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          Barry Meek 

Newsletter February 2018.

Previous Newsletter January  2018

Next meeting Thursday, February 8.

7:30pm, Blair Field Clubhouse.

By Dan Thomas

Angle of Attack (part 2)

Last month I wrote a little about Angle of Attack, or AoA as we’ll call it. As I said, it’s an often misunderstood or completely ignored aspect of flying, and that lack of knowledge causes innumerable loss-of-control accidents. This month we’ll expand on the subject somewhat, using pictures. After all, most of us see a lot better than we hear or read.

Around ten years ago, while a Director of Aircraft Maintenance at a college-based flight school, I also did some flight instructing and taught a course on Aircraft Systems. I found that visualizing AoA was difficult for many students, so I came up with this thing, building it out of steel rod and flat bar and some plywood, and using one of the models we made for the instructors while they were briefing the students.


The rods represent the relative wind. The nearest set represents a steep turn. The middle set represents level, climbing or descending flight, and the farthest combines the two for climbing or descending turns. Some interesting geometry appears once we place the model on those rods.


We’ll start with the level cruise flight. The airspeed is high, so the angle of attack is relatively low. Safe enough. Remember, lift is a function of airspeed and angle of attack: if speed is low, you need more AoA. Speed high, less AoA.


Note the low AOA, signifying a good speed.

All the angles on this AoA table are exaggerated to make understanding easier, and the turn radii are much smaller so that AoA differentials show up clearly. We don’t really want to descend at the angle shown above.


Low speed descent. The AoA is large, to make up for the low airspeed and still generate 1G of lift for the airplane. The sink rate will tend to be high due to the large AOA and the induced drag that goes with it. This can be used instead of slipping to descend more quickly in flapless airplanes, but speed control is critical since it will be low and can fall further quickly. My own Jodel will sink at truly alarming rates if I slow it up when high on approach and can leave insufficient airspeed for flaring.

And this points out two common mistakes pilots make: (1) Diving at the runway when too high increases airspeed, decreases AoA and therefore drag, and the airplane arrives in ground effect with far too much speed and several types of accidents can happen. (2) Pulling the nose up to stretch the glide doesn’t work. It increases AoA, reduces speed, and you actually fall short of your intended spot.

Several lessons can be drawn from this one. With the nose high and the airplane travelling in a level flight path, we have here either slow flight (where the low speed demands lots of AoA), or we’re on the edge of a stall (which is what slow flight is, anyway), or the pilot has pulled up real hard in an attempt to get that spectacular zoom. Let’s address the last scenario: the zoom. Remember Newton’s First Law of motion? “An object in motion stays in motion with the same speed and in the same direction unless acted upon by an unbalanced force.” This airplane, because it has mass, wants to keep going straight ahead, and if we want it to climb, the wing has to provide extra lift. If the change in direction takes some time, the wing has more time to do it, and therefore the extra load is less. If we pull up suddenly, we need a lot of extra lift and we feel significant G force as we do it. If we pull just a bit too hard, however, we can get what’s called an “accelerated stall,” and stall that wing and crash the airplane if we did it at low level. Aerobatic pilots do snap rolls by pulling back hard and stomping the rudder; in effect, they’re getting a horizontal spin. They spend many hours at high altitude, often wearing a parachute, getting training and practicing this sort of thing. They’re not the ordinary weekend warrior like you or me fooling around at low level trying to impress someone. They’re not that foolish


This shows the airplane climbing. See that the relative wind is at such an angle that the AoA is completely manageable? The airplane’s path has changed. The relative wind reflects that. The AOA is higher than in cruise, because the airspeed in a climb is lower than in cruise. If we keep pulling back, though, the speed falls, AoA increases and adds drag and speed falls further, and we’ll stall the airplane


In a level turn, the AoA is essentially the same on both wings. But wait a minute. Most airplanes exhibit an overbanking tendency caused by the speed differential between the wings, since the inside wing is travelling a shorter path than the outside wing, so it’s going slower and wants to keep dropping. SO we usually end up adding opposite aileron to stop the roll, and now we have a higher AoA on the inside wing and it might stall sooner if we get too slow or too steep. Some pilots tend to slip the airplane a bit so it won’t keep rolling. Safe but a little sloppy.

The relative wind’s Angle of Attack is between it and the wing’s chord line. Dropping an aileron or flap increases AoA. It also increases camber, which increases lift, which is the real function of a flap or aileron. It’s not just deflecting air up or down; it’s changing the camber of the whole airfoil, and therefore the speed of airflow over the top relative to the bottom. More camber = more speed differential = more lift.

If you’re still with me, things are about to get interesting. See the difference in AoA? It’s visible as a gap under the leading edge of the inside wing. It’s a result of the small radius of the flight path of that wing compared to the outside wing, and in a smaller radius the path has to be steeper to descend at the same rate as the outside wing. It helps to counter the overbanking tendency, but can cause this sort of trouble:

Skidding the turn increases the difference in AoA between the wings. And, as we noted last month, a skid requires opposite aileron, which increases further the AoA on that inside wing, bringing it closer to stall angle if we get slow. Remember that chord line changes with aileron input? Don’t do this. It’s a common cause of base-to-final turn accidents. If you’re skidding in this scenario, you’ve messed up the approach. Go around and try again. A good approach starts way back on downwind.

