Добавил:
Опубликованный материал нарушает ваши авторские права? Сообщите нам.
Вуз: Предмет: Файл:
1 курс / РЛЭ / РЛЭ DA40 NG (англ).pdf
Скачиваний:
6
Добавлен:
18.09.2024
Размер:
2.77 Mб
Скачать

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. 3

01-Jul-2014

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. 3

01-Jul-2014

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. 3

01-Jul-2014

Doc. # 6.01.15-E

 

 

 

 

Соседние файлы в папке РЛЭ