AIRPLANE
FLIGHT
MANUAL
LIMITATIONS
ANAC APPROVED 2-05
REVISION 7 code 20 Page 1
AFM-1385
WEIGHT
AIRPLANE
MODEL
MAX
Ramp
Weight
(MRW)
(lb)
MAX
Takeoff
Weight
(MTOW)
(lb)
MAX
Landing
Weight
(MLW)
(lb)
MAX
Zero Fuel
Weight
(MZFW)
(lb)
EMBRAER 175-STD (1)
EMBRAER 175-SU (1)
EMBRAER 175-LR (1)
89352 89000 75177 70547
NOTE: (1) For airplanes Post-Mod. SB 170-00-0016 or equipped with
an equivalent modification factory incorporated.
To comply with the performance and operating limitations of the
regulations, the maximum allowable takeoff and landing operational
weights may be equal to, but not greater than design limits.
The takeoff weight (weight at brake release or at start of takeoff run) is
the lowest between MTOW and the following weights:
− Maximum takeoff weight as calculated using the approved
software, and as limited by field length, climb and brake energy.
− Maximum takeoff weight, as limited by enroute, and landing
operating requirements.
The landing weight is the lowest among MLW and the following
weights calculated using the approved software:
− Maximum landing weight as limited by runway.
− Maximum approach and landing weight as limited by altitude,
temperature and climb gradient.
LOADING
The airplane must be loaded in accordance with the information
contained in the Weight and Balance Manual.
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