Sec. 25.1587 - Performance information.
(a) Each Airplane Flight Manual must
contain information to permit conversion of the indicated temperature to
free air temperature if other than a free air temperature indicator is
used to comply with the requirements of §25.1303(a)(1).
(b) Each Airplane Flight Manual must
contain the performance information computed under the applicable
provisions of this part (including §§25.115, 25.123, and 25.125 for the
weights, altitudes, temperatures, wind components, and runway gradients,
as applicable) within the operational limits of the airplane, and must
contain the following:
(1) In each case, the conditions of
power, configuration, and speeds, and the procedures for handling the
airplane and any system having a significant effect on the performance
(2) VSR determined in
accordance with §25.103.
(3) The following performance
information (determined by extrapolation and computed for the range of
weights between the maximum landing weight and the maximum takeoff
(i) Climb in the landing configuration.
(ii) Climb in the approach
(iii) Landing distance.
(4) Procedures established under
§25.101(f) and (g) that are related to the limitations and information
required by §25.1533 and by this paragraph (b) in the form of guidance
material, including any relevant limitations or information.
(5) An explanation of significant or
unusual flight or ground handling characteristics of the airplane.
(6) Corrections to indicated values of
airspeed, altitude, and outside air temperature.
(7) An explanation of operational
landing runway length factors included in the presentation of the landing
distance, if appropriate.
[Doc. No. 2000-8511, 66 FR 34024, June 26, 2001]