SA_F_2015_04_

(Barré) #1
46 SA Flyer

pitch and high airspeed, by introducing a
correcting force while still providing the pilot
with feel. For example, once I rolled the
aircraft past 45 degrees of bank I became
aware of a subtle resistance through the
yoke. At 60 degrees the sensation was
no longer subtle but a quite substantial
self-righting force, and although I could
have either physically over-powered it or
temporarily disabled the system by pressing
the AP disconnect or CWS (Control Wheel
Steering) buttons, the sensible (and logical)
course of action was to just let go and
let it sort itself out, which it promptly did
by returning to straight-and-level flight.
Intrigued, I try a few more excursions in roll
and then move onto various pitch angles,
and once again (this time at 15 degrees
nose down and 17 degrees nose up) I
sense the self-righting force through the
yoke.

Should you be hand-flying and become
incapacitated – possibly by illness or
vertigo – and begin to feel you are losing
control, all you or the person sitting next
to you has to do is punch the blue ‘LVL’ on
the panel. This automatically engages the
AP and returns the aircraft to straight-and-
level flight. This is all very impressive, as
the important point to remember here is
that should the ESP activate, it is entirely
automatic, while engaging the ‘LVL’ mode
only requires one clearly marked button to
be pushed. Furthermore, if the ESP has
been engaged for a significant length of
time (it’s quite complicated, but essentially
it’s any ten seconds in a 20-second period)
then the AP auto-engages in level mode.
A further enhancement of the
GFC-700’s capabilities is that the AP’s
engagement envelope has been expanded
significantly and it can engage up to
+/-50 degrees in pitch and 75 degrees in
roll. Now, some of you may be thinking
“this is all well and good, but if the pilot is
temporarily incapacitated and the non-pilot
passenger has punched the ‘LVL’ button,
what’s to stop it stalling?” Patience – I was
coming to that.
Under Craig’s direction, I press the
aforementioned ‘LVL’ button and then draw
the power lever back to idle. The airspeed

bleeds away as the AP initially maintains
straight-and-level flight, and then as the
airspeed becomes dangerously low and the
angle of attack increases the Underspeed
Protection (USP) kicks in and smoothly
lowers the nose to maintain the speed at
around five knots above the value at which
it would stall. I was hugely impressed – and
even more so when Craig explains that the
enhanced AFCS also provides for coupled
go-arounds. If you just hit the TOGA (take-
off/go-around) button on the power lever
the AP levels the wings and pitches the
nose up nine degrees, but if the published
missed approach procedure is loaded and
active the AP will fly it, all the pilot has to do
is push the NAV button on the AP controller.
And should you be sufficiently remiss to
press TOGA but neglect to increase power,
the USP system automatically pitches the
aircraft to maintain an IAS just above stall

warning activation. Frankly, I found the
whole thing rather incredible – as systems
boasting this level of sophistication are
typically only found in giant jetliners, not GA
aircraft with six seats and only one engine.
Descending rapidly back towards Vero
Beach it suddenly occurred to me that I
hadn’t even thought about the new digital
pressurisation system. It functions so
smoothly that I was completely oblivious of
its presence. The cabin pressurisation runs
at 5.6psi, which equates to a cabin altitude
of approximately 10,000 ft when the aircraft
is at its certified operating ceiling of 30,000
ft.
A power setting of 55% torque and a
speed of 100 kt seems about right on the
downwind leg, and as we pass abeam
the numbers I select the first stage of
flap and lower the undercarriage before
commencing the turn onto base and going
to Flap 2. As we turn final the long cowling
somewhat blocks my view of the runway,
but full flap smoothly pitches the nose
down, greatly improving the view.
Easing the power lever back to 25%
torque drops the speed to 90 kt, but I’m
momentarily distracted by an Archer in front
of us that the Traffic Advisory System has
detected but neither Craig nor I can see.
I allow the M500 to dip slightly below the

glideslope but quickly retrieve the situation
with some power, take the power back off
on short final and cross the fence bang
on the Vref of 85 kt. All I have to do now
is land, but I make the same mistake as
with the Mirage and Matrix and try for a
fully held-off landing, with its associated
prolonged float. Get that wing in ground
effect and it just doesn’t want to stop flying.
With all three wheels eventually on the
runway I pull the power lever into ‘Reverse’.
The engine bellows hoarsely and within
seconds we’ve lost 40 kt and I move the
power lever back into idle to avoid prop
erosion.

CONCLUSION
Later that evening I make a few notes,
think about what I’ve just seen and begin to
realise just how important – and influential


  • the latest aircraft from Piper might be.
    And these technologies will continue to
    mature, to the extent that, one day, the ‘LVL’
    button may be replaced by an ‘EMERG’
    button that literally flies the M500 to the
    nearest suitable airfield and lands it. This
    isn’t the same as the concept of pilotless
    airliners, but simply an emergency feature.
    Can you imagine what a confidence booster
    this would be for nervous passengers?
    Remember that the M500 is a single-pilot
    machine.
    Way back in 1939, Piper practically
    created practical General Aviation with the
    immortal J-3 Cub. Now, some 76 years
    later, Piper has quite possibly taken aviation
    safety to (if you’ll pardon the pun) another
    level.


Systems boasting this level


of sophistication are typically


only found in giant jetliners


Vortex generators along the wing.
A new addition to the PA-46 type.

j


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