TEST: Determining Appropriate Airspeeds for Emergency Operation
V_a
PROCEDURE:

1. Determine your stall speed
2. V_a is defined as the stall speed of the wing at max gross weight x limiting load factor. A Falcon XP is designed for operation within the normal category weight/C.G. limits. Therefore, a Falcon XP is designed for a max load factor of 4.4g's.
3. Load factor can be calculated as...:

   LF = V_a² / V_s²

4. Therefore, for the Falcon XP, V_a = square root (V_s² x 4.4)
5. V_a:____________________

V_{best glide}
PROCEDURE:

V_{min. sink}
PROCEDURE: