Emergency
DA 42 NG AFM
Procedures
Make use of the stand-by airspeed indicator and altimeter. Engine power can be set via visual reference of the POWER lever position.
END OF CHECKLIST
3.9.2 HIGH CURRENT
If high current is indicated on the G1000:
1.Circuit breakers . . . . . . . . . . . . . . . . . . . . . . . check
2.Reduce electric load to minimum required for continued safe flight.
3.Land on the nearest suitable airfield.
END OF CHECKLIST
3.9.3 STARTER MALFUNCTION
If the starter does not disengage from the engine after starting (starter engaged warning (STARTER L/R) on the G1000 annunciator field illuminates after the engine has started):
On Ground:
1.POWER lever affected engine . . . . . . . . . . . IDLE
2.ENGINE MASTER affected engine . . . . . . . . OFF
3.ELECT. MASTER . . . . . . . . . . . . . . . . . . . . . OFF
Terminate flight preparation.
In flight:
Terminate flight.
END OF CHECKLIST
Page 3 - 52 |
Rev. 1 |
18-Feb-2009 |
Doc. No. 7.01.15-E |
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DA 42 NG AFM
Emergency
Procedures
3.10 SMOKE AND FIRE
NOTE
The cabin hand fire extinguisher is located inside the airplane passenger compartment on the RH side of the cabin floor behind the co-pilot seat.
To release the fire extinguisher bottle out of the bracket, it is necessary to catch the bottle at the agent-outlet nozzle near the Y-spring.
3.10.1 ENGINE FIRE ON GROUND |
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1. |
ENGINE MASTER . . . . . . . . . . . . . . . . . . . . |
both OFF |
2. |
FUEL SELECTOR . . . . . . . . . . . . . . . . . . . . |
both OFF |
3. |
ELECT. MASTER . . . . . . . . . . . . . . . . . . . . . |
OFF |
after standstill: |
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4. |
Canopy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
open |
5. |
Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
evacuate immediately |
END OF CHECKLIST
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
Page 3 - 53 |
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Emergency
DA 42 NG AFM
Procedures
3.10.2 ENGINE FIRE DURING TAKE-OFF
1. Cabin heat & Defrost . . . . . . . . . . . . . . . . . . . OFF
CAUTION
In case of extreme smoke development, the front canopy may be unlatched during flight. This allows it to partially open, in order to improve ventilation. The canopy will remain open in this position. Flight characteristics will not be affected significantly.
Proceed according to 3.7.5 - ENGINE FAILURES DURING TAKE-OFF.
END OF CHECKLIST
Page 3 - 54 |
Rev. 1 |
18-Feb-2009 |
Doc. No. 7.01.15-E |
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DA 42 NG AFM
Emergency
Procedures
3.10.3 ENGINE FIRE IN FLIGHT
1. Cabin heat & Defrost . . . . . . . . . . . . . . . . . . |
OFF |
CAUTION
In case of extreme smoke development, the front canopy may be unlatched during flight. This allows it to partially open, in order to improve ventilation. The canopy will remain open in this position. Flight characteristics will not be affected significantly.
Proceed according to 3.7.6 - ENGINE FAILURES IN FLIGHT and shut down the engine according to 3.7.3 - ENGINE SECURING (FEATHERING) PROCEDURE.
END OF CHECKLIST
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
Page 3 - 55 |
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Emergency
DA 42 NG AFM
Procedures
3.10.4 ELECTRICAL FIRE ON GROUND
1. ELECT. MASTER . . . . . . . . . . . . . . . . . . . . . |
OFF |
If the engine is running:
2. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . both IDLE
3. ENGINE MASTER . . . . . . . . . . . . . . . . . . . . both OFF
4. FUEL SELECTOR . . . . . . . . . . . . . . . . . . . . . both OFF
When the engine has stopped / after standstill:
5. |
Canopy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
open |
6. |
Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
evacuate immediately |
END OF CHECKLIST
Page 3 - 56 |
Rev. 1 |
18-Feb-2009 |
Doc. No. 7.01.15-E |
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DA 42 NG AFM
Emergency
Procedures
3.10.5 ELECTRICAL FIRE IN FLIGHT
1. EMERGENCY SWITCH . . . . . . . . . . . . . . . . ON
2. AVIONIC MASTER . . . . . . . . . . . . . . . . . . . . OFF
3. ELECT. MASTER . . . . . . . . . . . . . . . . . . . . . OFF 4. Cabin heat & Defrost . . . . . . . . . . . . . . . . . . OFF
5. Emergency windows . . . . . . . . . . . . . . . . . . . open if required
6. Land at the next suitable airfield
CAUTION
Switching OFF the ELECT. MASTER will lead to total failure of all electronic and electric equipment. The attitude and heading reference system (AHRS) will also be affected.
However, by switching the EMERGENCY switch ON, the emergency battery will supply power to the standby attitude gyro (artificial horizon) and the flood light.
In case of extreme smoke development, the front canopy may be unlatched during flight. This allows it to be partially opened, in order to improve ventilation. The canopy will remain open in this position. Flight characteristics will not be affected significantly.
The maximum demonstrated airspeed for emergency opening the front canopy in flight is 117 KIAS. Do not exceed 117 KIAS.
END OF CHECKLIST
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
Page 3 - 57 |
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