Rans Inc. Section 4
Model S-7LS COURIER Performance
Original Issue March 3, 2005 4- 5
STALL SPEEDS
CONDITIONS:
Power Off
NOTES
1. Maximum altitude loss during a stall recovery may be as much as 160 feet.
2. IAS (MPH) Values are approximate.
3. All values are in MPH
4. Most forward center of gravity
At 1235 lb. At 1000 lb. Flap deflection
MPH IAS MPH CAS MPH IAS MPH CAS
UP 50 50 46 46
HALF 48 48 44 44
FULL 45 45 41 42
Table 4-4. Aircraft Stall speeds
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