A slipping turn actually decreases the AoA differential and makes the turn much safer. In fact, this is commonly taught as an altitude-losing maneuver if you’re a bit high on base. The inside aileron is up, decreasing the AoA further on that wing.

The angles apparent in the pictures are considerably larger than they are in real life. In a typical base-to-final turn, 30 bank, 70 MPH, the radius is such that there’s only a small fraction of a degree difference in AoA between the two wingtips, but it’s enough to cause grief. The accident history bears this out.

Aha! The classic departure stall scenario. A climbing turn puts the outside wing at a higher AoA, and it will stall first if we pull back too hard, and will try to roll into a spin out of the turn.  This sort of thing is the cause of accidents when a pilot takes off from a too-short strip and tries to clear some obstacles at the end. Read the POH! It has charts regarding takeoff distances over obstacles, and you have to pad those distances a lot if the strip has long grass or is soft or there’s no wind or it’s a hot day. Wishful thinking won’t lift the airplane clear of the trees.

As I said last month, the typical trainer like a 172 will probably just make lots of noise and drop its nose a bit and go on flying if you do this at altitude. They’re very forgiving (but will still hit the trees on that short strip). It’s like learning to drive in Grandpa’s 1971 Pontiac station wagon.  However, go buy an old Champ or Citabria or Super Cub and see what it thinks of this sort of thing. It will bite. There is no better way to spend your money than on thorough and competent training. It’s the best life insurance. When buying an airplane, you need to leave money aside for the inevitable maintenance surprises as well as that really good checkout.

From Paul Parsons

Who killed the Red Baron?

From Jan Nademlejnsky

182. Short Flight over North Ridge Downtown and Sandbars, Kamloops, Jan 13, 2018

The first flight in the new year. Kamloops received a bit of sunshine on snow covered ground and mild temperature, just below freezing. It was short time, which was limited by my level of freezing fingers. I counted 23 eagles on the ground and in the trees, and one in flight. It was good flight.

Video    Pictures

New in the Buy&Sell in the last month


2007 RV9A    USD$75.000.

Beautiful Airplane.   2007  RV9A in top shape !   TTAF 653hrs, TTE 275 hrs, Lycoming 0-320 160hp  Sensenich Prop Fix pitch 275hrs.  Slick Mag. 275hrs. Electronic Ign. 653 hrs. DYNON 180 with Auto Pilot. 327 Transponder Garmin ELT 406, Icom Radio 210, GPS 396 + 796  Antisplat nosegear and tail upgrade.  Always hangared, fresh annual inspection ! Price:  $75,000. USD  Contact: Roman Rotach, owner.    Location: Vernon BC, Canada.     Tel.   250-260-5787 evenings,  e-mail:



2001 Titan Tornado 2    $27,000.

2001 Titan Tornado 2 Advanced Ultralight.  Rotax 912 UL  Warp Drive Prop with nickel leading edges.  TTAF and Engine: 735 hrs.  Prop and Engine Rubber done 2 years ago.  ICOM Radio, Transponder, ELT, Intercom, GPS included.  135 MPH VNE Wing with spades.  Aircraft located at King George Airpark CSK8   Asking: $27,000. CAD or $22,000. USD  Contact Seller:  for more details.


  Need a Project Aircraft.   Will trade

Need a project aircraft. Willing to trade my 1980 low mileage Corvette and/or my 2003 HD RoadKing Classic.   Prefer a high wing aircraft - tail draggers or what have you. A flying aircraft will also be considered. Derek  780-619-1224   (I also use my cell # 780 619 1224 for texting)


1982 Yarrow Arrow   Asking only $3,600.

Single seater tail dragger,, electric start, wheel socks, Modified Lazair wings. Engine is 503 Rotax dual carbs, ignition points; needs rebuild (engine taken out of plane). Ballistic Chute.  Not very much to do and will be up in no time. Buyer will be responsible for moving the aircraft after purchase. (24-ft enclosed trailer recommended.)  $3,600.   ph 250-672-2316 Tom Sorensen


Headset:  AVCOMM  AC-900 PNR    $175.

Ph 250-672-2316 Tom Sorensen


Breezy    $19,000.  OBO

Easy to fly, open airplane:  Piper J3 wing.  Tandem seating, tricycle gear.  Lycoming 0-235 (118 hp) TT 580 hrs.  Top speed 100mph, cruise 80 mph.  Empty weight 800, gross 1250.  Instruments: Alt, AS, VS, tach, compass, oil pressure, oil temp, EGT.  Lost medical, must sell.  $40,000 into it.  Asking $19,000.  OBO.  Craig Lytle,  604-467-3304


1966 PA-28-235 B        SOLD!



Jodel D-11        NOW $3,500.

First flew 1979, 314 TT. This aircraft is being sold as a restoration project, not an airworthy airplane. It will need dismantling and hauling away. The engine (Continental A-65) is off the airplane and needs some valve work, and the fabric needs replacing (last done 22 years ago). The wooden structure needs to be thoroughly inspected and repaired or refinished where necessary. It comes with another old A-65 that has a few useable parts. Asking $3,500. Located in Kamloops. Email   for details.


Looking for adapter

To connect 5.1 speaker system to my laptop.  Cam  250-374-4181


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