Embraer 175 - Maximum Takeoff Weight - Mtow; Climb Limited Takeoff Weight (or Takeoff Wat); Landing Weight - Lw; Maximum Landing Weight - Mlw

AIRPLANE
FLIGHT
MANUAL
PERFORMANCE
ANAC APPROVED 5-01
REVISION 6 code 01 Page 13
AFM
-
1385
MAXIMUM TAKEOFF WEIGHT - MTOW
It is the maximum structural takeoff weight.
CLIMB LIMITED TAKEOFF WEIGHT (OR TAKEOFF WAT)
It is the maximum allowed takeoff weight for the airport altitude and
temperature, and complying with the takeoff and go-around climb
gradient requirements.
V
1
DEPENDENT TAKEOFF WEIGHT
It is the takeoff weight affected by V
1
selection. The V
1
dependent
takeoff weights are those limited by field length (TOD/OEI, ASD/OEI,
ASD/AEO), brake energy and obstacle clearance. The non-V
1
dependent takeoff weights are those limited by TOD/AEO, climb
gradients, tire speed and structure.
LANDING WEIGHT - LW
It is the gross weight of the airplane at the landing screen height.
MAXIMUM LANDING WEIGHT - MLW
It is the maximum structural landing weight.
CLIMB LIMITED LANDING WEIGHT (OR LANDING WAT)
It is the maximum allowed landing weight for the airport altitude and
temperature, and complying with the go-around climb gradient
requirements, either for AEO or OEI conditions.
REGULATED LANDING WEIGHT - RLW
It is the maximum allowed landing weight, derived by complying with all
requirements, such as those related to field length, climb gradients,
brake energy, tire speed, and structure.
MINIMUM LANDING WEIGHT
It is the minimum allowed landing weight, derived by complying with
steep approach requirements, based on the airplane approach glide
capability.