Parowan midair?

On 6/16/2010 10:20 PM, 5Z wrote:
On Jun 16, 12:34 pm, wrote:
There's several words to describe that - "competitor" and "big brass

Actually, I'd call it pretty irresponsible. That glider could, at any
moment have a system failure due to weakened structure. The only
smart response is to land IMMEDIATELY, and definitely avoid overflying
any people on the ground.

Just checked the rules, and there's nothing in there regarding a
pilot's responsibility after a collision.

But several years ago, at a national contest, there was some heated
debate at the mandatory meeting about what a pilot should do in such a
case. If I recall correctly, an immediate landing for inspection was
mandated, with one or two vocal "I'm here to WIN!!!" dissents.

Nothing bad happened this time. But what if someone had been hurt or
killed due to a system failure while the pilot continued to soar?
What would be reported in the media? What would the NTSB response be?

-Tom
Not only was this irresponsible, but it was most likely a violation of
the FARs:

49CFR § 830.5 Immediate notification.
The operator of any civil aircraft, or
any public aircraft not operated by the
Armed Forces or an intelligence agency
of the United States, or any foreign
aircraft shall immediately, and by the
most expeditious means available, notify
the nearest National Transportation
Safety Board (Board) field office when:
(a) An aircraft accident or any of the
following listed incidents occur:
(1) Flight control system malfunction
or failure;
(2) Inability of any required flight
crewmember to perform normal flight
duties as a result of injury or illness;
(3) Failure of structural components
of a turbine engine excluding compressor
and turbine blades and vanes;
(4) In-flight fire; or
(5) Aircraft collide in flight.
(6) Damage to property, other than
the aircraft, estimated to exceed $25,000
for repair (including materials and
labor) or fair market value in the event
of total loss, whichever is less.
(7) For large multiengine aircraft
(more than 12,500 pounds maximum
certificated takeoff weight):
(i) In-flight failure of electrical systems
which requires the sustained use
of an emergency bus powered by a
back-up source such as a battery, auxiliary
power unit, or air-driven generator
to retain flight control or essential
instruments;
(ii) In-flight failure of hydraulic systems
that results in sustained reliance
on the sole remaining hydraulic or mechanical
system for movement of flight
control surfaces;
(iii) Sustained loss of the power or
thrust produced by two or more engines;
and
(iv) An evacuation of an aircraft in
which an emergency egress system is
utilized.
(b) An aircraft is overdue and is believed
to have been involved in an accident.

It is hard to see how you could meet the requirements of this section if
you 1st finish flying the contest.

--
Mike Schumann