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How safe is stall practice in a non spin certified aircraft?

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How safe is stall practice in a non spin certified aircraft?

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Old 29th Apr 2011, 12:17
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Vabsie, crashes of light aircraft are very rare and the few statistics that might be gleaned from them will not tell you all that much about the safety of a particular airframe. So just because you happened to stumble upon a story about an R2120 crash doesn't mean they're less safe than a C152.

in fact, once you start reading accident reports a bit more you will quickly realize that the biggest cause of light aircraft crashes is actually pilot error. Continued flight into IMC, fuel exhaustion or fuel starvation, flight outside the structural limits of the aircraft or gross mishandling of the aircraft at low level. Not by engine or airframe failures.

Personally I like the R2160 a lot more than the C152. It feels much roomier with a much better view. And of course the one I fly has the ability to be turned upside down...

But anyway, you need to realise that at your stage of training it's best to stick to one airframe. Whether that's a C152 or an R2120 doesn't really matter. They're both perfectly good trainers. Once you've got your PPL and a few hours experience, you will want to get checked out on several (maybe all) types that the club operates. This gives you the ability to pick the aircraft type that's best for the mission that you're going to fly.

So pick an aircraft type that you find comfortable to fly in and that has good availability. Finish your training on that type. Other types will come in due course.
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Old 29th Apr 2011, 12:37
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If I remember correctly, that r2120 that crashed was the result of the pilot trying to out climb rising terrain.

I wouldnt say the robin is any more or less safe than anything else out there, the r2160 has pretty good performance (best i have had is 1700fpm on a high pressure winter morning with only me and 2 hours fuel) and visibility is excellent which is definitely a good safety feature.

Just gotta remember the plane is only as safe as the pilot flying it
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Old 29th Apr 2011, 14:47
  #23 (permalink)  
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I have lots of thoughts on this thread, and quite a few disagreements with some of the previous posters.

Firstly - a stall in itself, in a certified aeroplane, is NOT dangerous. At a safe height it is a perfectly reasonable thing to practice, and I believe that as well as stall avoidance and slow flight, all pilots should practice a proper stall once in a while. Very few certified aeroplanes will show any tendency to spin from a sensibly conducted stall, and pretty much all of those will recover from the incipient spin if you simply put all of the controls in the middle and close/keep closed the throttle.

What will kill you is not the stall and stall recovery, it is the height loss if you stall close to the ground. For this reason, it is generally sensible not to practice stalls anywhere below 1500ft agl, or 3,000ft agl if being particularly cautious for any reason. It is however sensible to practice stalls in the circuit - by which I mean visualise an imaginary runway at, say, 3,000ft and practice approaching the stall and recovering from the finals turn, approach, go-around, and climb-out (the last two being statistically the most dangerous, not the finals turn - although that certainly is significant).

A sharp pilot, practicing a stall and recovery deliberately is likely to lose 50-100ft in the recovery, whilst an average pilot recovering from an inadvertent stall will probably lose 200-300ft. Given that, and a bit of safety margin, it's below 500ft that stalls are truly dangerous.


When we certify a new aeroplane type, we will look at a range of stall scenarios - flap settings, power, bank angle, deceleration rates - going rather beyond what should be flown during PPL training. If the aeroplane shows any tendency to spin, that must be sorted out before the aeroplane is certified.

When we certify a non-aerobatic aeroplane type, we still spin it, still confirm that it will recover within a turn, still evaluate mishandled recoveries, and still confirm that it has no unrecoverable spin mode. What we don't do is go beyond 2 turns - rather more is required for an aerobatic aeroplane.

In the UK for the last 12 years, this has also applied to microlight aeroplanes - although that is not the practice in most countries. However, the large powerful cruciform tails on most microlights together with existing requirements for good low speed handling, tend to assure very good stalling characteristics anyhow. The best spin recovery for most microlights however is to close the throttle and put the stick and rudder in the middle - NOT the conventional light aeroplane opposite rudder recovery (there are numerous reports and research papers out there proving this, it's not just my opinion, although I did write some of the reports.)


