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FLIGHT DESIGN CTSW - Operating Limitations; Stalling Speeds; Flap Extended Speed Range; Maximum Maneuvering Speed

FLIGHT DESIGN CTSW
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Aircraft Type: CTSW
FLIGHT DESIGN
Aircraft Operating Instructions
Page: 4-1
AU 010 01000
Rev. No: 7
Original Issue Date: 28-Feb-2005
Revision Date: 29-Apr-2008
4 Operating Limitations
4.1 Stalling speeds at maximum takeoff weight (VS1 and VS0)
V
S0
: Stalling speed or the minimum steady flight speed in the landing configuration.
V
S1
: Stalling speed or the minimum steady flight speed obtained in a specific
configuration.
VS Flaps -6° (-12°) 44 KCAS (49 KCAS) 81 km/h CAS (90 km/h CAS)
VS1 Flaps 0° 42 KCAS 77 km/h CAS
VS0 Flaps 40° 39 KCAS 72 km/h CAS
4.2 Flap extended speed range (VS0 to VFE)
The White arc on the airspeed indicator is from VS0 to VFE, flaps 15°.
VFE: Maximum flap extended speed.
VFE: Flaps 100 KCAS 185 km/h CAS
15° 80 KCAS 148 km/h CAS
30° 62 KCAS 115 km/h CAS
40° 62 KCAS 115 km/h CAS
4.3 Maximum maneuvering speed (VA)
VA: Design maneuvering speed (above this speed only 1/3 of max. deflection may be
given, full or abrupt deflection of the control surfaces may cause structural failure).
LSA
registration
BFU / LTF-UL
registration
BCAR Section S
registration
USA Australia
km/h kts km/h kts km/h kts km/h kts
V
A
,
CAS
182 98 193 104 193 104 164 89

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