Tesla TI4676, Руководство пользователя

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CHAPTER 5
PERFORMANCE DATA
SECTION 1. INTRODUCTION
5-1. PURPOSE
This chapter provides performance data for the TI4676. Continual refer-
ence to this information will enable the user to obtain maximum perfor-
mance, utilization and service life from the TI4676. Although maximum
performance is not always required, regular referral to this chapter is
recommended for the following reasons:
a. To generate knowledge of unit’s performance margins to enable the
operator to make sound judgment when unexpected conditions or alter-
nate operational requirements are encountered.
b. To enable the user to readily recognize situations requiring
maximum performance.
c. To gain experience in accurately estimating the effects of vari-
ables for which data is not presented.
d. To help the operator determine if an aircraft system malfunction
exists by comparing actual performance with expected performance.
NOTE
The information provided in this chapter is primarily intended for op-
erational planning and is most useful when planning operations under
unfamiliar conditions or environmental extremes. The data may also be
used to establish local operating procedures and to ensure unit’s opera-
tional life is maximized.
5-2. GENERAL
The data presented covers the maximum range of conditions and perfor-
mance that can reasonably be expected. In each area of performance, the
effects of temperature and DC electrical load demand relating to the
ground power support requirements are presented. Wherever practical,
data is presented conservatively. However, NO GENERAL CONSERVATISM HAS
BEEN APPLIED. All performance data presented is within the applicable
limits of the TI4676 MPU.
5-1