So, in my opinion, whilst the first and most important part of stall training is avoidance, this is certainly followed by recovery. Practicing stalling is essential for a safe pilot, and at a reasonable height, is a perfectly safe and sensible thing to do. The risk of a spin is tiny, and of an unrecoverable spin far tinier still.




Further thoughts: train now on the nearest possible aeroplane to what you plan on flying after you have your licence. There's nothing wrong with either the C152 or the Robin, nor particularly with switching types in the middle of training - just don't switch too often until you're rather more experienced (and licenced). Personally I'd stick with the Robin, but purely because I think that they're more enjoyable to fly.

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Old 29th Apr 2011, 15:09
  #24 (permalink)  
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Ideally, good initial training will focus first, but by no means only, on stall and spin avoidance. With good pilot skill (though still in the training phase) stall recovery should be instinctive. A stall which threatens flight safety is going to happen when you're trying to do/not do something else in flight, and you're distracted. Recovery must be instinctive. Also, remind yourself, that it is perfectly acceptable for a well controlled stall to go unrecovered on every flight - the flare and touchdown.

It is possible in any light type (certainly some more easily than others) to aggravate a simple stall into something which turns into a spin. This is why you'll be taught to recognize and recover a stall promptly, but effectively, the first time. A buggered up stall recovery is taking you much closer to a spin.

The spin in a certified light aircraft, in and of itself, is not a serious problem, as long as you are going to correctly recover it, with lots of space around you, and without exceeding limitations. Do not go spinning without proper training and supervision, but certainly do go spinning. I am not an expert on spinning, as it is a very complex subject. But, I have spun about a dozen aircraft types during certification flight testing, and have experienced very different characterisitcs, and recovery conditions.

(Nearly) all ('cause I know nothing about Cirrus) certified aircraft are recoverable from a spin, it's a design requirement. Those which are not spin approved are so either because the manufacturer did not wish to have spin approval, or more commonly, because though recoverable, you get very close to limitations doing it. Add to that, that the recovery technique may be variable, based on configuration, and the techniques or cautions too variable to try to describe to the pilot in the flight manual.

My recent testing experience (on test flight permits) includes many stalls in two Piper Navajos, where, while trying to accomplish minimum altitude loss, it was easy to get a secondary stall, and have a rather messy secondary recovery. Certainly a spin could have been obtained doing that, if one was careless. In January, I did more than a dozen spins in a modified Cessna Grand Caravan. Though the handling of this larger aircraft in the spin is magnificent, it would be easy to exceed limitations during the recovery, without great caution. I installed a G meter, and was happy I did, as the recovery for a forward C of G gross weight spin required a 2.8G pull, at Vne. There's not much room to get that recovery wrong! The aft C of G handling and recovery, though also fine, was very different.

There's a video clip here:
?rel=0" frameborder="0" gesture="media" allow="encrypted-media" allowfullscreen>

[They're both the same video, I don't know why it's there twice]

As for your instructor making a remark about it being risky to spin the aircraft, perhaps your instructor is more referring to his/her comfort level, rather than the capability of the aircraft. Ask how experienced you instructor is spinning this type.
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Old 29th Apr 2011, 15:25
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Is that video a spin - looks barely developed to me.
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Old 29th Apr 2011, 15:29
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One turn in, one turn out, that's all I am required to do. At forward C of G, I could not have held it in any more than that, it was on it's way out, no matter what I did. Observed peak rate of descent later calculated to be 9200 FPM.

At aft C of G, it would have stayed in much longer, I had to actually recover it out.
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Old 29th Apr 2011, 15:53
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Genghis, can I interpret your words to mean that, if my beautiful new bird has been certified in the UK, it has been tested to resist and survive a certain degree of spinning? Not that I am wanting to try it out, my stomach is rather delicate, and surely I'd not even think of trying it without proper training - but it would be nice to know, for added reassurance.
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Old 29th Apr 2011, 17:06
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PilotDAR, fabulous video. It must be something else to spin something so big!
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Old 29th Apr 2011, 18:33
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It's likely that intentional spins are prohibited - if you find yourself spinning you are still permitted to recover the aircraft.

