AAflyer
Well-known member
- Joined
- Nov 26, 2001
- Posts
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machaf said:Yes Vmc decreases as you climb. Less thrust, less yaw, less rudder = lower Vmc speed.
In a Seminole you will almost ALWAYS STALL before you lose directional control. Why? Because Vs is 57 and VMC is 56. The only way you will lose directional control before you stall is at high negative density altitude.
Remember VMC was determined in basically the worst possible airplane configuration.
Good point, many forget that as DA increases, VMC decreases, however I would not go so far to stand firm on the 56 knots. Remember that airspeed is subject to a host of factors;
AFT CG
MAX POWER
TO COWL FLAPS
TO FLAPS
GEAR RETRACTED
STANDARD ATMOSPHERIC DAY
OUT OF GROUND EFFECT
PROP WINDMILLING
BANK UPTO 3-5 DEGREES
1/2 BALL DEFLECTION
these items in different configurations can lead to more or less rudder effectiveness, basically changing the airspeed at which we can experience VMC.
AA