Originally Posted by
randylervold
CC11s (Carbon Cub, Sport Cub) slip just fine with full flaps, and you can really get them to come down nicely in a full rudder slip.
I did that just this morning in my Sport Cub! For a nice, short approach from downwind abeam the numbers I just crank it all the way around 180 degrees in the slip, modulating the amount of slip as needed for the desired glide path. Fun!
I do notice a very mild "pitch pumping" in the stick in a slip with more than one notch of flap. This is probably from the vortex of the outboard end of the wing-down flap grazing the outboard end of the elevator. No biggie, it's just the airplane talking to me.
Some pilots believe slips with flaps are inherently bad, that they somehow "blank the tail". No and no. The grain of truth that gave rise to the mythology stems from the experiences of Cessna test pilots during development of the C-170 and C-172. Here's what former Cessna Manager of Aerodynamics and Flight Test William Thompson said in his book, Cessna - Wings for The World: The Single-Engine Development Story:
With the advent of the large slotted flaps in the C-170, C-180, and C-172 we encountered a nose down pitch in forward slips with the wing flaps deflected. In some cases it was severe enough to lift the pilot against his seat belt if he was slow in checking the motion. For this reason a caution note was placed in most of the owner’s manuals under “Landings” reading “Slips should be avoided with flap settings greater than 30 deg. due to a downward pitch encountered under certain combinations of airspeed, side-slip angle, and center of gravity loadings”. Since wing-low drift correction in crosswind landings is normally performed with a minimum flap setting (for better rudder control) this limitation did not apply to that maneuver. The cause of the pitching motion is the transition of a strong wing downwash over the tail in straight flight to a lessened downwash angle over part of the horizontal tail caused by the influence of a relative “upwash increment” from the upturned aileron in slipping flight. Although not stated in the owner’s manuals, we privately encouraged flight instructors to explore these effects at high altitude, and to pass on the information to their students. This phenomenon was elusive and sometimes hard to duplicate, but it was thought that a pilot should be aware of its existence and know how to counteract it if it occurs close to the ground.
I've never heard of the pitch-down phenomenon ever occurring in any airplane other than a C-172 earlier than 1972. The '72 Skyhawk introduced a larger dorsal fin that apparently solved the problem. The old C-172 owners manuals did say that slips with full flap were "prohibited," but the TCDS (which is the legal authority) only says "should be avoided."
But that does not apply to our Cubs, and as Randy says, slip away!