A number of long-winged gliders are not certified for intentional spinning, but have all been tested in certification and shown to recover. These gliders are likely to exceed vne during the recovery or suffer some structural damage, so won't be re-usable, but you should survive.
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Old 29th Apr 2011, 18:56
  #30 (permalink)  
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Originally Posted by Jan Olieslagers
Genghis, can I interpret your words to mean that, if my beautiful new bird has been certified in the UK, it has been tested to resist and survive a certain degree of spinning? Not that I am wanting to try it out, my stomach is rather delicate, and surely I'd not even think of trying it without proper training - but it would be nice to know, for added reassurance.
That's correct, although do check that you have the same build and modification standard as we do, and we only started spin testing in 1999 - anything certified before then probably hasn't been spin tested.

The approved lists are to be found on the BMAA and LAA websites (look for documents called "TADS" and "HADS".

I'm a little out of touch, but I don't *think* that your Apollo Fox has ever been approved in the UK.


If you want a stalling or spinning assessment doing, I'm open to offers, or I'm sure that Pilot_DAR would enjoy a holiday in Belgium. It's a necessarily slightly slow process however.

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Old 29th Apr 2011, 19:20
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Very apt this thread.......... We had a situation within our group just the other day with our vintage taildragger (Intentional spins prohibited). The aircraft was on a Permit test flight and the pilot flying the test schedule managed to put the aircraft into a spin whilst carrying out the stall test..........As the aircraft stalled it dropped a wing ( usual behaviour in this aircraft....it rarely stalls straight ahead) and this "ace" only tries to use aileron input to pick up the dropping wing....... result is that aircraft immediately drops away and rotates quickly..........luckily the pax/observer ( another group member with a lot more experience and awareness) quickly intervenes and applies corrective rudder and gets the stick central for a standard recovery....which takes a lot more height than would have been ......Ace seems suitably chastened and hopefully has learnt a valuable lesson...........If this had happened at a lower altitude and unexpectedly , then I think that we would all have be reading about a smoking hole

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Old 30th Apr 2011, 02:58
  #32 (permalink)  
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stick central for a standard recovery
Well.... it sounds that the corrective control inputs were appropriate in this case, and credit to the mentor pilot for keeping things safe...

However, the use of ailerons, in correct harmony with the other flight controls, for a spin recovery, is entirely correct. There are some instructors who teach that ailerons are not to be used during spin recoveries. Generally, this is not correct.

Though the wording of the standard has varied over time, the most recent reads:

[It must be impossible to obtain unrecoverable spins with any use of the flight or engine power controls either at the entry into or during the spin;

A manufacturer may specify a recommended spin recovery procedure, and that may be the one which has shown to result in the quickest recovery, but the "normal" (co-ordinated) use of controls, which certainly would include the use of ailerons, must also work. The only example I can find of a recommendation to NOT use ailerons during a spin recovery, is the Cessna Caravan, where an up going aileron also sends up a roll spoiler. But, I'm sure that it would still recover either way.

I am in the third day of flight test technique training, and this was a highlighted issue today, from the very experienced (ETPS Grad) test pilot. The flight controls are to be used "normally" for a spin recovery. "Rudder only" can be dangerous. You've just departed controlled flight because you have attempted yawed or cross controlled flight, now you're going to completly yaw the aircraft in the other direction in an attempt to regain control. It does not sound as good as the co-ordinated use of all controls as they are designed, approved, and intended, to regain control.

I have challenged instructors to show where the use of ailerons is prohibited in spin training techniques, and no instructor ever has, other than to say "that's the way I was taught"....

