Re the
Der Spiegel Article Below
Quite likely to be the
LUXAIR F50 accident cause because of the appearance of the wreckage
(virtually fell straight down as if it had lost airspeed very rapidly - as
it surely would if it experienced GROUND IDLE in flight.
No sane pilot is going to lift a guard and select power-levers to
ground-fine whilst airborne (that's a very definite action in any
turboprop). In
fact Ground fine is an F-27 term, whereas on the F50 Ground Idle equates to
the start of the beta range (alpha range being the flight range in most
turboprops and very positively divides forward thrust from the reverse
thrust commencing at the top of the beta range).
It's far more likely that another selection on the centre console (flap
perhaps, but may have been anything?) caused an
electrical short and removed
the beta stop baulk, allowing the pilot's reduction to low Flt Idle power to
"go through" into ground idle. Or maybe the short was there all along and
the baulk just wasn't there. I would guess that a box swap-out may have
occurred on that centre console during the "technical check the day
before".... and that could have set up a short (or the makings of a short).
But they'd fall out of the sky really quickly if both had gone into GI.
Really needs a further explanation for why they were so far right of the
final approach course for the ILS and heading even further right. So it may
have been that the excursion into Ground idle occurred on only one
engine (i.e. he didn't bang both against the "disappeared stop" and only
one, the RH one, went through). The asymmetrics would have then taken them
(and their heading) right of course. I'm not sure whether immediate
feathering action is available on an engine with its prop stuck in ground
idle. Would it possibly be inhibited? And how feasible is a quick
reselection of the Flight Range (assuming that they tumbled to what had
happened?)
Can a tripped CB remove that GI baulk? All good questions that remain
to be answered.
******
Up until the point where this info came
out, it was a quite confusing accident (and aren't they all). It's now
falling into place and may well have been a wiring-related/electrical
cause - because that GROUND IDLE BAULK is a solenoid-operated electrical
device (weight-on-wheels or manual override).
So either:
a. the technicians left the CB (for
the baulk) out during the previous day's servicing (and the
pilots didn't notice it out )
or
b. the CB had shorted out itself out
(or tripped enroute) or
c. There was a short that kept the
baulk in absentia through-out or
d. There was a shorting-out (that
removed the GI baulk) when a flap handle (or something else was moved -
at about 1000ft AGL on finals).
e. The pilot had
intentionally selected Ground Idle (unlikely)
All it would have then taken was a power
reduction to against that non-existent GI stop
and the one (or both) P/L's could go through (into GI). However some
turbo-prop aircraft have an additional soft-stop that must be overridden
airborne (pulled through - but needs brutish force). I'm not sure whether
that's the case for the F50. I'd doubt it actually.
I It still seems
(prima facie) to best be an electrical explanation. Finding evidence of
that may be possible as the cockpit was about 75% intact.
The Relevant AirWorthiness
Directives (for the Flight Idle Stop Hazard)
Four Very Similar CASA 212 accidents
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