Embraer EMB145, Operation Manual

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AIRPLANE
OPERATIONS
MANUAL
LIMITATIONS
EMB-145 EP FAA
REVISION 31
1-01-05
Page
5
Code
21
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, the design limits.
The takeoff weight (weight at brake release or at start of takeoff run) is
the lowest among MTOW and the following weights:
−
Maximum takeoff weight for altitude and temperature
determined from Maximum Takeoff Weight - Climb Limited
chart.
−
Maximum takeoff weight, as limited by (dry or wet) runway
length and determined from Maximum Takeoff Weight - Field
Length Limited chart (if applicable, determined from Takeoff
Distance on Contaminated Runway and Accelerate Stop
Distance on Contaminated Runway charts).
−
Maximum takeoff weight, as limited by brake energy and
determined from Maximum Takeoff Weight - Brake Energy
Limited chart.
−
Maximum takeoff weight, as limited by obstacle clearance,
enroute, and landing operating requirements.
The landing weight is the lowest among MLW and the following
weights:
−
Maximum approach and landing weight for altitude and
temperature determined from Maximum Landing Weight - Climb
Limited charts.
−
Maximum landing weight, as limited by (dry or wet) runway
length and determined from Maximum Landing Weight - Field
Length Limited chart (if applicable, determined from Landing
Distance on Contaminated Runway charts).
LOADING
The airplane must be loaded in accordance with the information
contained in the Weight and Balance Manual.