Take spin training, which should include the appropriate, co-ordinated use of ailerons during recovery.
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Old 30th Apr 2011, 06:50
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Take spin training, which should include the appropriate, co-ordinated use of ailerons during recovery.
Although I agree with the theory that you present, I don't agree with this blanket advice. For someone without a lot of experience in aerobatics or test flying (as the OP on this thread) I would say: Take spin training but not before you have read the POH and found the correct spin recovery technique for your aircraft. Then use that technique.
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Old 30th Apr 2011, 13:34
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Take spin training but not before you have read the POH and found the correct spin recovery technique for your aircraft. Then use that technique.
Absolutely. Where a flight manual specifies any procedure or technique for that particular aircraft, that supercedes "blanket" techniques.

During certification, the authority will be evaluating the flight manual, to assure that it provides information which is in harmony with the design requirements.
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Old 30th Apr 2011, 17:20
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"Take spin training, which should include the appropriate, co-ordinated use of ailerons during recovery."

With respect, I think the physics of the spin suggest otherwise. The spin is due to coupled roll/yaw and is maintained by this couple -coordination of controls at that point are moot. It is a stable state that demonstrably does not respond to aileron control inputs (unless it flattens to the point where rudder is less effective than aileron due to rudder stall/blanketing in which case either pro- or anti-spin may work and you may not know which will reduce the AOA on the more deeply stalled wing which is needed to weaken the roll/spin couple). If there were to be a general method, rather than that stated in the POH, I believe the key is to break the powerful yaw component with neutral aileron (the PARE method not MB). When the yaw stops in PARE the plane is in co-ordinated flight and the rudder used by the pilot to only to stop further yaw i.e. the controls _are_ then automatically co-ordinated because the aileron is already neutral! In PARE the elevator then fixes the stalled wing and the pilot recovers the dive. I think it interesting that if a little excess rudder still exists, it actually helps unstall the more deeply stalled wing (which is good) and is not what coordinated aileron would do. For most pilots, talk of coordinated aileron implies putting aileron and rudder in the same direction which is certainly not what should be advocated for a spin recovery technique IMHO. The PARe method s simple and does not require the pilot to think about establishing coordinated flight which could be hard when disorientation may also be present. If any general technique is to be advocated then the KISS principle is essential and talk about "appropriate" co-ordination is not going to help (the pilot is already sensory overloaded without having to interpret what might be appropriate).

Further, if the pilot has put in a coordinated rudder/aileron control input to stop yaw he worsens the stall on the already more deeply stalled wing which will oppose the rudder input and delay (or even prevent) recovery. I don't think that the idea of inducing opposite yaw by holding in opposite rudder was ever implied in any spin recovery technique, in all the texts I have seen they say when the yaw _stops_ recover by ... (a method that does not add yaw couples)

Cheers

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Old 30th Apr 2011, 19:04
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If you come out of the spin and find yourself with nose and one wing down, do you think it is a good idea to recover the normal pitch attitude, before using the aileron to roll wings level?
 
Old 30th Apr 2011, 20:18
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Moreflaps,

I'm thinging about what you've presented, though perhaps I am missing some of the intent, as I have no idea what "PARE" means. I have never seen this term in standards, flight manuals, or training texts.

I agree that there are probably reasons of aerodynamics why aileron use may have no benefit in some instances of spin recovery. I do not agree that a pilot is overloaded in having to consider the use of the ailerons during a spin. Rather, I opine that it may be overloading the pilot, to have him/her overcome the instinctive reaction to return to unstalled, co-ordinated flight by "normal" use of the controls.

Many pilots are rudder challenged at the best of times, to now have them concentrate on the use of control which recieves too little attention, to the exlusion of the one they normally use too much, may be overloading.

