Airplane Flight Manual XA42
AFM-XA42-0040-002-A.01
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Chapter 05
24.01.2011
5.
PERFORMANCE
5.1
GENERAL
Performance data charts on the following pages are presented to facilitate the planning of flights in
detail and with reasonable accuracy under various conditions. The data in the charts have been
computed from actual flight tests with the aircraft and engine in good condition and using average
piloting techniques.
It should be noted that the performance information presented in the range and endurance charts
allow for 60 minutes reserve fuel at specified speeds. Some indeterminate variables such as engine
and propeller, air turbulence and others may account for variations as high as 10 % or more in range
and endurance. Therefore, it is important to utilize all available information to estimate the fuel
required for the particular flight.
5.1.1
PERFORMANCE CHARTS
Performance data are presented in tabular or graphical form to illustrate the effect of different
variables. Sufficiently detailed informations are provided in the tables so that conservative values can
be selected and used to determine the particular performance figure with reasonable accuracy.
All speeds in this chapter are indicated air speeds IAS except otherwise stated. The performance
figures below are given under following conditions:
• Maximum allowed weight 999 kg / 2200 lbs except otherwise stated
• Take-off and landing on concrete surface
• No wind
• Standard atmospheric condition
5.1.2
DEFINITION OF TERMS
For definition of terms, abbreviations and symbols refer to chapter 1.
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