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5.   PERFORMANCE

5.1   Introduction

5.2   Approved data

5.2.1   Airspeed indicator system calibration

5.2.2   Stall speeds

5.2.3   Take-off performance

5.2.4   Landing distances

5.2.5   Climb performance

5.3   Additional information

5.3.1   Cruise

5.3.2   Endurance

5.3.3   Balked landing climb

5.3.4   Effect on flight performance and characteristics

5.3.5   Demonstrated crosswind performance

5.3.6   Ceiling

5.3.7   Noise data

5.1  Introduction

Section 5 provides approved data for airspeed calibration, stall speeds, take-off performance and non-approved additional information.

The data in the charts has been computed from actual flight tests with the aircraft and engine in good conditions and using average piloting techniques.

If not stated otherwise, the performance stated in this section is valid for the max. take-off weight and flight under ISA conditions.

The performance given in this section is valid for aircraft with given engine and propeller types.

5.2  Approved data

5.2.1 Airspeed indicator system calibration

5.2.2 Stall Speeds

5.2.3 Take-off performance

Take-off distances stated in the following table are valid at sea level and ambient temperature of 15 °C ( 59 °F ).

 

5-2-4 Landing distance

Landing distances stated in the following table are valid at sea level and ambient temperature of 15 °C ( 59 °F ).

5.2.5 Climb performance

(1m/s = approx 200 ft/min; 115 km/tim = 62 kts)

5.3  Additional information

5.3.1 Cruise

Horizontal speeds

In the following tables state indicated airspeeds (IAS) and corresponding True air speeds (TAS) versus altitude, all for various engine speeds.

5.3.2 Endurance

The following table states fuel consumptions, endurances and ranges for appropriate regimes.

5.3.3 Balked landing climb

Not measured

5.3.4 Effect on flight performance and characteristics

Flight performance and characteristics are not substantially affected by rain or accumulation of insects on the aeroplane surface.

 

5.3.5 Demonstrated crosswind performance

Max. permitted cross wind velocity
for take-off and landing   ................................. 5   m/s    10   kts

Max. permitted head wind velocity
for take-off and landing   .............................. 12   m/s    23    kts

 

5.3.6 Ceiling

Service ceiling   .......................................... 5000   m    16500   ft

 

5.3.7 Noise data

64.4 dB(A) - with Rotax 912 UL (80 hp) and V 230C prop

59.4 dB(A) - with Rotax 912 UL (80 hp) and Fiti Eco Competition prop

58.3 dB(A) - with Rotax 912 ULS (100 hp) and SR 2000 prop

59.2 db(A) - with Rotax 912 ULS (100 hp) and Klassic 170/3/R prop

59.1 db(A) - with Rotax 912 ULS (100 hp) and Varia 170/2/R prop

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