However, I'll wait to learn about PARE, and keep my mind open....
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Old 30th Apr 2011, 20:28
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I'm just a PPL. I've been taught entry and recovery from spins in Tiger Moth, Chipmunk, C150, C152, and Zlin242L. Each time the instruction was:
Power off. No aileron. Full opposite rudder. Stick progressively forward until spin stops. Centralise controls. Pull out of dive.
I was told the use of aileron to try to lift the more stalled wing would increase the spin forces. I follow the logic of that. Can someone explain the rational for aileron use in simple terms? Both wings are stalled.
P.S. Might it be possible to enter a spin inadvertantly from cruise in turbulence? I'm remembering two NTSB reports of spins.
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Old 30th Apr 2011, 21:11
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the instruction was
Without being disrespectful, was that instruction from the aircraft flight manual? If so, it should be followed. If a pilot chooses a techniqe which is not described in a flight manual, it might be fine, though it still might not be in harmony with the design standards for the aircraft. This also could be okay, I just wonder why not fly the plane the way it was proven to fly for certification.

If the aircraft is in autorotation, one wing has less lift than the other. Both wings still have some lift, just not enough to sustain 1G flight. Generally the outer portions of the wing retain lift longer than the inner portions, into the stall. So if the outer portion of the wing which is providing less lift of the two is still providing some lift, some aileron may provide some more. That small additional lift may help, I've spun types where it did, though only a little.

An interesting exercise when flying an aircraft (which is properly prepared for unusual attitudes and stall practice) is to push the aircraft to between 1G and .5G "over the top", while the airspeed decreases to a little less than the speed commonly associated with a 1G stall. You will find that if you're not demanding the wing lift 1G for a few moments, it will remain unstalled to an even lower airspeed, and the aileons will remain quite responsive. May as well use 'em, unless the flight manual says not to....
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Old 30th Apr 2011, 21:14
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If you come out of the spin and find yourself with nose and one wing down, do you think it is a good idea to recover the normal pitch attitude, before using the aileron to roll wings level?
(my bold)

AIUI, in a spiral dive recovery you are supposed to level the wings first and only then use the elevator. The reason given is to reduce the stress on the tail section.

So I would guess that once you recover from a spin, and you are going fast enough forward for ailerons to work (i.e. perhaps not the AF447 case ) then levelling the wings could be a good idea, before pulling back out.

However, one variation of the spiral dive recovery involves a recovery from a very "advanced" spiral dive (at/above Vne) where once you level the wings, the speed is too great for the current pitch trim setting and if one did nothing with the pitch, one would overload the wings (+G), so one actually needs to push the yoke forward a bit to limit the +G.
Might it be possible to enter a spin inadvertantly from cruise in turbulence? I'm remembering two NTSB reports of spins.
I don't think so unless you are doing stuff which brings you close to Vs in cruise.

One way to do this is to be probing the operating ceiling. In high altitude flight, engine power drops off and IAS keeps reducing. TAS holds up well but eventually IAS reaches Vs... I have come close to the stall a number of times, trying to climb to say FL200 at ISA+something. It's easy to do this wrong with autopilot controlled climbs. Program +300fpm and let it go and it will do it. Throw in uncoordinated flight (lack of elevator input or lack of elevator trim) and some turbulence and a pilot who is dumb (or hypoxic) and you can lose it. I think one SR22 chute pull was after doing that (though surviving pilots have a reason to not say too much).

Another way is to ice up. All bets are off then. You can be flying at 150kt, collect a couple of inches of ice, speeds drops off but actual Vs goes way up, no stall warning because the tab is frozen in the ice, and with some turbulence you can lose it too. I think another SR22 chute pull was after doing that (though surviving pilots have a reason to not say too much).

But I can't see one could do it in say Vs * 1.5 or faster because (on any certified plane) the vertical stabiliser will have tons of authority to limit the yaw caused by turbulence.

But it's a good Q whether turbulence causes roll (with yaw being a secondary effect), or yaw (with roll being a secondary effect). I have noticed that I get a lot of yaw in turbulence, whereas say a 737 (with yaw damping) gets no yaw and very little roll (and just gets a rough up/down ride). Does turbulence really affect one wing more than the other?
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