AIRPLANE
OPERATIONS
MANUAL
WEIGHT AND
BALANCE
REVISION 29
1-06-40
Page
13
Code
03
Forward Center of Gravity Limits:
AFM values Allow- Constrained values
Wt. CG arm Mom.
ance
Mom. arm CG
(lb) (%) (in) (lb.in) (lb.in) (lb.in) (in) (%)
Takeoff & Landing & In-flight limits:
25353 30.0 529.67 13428724 -10155 13438879 530.07 30.4
27558 15.0 512.75 14130365 -83802 14214167 515.79 17.7
31967 15.0 512.75 16391079 -83802 16474881 515.37 17.3
Takeoff & Landing limits:
35274 16.5 514.44 18146357 -69630 18215987 516.41 18.3*
44092 21.1 519.63 22911526 -69630 22981156 521.21 22.5*
In-flight limit:
35274 15.0 514.44 18146357 -83802 18230159 516.82 18.6
44092 18.9 519.63 22911526 -83802 22995328 521.53 22.8
* points disregarded because of the existence of more limiting points at
the same weight.
The table below shows the determination of the aft constrained limit for
the EMB-135LR model.
For Takeoff & Landing & In-flight limits the allowance used was:
• +150865.00 lb.in (aft flight allowance)
• + 71857.19 lb.in (aft seating allowance)
+222722.19 lb.in = total aft allowance
NOTE: The allowance at 25353 lb is zero because in this weight range
it is impossible to have passengers loaded, so the seating
allowance was disregarded and also the flight allowance.
Aft Center of Gravity Limits:
AFM values Allow- Constrained values
Wt. CG arm Mom.
ance
Mom. arm CG
(lb) (%) (in) (lb.in) (lb.in) (lb.in) (in) (%)
Takeoff & Landing & In-flight limits:
25353 30.0 529.67 13428724 0.0 13428724 529.67 30.0
26455 38.0 538.69 14251044 222722 14028322 530.27 30.5
35274 38.0 538.69 19001751 222722 18779029 532.38 32.4
44092 38.0 538.69 23751919 222722 23529197 533.64 33.5