AIRPLANE
FLIGHT
LIMITATIONS
ANAC APPROVED 2-40
REVISION 6 code 09 Page 3
ENGINE THRUST
Operation at reduced takeoff thrust based on the assumed
temperature higher than the actual ambient temperature as calculated
by CAFM is permissible if the airplane meets all applicable
performance requirements at the planned takeoff weight and reduced
thrust setting. The total thrust reduction must not exceed 25% of the
full takeoff thrust. As a condition to the use of reduced thrust
procedures, operators must establish a means to ensure that the
engines are capable of producing full takeoff thrust without exceeding
any engine operating limits. Use of reduced takeoff thrust procedures
is not allowed on runways contaminated with standing water, slush,
snow, or ice, and are not allowed on wet runways unless suitable
performance accountability is made for the increased stopping
distance on the wet surface. Application of reduced takeoff thrust is
always at the pilot discretion. When conducting a takeoff using reduced
takeoff thrust, normal takeoff thrust may be selected at any time during
the takeoff operation.
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