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Emergency

DA 40 NG AFM

Procedures

3.4 FAILURES IN THE ELECTRICAL SYSTEM

3.4.1 COMPLETE FAILURE OF THE ELECTRICAL SYSTEM

1. Circuit breakers . . . . . . . . . . . . . . . . . . . . . . check IN

2. ESSENTIAL BUS . . . . . . . . . . . . . . . . . . . . . ON

If There Is Still No Electrical Power Available:

% 2. EMERGENCY switch (if installed) . . . . . . . . ON 3. Flood light, if necessary . . . . . . . . . . . . . . . . ON

4. POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . set based on lever positions and engine noise

5.Prepare landing with flaps in the given position. Refer to 4B.5 - FAILURES IN FLAP OPERATING SYSTEM.

6.Land on the nearest suitable airfield.

WARNING

Engine stoppage may occur, depending on the failure mode.

A backup battery is installed for the ECU to provide electrical power solely to ECU B and its system for at least 30 minutes.

NOTE

The backup artificial horizon and the flood light will have electrical power for at least 1.5 hours.

%If G1000 is installed 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

Page 3 - 30

Rev. 1

15-Mar-2011

Doc. # 6.01.15-E

 

 

 

 

DA 40 NG AFM

Emergency

Procedures

3.4.2 HIGH CURRENT

% If HIGH CURRENT (> 70 A) is indicated on the G1000 (if installed) or SED (if installed):

1. ESSENTIAL BUS . . . . . . . . . . . . . . . . . . . . . ON

%2. ENGINE SYSTEM DISPLAY

%

(if G1000 is installed) . . . . . . . . . . . . . . . . . .

select by pressing ENGINE and

%

 

SYSTEM softkey on MFD

3.

Circuit breakers . . . . . . . . . . . . . . . . . . . . . .

check IN

% 4.

Ammeter/Voltmeter . . . . . . . . . . . . . . . . . . .

monitor

5.

Land on the nearest suitable airfield.

 

END OF CHECKLIST

Doc. # 6.01.15-E

Rev. 1

15-Mar-2011

Page 3 - 31

 

 

 

 

Emergency

DA 40 NG AFM

Procedures

3.4.3 STARTER MALFUNCTION

If the starter does not disengage from the engine after starting (Starter engaged warning

%(STARTER) on the G1000 (if installed) or START on the White Wire annunciator (if

%installed) illuminates after the engine has started):

On Ground:

1. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . IDLE

2. ENGINE MASTER . . . . . . . . . . . . . . . . . . . . OFF

3. ELECTRIC MASTER . . . . . . . . . . . . . . . . . . OFF

Terminate flight preparation!

In Flight:

Land as soon as possible.

END OF CHECKLIST

Page 3 - 32

Rev. 1

15-Mar-2011

Doc. # 6.01.15-E

 

 

 

 

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