TBM
PILOT’S OPERATING HANDBOOK
700
SECTION 6
WEIGHT AND BALANCE
Page 6.4.10
Edition 1 -- November 30, 2010
Rev. 0
CG m.a.c.%
=
(do
−
172.93)
59.45
×
100
Use the above formula to express arm ”d
o
” in % of mean aerodynamic chord.
NOTE :
Arm expressed in inches with regard to reference.
Front seats
: 180.5 in. (4.585 m) } Valid S / N 1 to 23, 25,
Intermediate seats
: 219.1 in. (5.565 m) } 28, 33 and 35, except
Rear seats
: 259.3 in. (6.585 m) } airplanes equipped as
FWD cargo compart. : 128.0 in. (3.250 m) } a retrofit with
Aft bagg. compart.
: 297.6 in. (7.560 m) } modification
Fuel
: 189.8 in. (4.820 m) } Nr MOD 70--019--25
Front seats
: 180.5 in. (4.585 m) } Valid S / N 24, 26, 27,
Intermediate seats
: 222.1 in. (5.641 m) } 29 to 32, 34, 36 to 9999,
Rear divan (2 seats) : 272.3 in. (6.916 m) } plus airplanes equipped
FWD cargo compart. : 128.0 in. (3.250 m) } as a retrofit with
Aft bagg. compart.
: 303.0 in. (7.695 m) } modification
Fuel
: 189.8 in. (4.820 m) } Nr MOD 70--019--25
