EVEKTOR-AEROTECHNIK Harmony LSA, Руководство по эксплуатации

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AIRCRAFT OPERATING INSTRUCTIONS
Doc. No. HARMAOIUS
June 01, 2011
5-5
Section 5
Performance
5.2.2 Stall speeds
Conditions:
-
wing level stall - engine at idle power
-
turning flight stall - engine at 75% max. continuous power
-
airplane weight: 1320 lbs (600 kg)
-
Vortex generators along the whole span of the wing
NOTE
The stated stall speeds are valid for all flight altitudes.
Altitude losses shown in the table present max. values
determined on the basis of flight tests using average
piloting technique.
600 kg Flaps Altitude loss
1320 lbs position IAS [km/h] CAS [km/h] [ft]
Retracted (0°)
63 83
Take-off (15°)
61 82
Landing (50°)
60 75 200
Retracted (0°)
72 91
Take-off (15°)
70 88
Landing (50°)
70 84
Stall speed
Wing level flight
Turn flight (coordinated
turn 30° bank)
1320 lbs Flaps Altitude loss
600 kg position KIAS KCAS [ft]
Retracted (0°)
34 45
Take-off (15°)
33 44
Landing (50°)
33 40 200
Retracted (0°)
39 49
Take-off (15°)
38 48
Landing (50°)
38 45
Wing level flight
Turn flight (coordinated
turn 30° bank)
Stall speed
1320 lbs Flaps Altitude loss
600 kg position IAS (mph) CAS (mph) [ft]
Retracted (0°)
39 52
Take-off (15°)
38 51
Landing (50°)
38 46 200
Retracted (0°)
45 56
Take-off (15°)
44 55
Landing (50°)
43 52
Turn flight (coordinated
turn 30° bank)
Stall speed
Wing level flight