Sennheiser SI 234 - ANNEXE 802 Operations Instructions download pdf (Page 150)

100

101

Emergency

Procedures

DA 42 NG AFM

Page 3 - 66 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E

(b) Propeller Overspeed

NOTE

This procedure applies for continued propeller overspeed due

to a malfunction in the propeller constant speed unit or a

engine control unit malfunction.

1. POWER setting....................... reduce as required

If the problem does not clear:

2. Garmin G1000 ....................... check L/R ECU A/B FAIL caution

If L/R ECU A FAIL indicated:

3. VOTER switch........................ ECU B

If L/R ECU B FAIL indicated:

3. VOTER switch........................ ECU A

CAUTION

If the problem does not clear itself, switch back to AUTO and

land on the nearest suitable airfield. Prepare for engine

malfunction according to 3.7.6 - ENGINE FAILURES IN

FLIGHT.

CONTINUED

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Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 150

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