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Ch-9 Weather TheoryV8-BAK_Basic Master Frame.qxd  12/19/2019  7:46 PM  Page 76







                 9-76               Rod Machado’s Instrument Pilot’s Handbook
                attitude change). Should you experience an uncommand-
                ed roll due to ice formation forward of the ailerons you
                should reduce the angle of attack and roll the wings level.
                If the flaps are extended don’t retract them unless you can
                determine  that  the  upper  wing’s  surface  is  free  of  ice.
                Retracting flaps in this instance raises the airplane’s stall
                speed (which is probably a bit higher because of ice accre-
                tion on the upper wing surface).
                Tailplane Icing
                  It’s one thing to have ice form on the wings where you
                have  a  chance  to  see  it  and  do  something  about  it.  It’s
                                                                                                                   Fig. 139
                another not to be able to see it because it’s on the tail (hor-
                izontal stabilizer, elevator, stabilator, or T-tail surface) of
                your  airplane  (Figure  137).  At  least  when  Burt  Rutan
                makes an airplane you can see the tail because he puts it
                out in front of the machine where you can keep an eye on
                it. So, why is tailplane (tail surface) icing so serious? Let’s
                find out.

                   Tailplane Icing is Difficult to Detect Visually















                                                           Fig. 137    tail closer to its critical angle of attack. The result of this
                                                                       configuration is that actions that move the wing away from
                  Downward Lift: What? Isn’t Lift                      stall,  such  as  deployment  of  flaps  or  increasing  speed,
                  Supposed to Act Upward?                              might move the tail toward its critical angle of attack, pos-
                  Most airplanes have a nose-down pitching moment gen-  sibly resulting in a tailplane (or tail) stall (Figure 139). The
                erated by the center of gravity (CG) being ahead of the  disadvantage here is that a tailplane stall typically would
                wing’s center of lift (Figure 138). It is the role of the tail  occur during approach and landing—a time when the air-
                surface to counteract this moment by providing lift that  plane has less altitude to recover from a stall.
                acts in a downward direction. Unfortunately, this arrange-  Tailplane Stall: What? Another Part
                ment often allows an application of flaps (as an intention-  Of the Airplane That Can Stall?
                al move to reduce the airplane’s stall speed) to increase  As  an  airplane’s  tail  surface  (also  called  tailplane)  is
                the negative angle of attack (AOA) on the tail. In other  ordinarily thinner than the wing, it is a more efficient col-
                words, the application of flaps might require slight aft ele-  lector of ice. Because it’s often not possible to observe the
                vator  pressure  (creating  more  downward-acting  lift)  to  tail surface and see how well it is cleared of ice by any de-
                maintain  the  desired  attitude.  Aft  elevator  pressure  icing  system,  you  must  be  alert  to  the  possibility  of  a
                increases the AOA (in the negative direction), moving the  tailplane stall, particularly after full flap deflection. This













                                                                  Fig. 138
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