DG Flugzeugbau DG-1000M Flughandbuch - Seite 5

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2.4 Power plant

Engine

manufacturer:

Engine

Maximum

power:

Max.

Max. cylinderhead (coolant) temperature:

Reduction gear (with 5 V-belts)

Caution: The engine is equipped with an emergency system which may be

activated via a switch in the front (and optionally in the rear) instrument panel in

case of a failure of the engine control unit (ECU). This system ensures

uninterrupted engine operation.

Note: The engine control (ECU) prevents exceeding an engine RPM of 6700 by

switching off the ignition. If you reduce the engine speed the ignition will be

activated again.

Note: The max. engine RPM given by the engine manufacturer is 6700 RPM.

This max. RPM is reduced for operation in the DG-1000M for not exceeding the

max. permissible RPM of the propeller.

Propeller:

Manufacturer:

Type /Variant:

2.5 Power plant instrument markings

(on DEI-NT, DEI=digital engine indicator)

Power plant instrument markings and their significance are shown below:

Engine speed indicator:

At the centre of the DEI-NT display, digital indication with 4 digits,

limitation data printed above display:

green

red

Max. continuous RPM:

No indication as identical with max. RPM.

Max. RPM:

When exceeding this RPM a full screen warning message "Engine

Speed" appears, when this warning has been confirmed (by pushing the

selector knob at the right hand side of the display) the engine speed display

is blinking whilst the engine speed is above max. RPM.

Issued: July 2014

Flight Manual DG-1000M

Solo Kleinmotoren

Sindelfingen/Maichingen

Germany

Solo 2 625 02 i, liquid cooled

two cylinder two stroke engine

Start:

Continuous:

Engine RPM:

Continuous RPM:

Diameter 1.6 m (5.25 ft)

Binder Flugzeug und Motorenbau GmbH

BM-G1-160-R-120-1

0-6600

6600

TN1000/23

50 KW / 68 PS (horse power)

50 KW / 68 PS

6600 1/min

105°C

approx. 1:2,8

normal operation range RPM

max. RPM

EASA app. 2.5