DG Flugzeugbau DG-1001M Flight Manual page 14

Powerplant and powerplant controls:
 Retractable powerplant with liquid- cooled Solo 2 625 02 i two stroke
engine with electronic fuel injection and Composite propeller.
The engine is mounted flexibly to the propeller mast for vibration insulation.
Reduction gear with 5 high-tech V-belts.
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 during take-off and climb.
Battery ignition with normal and emergency system.
 Electrical engine extension-retraction, operated automatically with the
ignition switch or manually as back-up, electronic safety devices to avoid
incorrect operation.

Engine control instruments with digital LCD indication (Microprocessor
technology) DEI-NT including stall warning, outside air thermometer,
landing gear warning and canopy warning.
Technical data
Wingspan
Wing surface
Aspect ratio
Length
Fuselage height
Fuselage width
Horizontal tailplane span
Waterballast (optional)
Empty mass with basic instruments approx.*
Wing loading (with 80kg payload) approx.
Max. mass
Max. wing loading
Max. speed
Certified for aerobatics
Powerplant
Engine
Power
Reduction gear
Fuel tank capacity
Propeller
Propeller diameter
*Options will increase the empty mass accordingly!
Issued: October 2012
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Flight Manual DG-1000M
Solo 2 625 02 i two-cylinder-two-stroke-engine with
electronic fuel injection
BM-G1-160-R-120-1
TN1000/22
m / ft
m² / ft²
/
m / ft
m / ft
m / ft
m / ft
kg (l) / US.gal
kg / lbs
kg/m² / lbs/ft²
kg / lbs
kg/m² / lbs/ft²
km/h /kts
Category U, simple aerobatics approved
up to a max. mass of 683 kg /1506 lbs.
20 / 65.62
17.53 / 189
22.82
8.57 / 28.12
1.0 / 3.28
0.73 / 2.4
3.2 / 10.5
160 / 42.3
530 / 1168
34.8 / 7.13
790 / 1742
45 / 9.22
270 / 146
50 KW / 68 hp
approx. 1:2.8
40 Liter
Composite
1.6 m / 5.25
1.5