DG Flugzeugbau DG-1001M Flight Manual page 97

If the actual pilot C.G. is not known, you have to take the values from the
following table:
flight: v = near the forward C.G.
h = near the aft C.G.
Pilot mass
[kg] (lbs.) [m]
110 243 -1.388 -54.65 -1.335 -52.56 -0.317 -12.48 -0.272 -10.71
105 231 -1.390 -54.72 -1.336 -52.60 -0.318 -12.52 -0.273 -10.75
100 220 -1.391 -54.76 -1.337 -52.64 -0.319 -12.56 -0.274 -10.79
95 209 -1.392 -54.80 -1.338 -52.68 -0.320 -12.60 -0.275 -10.83
90 198 -1.393 -54.84 -1.340 -52.76 -0.321 -12.64 -0.276 -10.87
85 187 -1.395 -54.92 -1.341 -52.80 -0.323 -12.72 -0.277 -10.91
80 176 -1.396 -54.96 -1.342 -52.83 -0.324 -12.76 -0.278 -10.94
75 165 -1.397 -55.00 -1.343 -52.87 -0.325 -12.80 -0.279 -10.98
70 154 -1.399 -55.08 -1.344 -52.91 -0.326 -12.83 -0.280 -11.02
65 143 -1.400 -55.12 -1.345 -52.95 -0.328 -12.91 -0.281 -11.06
60 132 -1.401 -55.16 -1.346 -52.99 -0.329 -12.95 -0.282 -11.10
55 121 -1.402 -55.20 -1.347 -53.03 -0.330 -12.99 -0.283 -11.14
Further C.G. positions:
Item
Baggage and battery in baggage compartment
Water ballst in the wings
Ballast box in the fin (see section 6.8.7)
Instruments in front panel
Instruments in rear panel
Removable ballast (in front cockpit, Option, see section 7.17.1) -1.960 -77.17
Battery in fin (Option see section 6.8.4)
Powerplant (see section 4.6)
Fuel tank
C.G. Shift due to extension of the engine
XS2 = XS1 – 3.8/W
Issued: October 2012
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Flight Manual DG-1000M
Pilot C.G. lever arm
Front cockpit
v h
[in.] [m]
W = total mass (kg)
XS2 = C.G. position with engine extended (m)
XS1 = C.G. position with engine retracted (m)
TN1000/22
Rear cockpit
v
[in.] [m] [in.]
h
[m] [in.]
C.G. positions
m in.
0.270 10.63
0.206 8.11
5.400 212.60
-1.910 -75.20
-0.740 -29.13
5.340 210.24
1.261 49.65
0.425 16.73
6.15