indicator (2x) |
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* gearbox temp. (2x) |
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* load (2x) |
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* prop. RPM (2x) |
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* fuel temp. left & |
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right tank |
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* fuel flow (2x) |
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* fuel px warning |
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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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Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
EASA |
Page 2 - 23 |
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Operating Limitations |
DA 42 NG AFM |
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for daytime |
in addition for |
in addition for |
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VFR flights |
night VFR flights |
IFR flights |
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Other |
* stall warning |
* Pitot heating |
* emergency battery |
operational |
system |
system |
(for backup attitude |
minimum |
* variable elevator |
* alternate static |
gyro and flood light) |
equipment |
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stop |
valve |
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* alternate means for |
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fuel quantity |
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indication (see |
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Section 7.9) |
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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.
Page 2 - 24 |
Rev. 1 |
18-Feb-2009 |
EASA |
Doc. No. 7.01.15-E |
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