Sorry for this long response but I am passionate about this issue and some
clarifications are necessary.

It is only true that most spins can be prevented if 1.5Vs is maintained. A
mishandled entry of more than 1 "G" steady is possible at much higher
speeds. (E.g. Mishandling and Snap rolls)

Many things lead up to the inadvertent spin accident. Having reached
autorotation, only a successful spin recovery can save the final accident
chain outcome.

We must mitigate against this identified risk. Obviously, safe speed near
the ground training is not working all the time and only gives the training
department a false sense of security in their job of preparing a safe
pilot. We all perform this monkey do action for the instructor and yet we
still have spin accidents. The fact is that all pilots can make mistakes
when loaded up in a circuit and our best laid plan is falling apart. This
stress can and has resulted in slower than intended speeds. The majority of
spin accident result from too slow/high angle of attack flight.

When everything else has failed, it is the ability to recover from;

1. Slow flight

2. Stall,

3. Incipient spin, and finaly

4. Spin

that may save the day. I certainly wouldn’t give up on a full spin recovery
well below 1000ft AGL! An incipient spin recovery on final should still
result in a controlled landing. And every one of us has recognised
inadvertent slow flight on short final and done something about it to avoid
the heavy landing. Instructors see this one every day.

We need more low speed, high angle of attack flying training; not less. A
yearly check in a training ACFT by an instructor under pressure to accept
the minimum requirement, with the average pilot, no longer current and now
in another type, 12 months later, who has inadvertently allowed his IAS to
decrease below some nominated speed is an accident chain. If progressed to
this stage, then the final outcome will only be saved by knowing how to
identify high angle of attack flight and a speedy recovery.

With regard to the “slippery” training ACFT not providing realistic anti
spin training.

It is the instructor who makes the over-riding difference but even then,
one should not blame the tools he has to work with. I also note the high
drag/low drag and the money savings/pilot satisfaction arguments. I address
the high drag verses low drag argument as it applies to the ACFT I'm
familair with, having read their Flight Manuals. I use the techniques
personally taught me and described in AG by Mike Valentine and the GFA
Instructors Manual and I do have aerobatic endorsements. I mention this
because I want to stress that the aerodynamic/gyroscopic/CofG
characteristics of the preferred types mentioned are consistant when using
Mike's technique.

I know that the DG1000 can be recovered with the same or less height loss
as the Puchacz and both of these take a little more than the older L13 and
the L23. This is directly related to the type of *autorotation*
entry/recovery characteristics of the types, not the pull out from the
ensuring dive. The Blaniks take just a little over 90 degrees of turn to
recover from the autorotation. I have also extensively checked the spin
entry and recovery characteristics of the ASK21 with its required spin kit
fitted. Suffice to say no instructor willingly uses the ASK21 for spin
awareness training at Beverley. Other clubs may have no other choice.

The full spin recovery is designed to minimise the height loss once a spin
has been allowed to develop. A major part of height conservation is gained
by correctly identifying when the ACFT has recovered from the autorotation
phase and we can therefore re-apply back stick but importantly play “G”
against airspeed. Amazingly, in the majority of cases on all types, this is
the area where most will lose excessive height; just when the ACFT is under
their complete control! The problem is one of identification and this can
only be improved by determined training and greater currency; not less. It
is not ACFT specific and it is a cop out to propose one ACFT is worse than
another. The instructor needs to become current with all his ACFT and teach
minimum height loss with that particular tool. After all, it is a club ACFT
and will be flown be a wide cross section of club members, all of whom form
an accident chain sooner or later.

The DG1000 autorotation recovery is both predictable and quick at all pilot
weight combinations because of the ingenious and quick tail ballasting
facility allowing a generous CofG range for spin training, even with the
GFA 5% reduction over the Flight Manual range. The following pull-out
phase, due to the initial lower zero “G” drag and subsequent increasing “G”
lower drag during pull out provides a higher acceleration meaning less time
to achieve safe flying recovery speed and therefore less height loss in
this fully aerobatic ACFT. One should be achieving a recovery speed maximum
of 65-70IAS on this type or redoing the exercise before sign off. I would
need to check my flight logger but expect two full spins before initiating
recovery to take less than 1000ft from entry height to lowest part of
recovery height before recovering much of this height loss when back at
1.5Vs again. In any case, I get the same number of training exercises in
the DG1000 as I did with the older L13/L23 and like those earlier ACFT, the
DG1000 is always spin training ready for all flights; an important factor
if we are to truly keep our pilots current.


-- 
Kind regards
Daryl Mackay
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