JS-MD 3
Aircraft Flight Manual
MD10-AFM-00-001
Issue: 01
Rev. 00
Rev. Date: 14-Feb-20
Page 2
–9
Table 2.6-2 gives the forward and rear CG limits (no payload) for different
empty masses that will allow a cockpit range of 70 kg to 115 kg.
Empty mass
Empty Centre of Gravity range
Forward limit
To allow a maximum
cockpit load of 115 kg
(253 lbs)
Rear limit
To allow a minimum
cockpit load of 70 kg
(154 lbs)
Kg
lbs
15 m
18 m
15 m
18 m
260
573
675
mm
675
mm
669
mm
679
mm
26.6
in
26.6
in
26.3
in
26.7
in
270
596
660
mm
660
mm
660
mm
668
mm
26.0
in
26.0
in
26.0
in
26.3
in
280
618
646
mm
646
mm
649
mm
659
mm
25.4
in
25.4
in
25.5
in
25.9
in
290
640
637
mm
633
mm
640
mm
650
mm
25.1
in
24.9
in
25.2
in
25.6
in
300
662
630
mm
626
mm
632
mm
641
mm
24.8
in
24.6
in
24.9
in
25.3
in
310
684
623
mm
619
mm
624
mm
634
mm
24.5
in
24.4
in
24.6
in
24.9
in
320
706
616
mm
612
mm
616
mm
626
mm
24.3
in
24.1
in
24.3
in
24.7
in
Table 2.6-2 Empty Centre of Gravity range
If the calculated empty CG falls outside of this envelope, the minimum
and maximum cockpit loads must be determined using the formula given
in the JS-MD 3 Aircraft Maintenance Manual 08-10-00.
