Weighing Report (For Section 6.3); Empty Weight C.g. Limits (For 6.4) - DG Flugzeugbau DG-1000S Flight Manual

Flight manual DG-1000S
6.8.8

Weighing report (for section 6.3)

Distances in mm, masses in kg -- 25.4 mm = 1 inch / 1 kg = 2.2046 lbs.
Date of weighing:
Executed by:
Date of equipment
list:
wing span 18m 20m
Empty mass
Empty mass C.G.
Max. mass without
W.B. Cat. U
Cat. A 630 /
Max. load without
W.B. Cat. U
Cat. A
max. mass with
WB
max. useful load
with W.B.
min. cockpit load
YY (kg)
min. cockpit load
XX (kg)
max. load in both 210 210
seats
Inspector,
signature, stamp
YY= min. load in front seat for solo flying with fin ballast box empty.
XX= YY+40= min. load in front seat for solo flying with fin ballast box filled.
Weighing was executed with: battery in the fin Z110
tailwheel with:
Issued: March 2002
plastic hub
brass hub (see section 7.15.4)
6.7
Flight manual DG-1000S
6.8.9

Empty weight C.G. limits (for 6.4)

x mm
S
820,0
815,0
810,0
805,0
800,0
795,0
790,0
785,0
780,0
775,0
770,0
765,0
760,0
755,0
750,0
745,0
740,0
735,0
730,0
725,0
720,0
715,0
710,0
705,0
700,0
695,0
690,0
685,0
680,0
675,0
670,0
665,0
660,0
655,0
650,0
645,0
640,0
415 420 425 430 435 440 445 450
Issued: March 2002
Load front
seat
65 kg
70 kg
75 kg
80 kg
85 kg
xSV
Aft C.G.
limits
Front C.G.
limits
Empty mass
455 460 465 470 475 480
kg
6.8