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5.3.12 GRADIENT OF CLIMB ON GO-AROUND .............5-34
5.3.13 APPROVED NOISE DATA .........................5-35
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 5 - 1
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 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 1,013.25 hPa / 29.92 inHg at sea level).
The performance diagrams 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.
5.3 PERFORMANCE TABLES AND DIAGRAMS
5.3.1 AIRSPEED CALIBRATION
NOTE
The position of the landing gear (extended/retracted) has no influence on the airspeed indicator system.
5.3.2 FUEL FLOW DIAGRAM CAUTION
The diagram shows the fuel flow per hour for one engine.
NOTE
The fuel calculations on the FUEL CALC portion of the G1000 MFD do not use the airplane's fuel quantity indicators. The values shown are numbers which are calculated from the last fuel quantity update done by the pilot and actual fuel flow data. Therefore, the endurance and range data is for information only, and must not be used for flight planning.
5.3.3 INTERNATIONAL STANDARD ATMOSPHERE
5.3.4 STALLING SPEEDS
CAUTION
The calculated stalling speeds may be higher than the maximum approved / limiting flap-extended and / or maneuvering airspeeds.
Stalling speeds at various flight masses
Airspeeds in KIAS at idle power:
1400 kg (3086 lb) Bank Angle
Gear Flaps 0° 30° 45° 60°
UP UP 56 60 68 83
DOWN APP 53 58 65 78
DOWN LDG 49 53 61 75
1700 kg (3748 lb) Bank Angle
Gear Flaps 0° 30° 45° 60°
UP UP 62 67 76 92
DOWN APP 59 64 72 87
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