DG Flugzeugbau DG-1000 Flight Manual page 14

Powerplant and powerplant controls

Retractable powerplant with air- cooled Solo 2350C two stroke engine and
CFRP-Composite propeller DG-P001-1

Electrical engine extension-retraction, operated automatically with the
ignition switch or manually as back-up, electronic safety devices to avoid
misoperation.

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
Span
Wing area
Aspect ratio
Length
Fuselage height
Fuselage width
Span of the horiz. tailplane
Waterballast Wings max.
Waterballast fin
Trim ballast fin
Empty mass with basic
instruments*
Wing loading (with one Pilot
80kg / 176 lbs)
max. take-off mass (max. TOW) kg / lbs
max. wing loading
Aerobatics
max. TOW for aerobatics
(cat. A)
max. speed
Powerplant
power
Reduction gear
Fuel tank capacity
Propeller
*Options will increase the empty mass accordingly!
Issued: February 2016
Flight manual DG-1000T
m / ft
m² / ft²
/
m / ft
m / ft
m / ft
m / ft
kg (l) / US.gal
max. kg (l)/ US.gal
max. kg / lbs
kg / lbs
approx.
kg/m² / lbs/ft²
approx.
kg/m² / lbs/ft²
kg / lbs
km/h /kts
Solo 2350C two-cylinder-two-stroke-engine
TN1000/25
17,2 18 / 59.1
16,3 16,72 / 180 17,53 / 189
18,15 19,38
8,57 / 28.12
1,0 / 3.28
0,73 / 2.4
3,2 / 10.5
160 / 42.3
6,2 / 1.64
12 / 26.5
457 / 1007 461 / 1016
32,9 / 6.75 32,4 / 6.64
750 / 1653 750 / 1653
46,0 / 9,4
unlimited
Category „A" Category „A"
630 / 1389
270 / 146
KW / hp
-
Liter / US.gal
DG-P001-1 CFRP-Composite
m / ft
20 / 65.62
22,82
465 / 1025
31,1 / 6.37
750 / 1653
44,9 / 9.2 42,8 / 8.77
unlimited simple
630 / 1389
270 / 146 270 / 146
22 / 30
1:2,3
22 / 5.81
1,48 / 4.86
1.5
/