Sennheiser SI 234 - ANNEXE 802 Operations Instructions download pdf (Page 272)

Performance DA 42 NG AFM

Page 5 - 2 Rev. 3 01-Apr-2014 Doc. No. 7.01.16-E

5.1 INTRODUCTION

The performance tables and diagrams on the following pages are presented so that, on

the one hand, you can see what performance you can expect from your airplane, while

on the other hand they allow comprehensive and sufficiently accurate flight planning. The

values in the tables and the diagrams were obtained in the framework of the flight trials

using an airplane and power-plant in good condition, and corrected to the conditions of

the International Standard Atmosphere (ISA = 15 EC / 59 °F and 1013.25 hPa / 29.92 inHg

at sea level).

The performance diagrams and tables do not take into account variations in pilot

experience or a poorly maintained airplane. The performances given can be attained if

the procedures quoted in this manual are applied, and the airplane has been well

maintained.

5.2 USE OF THE PERFORMANCE TABLES AND DIAGRAMS

In order to illustrate the influence of a number of different variables, the performance data

is reproduced in the form of tables or diagrams. These contain sufficiently detailed

information so that conservative values can be selected and used for the determination

of adequate performance data for the planned flight.

For a conversion of units see Chapter 1.6 - UNITS OF MEASUREMENT.

For temperatures, altitudes and weights between those provided, use a linear interpolation

between the neighboring values.

For weights below 1700 kg (3748 lb), use data for the lowest weight.

For operation in outside air temperature lower than provided in these tables, use data

for lowest temperature shown.

Use extreme caution for operation at outside air temperature higher than provided in the

tables (areas are indicated with a diagonal line).'

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Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 272