PERFORMANCE
AIRPLANE
F
LIGHT
5-00 ANAC APPROVED
Page 2 code 01 REVISION 4
INTRODUCTION
The performance information given in this Section is applicable and
common to all EMBRAER 170 and EMBRAER 175 models. For
performance information related to the EMBRAER 170 or
EMBRAER 175 equipped with specific engine model, refer to the
Supplement 1 - CAFM.
The performance data are based on the following conditions:
− Pertinent power less installation, air bleed, and accessory
losses.
− Full temperature accountability within the operational limits for
which the airplane is certified.
− For landing, full brake application after touchdown.
The performance information is not valid if:
− The airplane’s gross weight exceeds the appropriate maximum
allowable limits.
− Any of the limitations in Section 2 is not observed.
− A reading from any graph is obtained by extrapolation (i.e. using
values of parameters outside the range given on the graph).
NOTE: In the case of headwind components, the airplane may be
operated in reported components greater than 30 kt, but the
effect of only 30 kt may be taken.
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