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Avoiding Maneuvering Flight Accidents Background
It is hardly news that pilots and passengers are killed because of "stall/spin" accidents. Since I learned to fly in the 1960s instructors and aviation safety organizations including the FAA have been harping on the subject, apparently to many deaf ears. Another no-no of classic fame is "buzzing" or otherwise showing off in an airplane. Nobody will admit to thinking that such ostentatious displays are smart, but we still have a significant number of these accidents each year. Any accident that results from maneuvering the airplane, whether part of the normal flight routine or not, is categorized as a "maneuvering flight" accident. This includes normal traffic pattern operations such as turning from base to final. It includes the various maneuvers we do while training for a certificate or rating. It also includes "buzzing" accidents. The 2010 Nall Report (most recent data available as of August 2011, covers accidents occurring in 2009) states that more fatal accidents occur in maneuvering flight than any other pilot-related category. for the period studied, there were sixty-seven maneuvering flight accidents, thirty-nine of them were fatal. That provides a lethality index of 58%. That means that if a maneuvering flight accident occurs, there is a better than one in two chance that somebody will die. Two Kinds of Maneuvering Flight Accidents As one reads through the NTSB reports on the considerable number of maneuvering flight accidents, a clear divide emerges. Most of the crashes arise out of normal operations. Then there is the other side of the divide where the accidents are the result of buzzing or some other reckless act. Our Purpose and Path Our purpose here is to help the reader avoid the maneuvering flight accident. Since our purpose is not primary flight instruction, we will only briefly review some of the aerodynamics involved. Mainly, we will examine actual accidents, try to learn how the pilot got into the particular accident situation, and how that particular scenario might be avoided by other pilots. Since pilots who are likely to buzz the neighbors' house or perform a roll on final approach are probably not spending their time reading safety articles such as this one, we will only look at one such crash and concentrate on several of the accidents that have occurred during normal operations. Basics Review Airplanes need more than just airspeed to fly. They need smooth airflow over the wing. The aerodynamic stall occurs when this smooth airflow is disrupted. The disruption always is the result of exceeding the critical angle of attack. Remember that the angle of attack is the angle between the relative wind and the chord line of the wing.
Remember that an airplane can be stalled at an airspeed well above the published stalling speed. If the airplane is being subjected to higher than normal 1g forces, the stalling speed is increased. Turning, pitching up, or pulling out of a descent are all things that will increase the stalling speed. Recall that at normal cruise, the airplane is subjected to 1g or a load factor equal to 1. Any maneuver, no matter how slight that forces the pilot down into the seat causes the load factor to increase. In a 60° bank, the load factor is 2. The stalling speed increases with the square root of the load factor. The square root of 2 is about 1.4 so in a 60° bank the stalling speed is 40% greater than in normal cruise flight. But even lesser bank angles will produce higher than normal stalling speeds. Couple that fact with reduced airspeed while in the traffic pattern and the possibility of a gust, and things can turn sour pretty fast. Now remember that a stalled airplane, even a partially stalled one, is a candidate for a spin. A spin is an aggravated stall resulting in autorotation. another word for "aggravated" is "uncoordinated". If the airplane is stalled with the inclinometer ball out of the center, the stage is set for a spin. If anyone believes that their airplane is docile and that this is not likely to happen to them, they're literally dead wrong. Once it happens at low altitude such as in the traffic pattern it is almost certainly unrecoverable. A final consideration of all this is the structural limits of the airplane. Without going into all the numbers associated with limit load factors and ultimate load factors, it is possible to overstress the airplane and disassemble it in flight. The theory holds that if the airplane is flying at a speed less than the published maneuvering speed (Va) it will stall before failing structurally. Of course, a stall is preferable to structural failure, but can have the same result at low altitude. And, the notion that structural failure won't occur at a speed below maneuvering speed is rather iffy. Maneuvering speed is affected by the airplane weight. The maneuvering speed actually decreases with decreased weight as counter-intuitive as that may seem. Also, is a thirty year old airplane or one that has been subjected to the rigors of flight training for many hours as strong as it was when it was built? What toll has that corrosion and its associated treatment taken on the structural integrity of the airframe? Accident Analysis - Reckless Operation
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Disclaimer: Material contained on this web site and in this section is for informational purposes only. It is intended to be supplementary only and never to substitute for formal training. It should not be construed as directive, doctrinal, or instructive. Individuals should consult with their flight school management, certificated flight instructors, aircraft manufacturer recommendations and directives, Flight Standards District Office (FSDO) and/or appropriate FAA publications including the Aeronautical Information Manual (AIM), the Federal Aviation Regulations (FARs), and applicable FAA Advisory Circulars (ACs) for specific guidance relative to any information or before employing any recommendations contained on this web site or in this section. Further, nothing on this web site or in this section is intended to contradict or be in disagreement with any official FAA rule or regulation, nor should such material be interpreted or construed as such. This web site is intended exclusively to promote general aviation and to increase awareness of current events in aviation. GeneBenson.com is a service of Bright Spot, Inc. |
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