CS 25.1587 Performance information
ED
Decision 2018/005/R
(a) Each aeroplane 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 CS 25.1303(a)(1).
(b) Each aeroplane Flight Manual must contain
the performance information computed under the applicable provisions of this
CS-25 (including CS 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 aeroplane, and must contain the following:
(1) In each case, the conditions of power,
configuration, and speeds, and the procedures for handling the aeroplane and
any system having a significant effect on the performance information.
(2) VSR determined in accordance
with CS 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 weight):
(i) Climb in the landing configuration.
(ii) Climb in the approach configuration.
(iii) Landing distance.
(4) Procedures established under CS 25.101(f) and (g) that are related to the limitations and information required by CS 25.1533
and by this paragraph in the form of guidance material including any relevant
limitation or information.
(5) An explanation of significant or unusual
flight or ground handling characteristics of the aeroplane.
(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.
c) Each aeroplane flight manual (AFM) must
contain the performance information associated with abnormal landing
configurations (see AMC 25.1587(c)).
[Amdt
25/21]
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