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FLIGHT DESIGN CTSW - Never Exceed Speed (VNE); Wind Limitations; Load Factors

FLIGHT DESIGN CTSW
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Aircraft Type: CTSW
FLIGHT DESIGN
Aircraft Operating Instructions
Page: 4-2
AU 010 01000
Rev. No: 7
Original Issue Date: 28-Feb-2005
Revision Date: 29-Apr-2008
4.4
Never exceed speed (VNE)
VNE: Never-exceed speed.
LSA
registration
USA Australia
km/h kts km/h kts
V
NE
,
CAS
268
2
145
2
301
1
/296
2
163
1
/159
2
BFU / LTF-UL
registration
km/h kts
V
NE
,
CAS
276
3
150
3
BCAR Section S
registration
km/h kts
V
NE
,
CAS
280 151
1 - Without rescue system;
2 - With BRS 1350 HS.
3 - With BRS 1050.
4.5 Crosswind and wind limitations
The maximum demonstrated crosswind is 30 km/h / 16 knots.
CAUTION!
Due to the light operating weights and low minimum flight speeds of
Light Sport Aircraft, operations with surface winds in excess of 46 km/h /
25 kts should not be attempted.
4.6 Service Ceiling
The Service Ceiling is the maximum altitude at which a climb rate of 100 ft/min /
30 m/min can be achieved. For the CTSW it is 4,250 m / 14,000 feet.
Note: An aircraft must be properly equipped and the pilot appropriately certificated for
operations above 10,000 feet / 3,000 m.
4.7 Load factors
The maximum maneuvering limit load factor is: + 4 g / -2 g Flaps up
+ 2 g / -0 g Flaps down

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