In a message dated 11/14/2006 11:49:32 A.M. Central Standard Time,
kevin@airforcemechanical.com writes:
I am
starting to wonder if it is a bad idea for the LML to be used as
a
form for speculation regarding the causes of an accident,
especially
after a death.
Would it make more sense to wait until the NTSB publicly
publishes
their results. At which time we can have an informed
dialogue where
we all can potentially learn something from the
tragedy.
Kevin,
Sometimes the NTSB never publishes a "Probable Cause" report. People
often want to discuss an accident while it is fresh in their mind.
Speculation is not necessarily a bad thing in that there are often safety
offshoot discussions resulting from some of the speculation.
Take the Cirrus 20 crash into a mountain side like residential
building in NYC whilst in an impossible turn. USA Today had some great
graphics and the NTSB, having more information than many of us, indicated the
problem with the turn - i.e. the turning space was a bit tight worsened by the
east wind moving the air mass towards the riverside buildings. While there
was some question about the reason for turning, it seems that the PIC just
didn't want to contact La Guardia tower for transit through their airspace as
the VFR defined corridor was coming to an end. The claim is that the 180
degree turn had to be done in less than about 1700 feet of horizontal space with
an approximate loss of about 300 feet because of crosswind drift and at a
constant bank of over 50 degrees at the estimated speed of 97 Kts, reducing the
width to about 1400 feet. Well and good as this seems to be the box canyon
problem. Do you know the turn radius of your aircraft at several speeds
and bank angles?
I had a spreadsheet for calculating the distance traveled and radius of
turns at race speeds and different bank angles. I modified the Excel
spreadsheet to calculate the Width of an 180 degree turn at different bank
angles at a given speed and crosswind component. It also calculates the
increase in stall speed for a given clean level flight stall speed based on
increased load factor. My numbers are very close to those in the NTSB
statement. Down load the spreadsheet and plug in your
own numbers in the shaded boxes. For example, were I sightseeing at 140
KTAS and did a 180 with the same wind conditions at a 60 degree bank, the turn
width would have been 2300 feet (300 feet contributed by the 13 Kt cross
wind - maybe that would have put me beyond that building). My clean stall
speed would have moved up to about 100 Knots. It would have been a
lot easier to just call the LGA tower.
I have been interested in one where a 235 hit the perimeter fence at a CA
airport - what was the purpose of the low approach angle? This one took
the NTSB 15 months to issue the probable cause report. The pdf is
attached. Personally, I like an approach steeper than 3 degrees on final -
more options should something not be right.
How about this spin accident? Training, showoff, bad mistake or
something else? This accident was in Jan, 2005 and there is still no
probable cause report. There are spin discussions on the LML all the
time - If only we knew what was going on in the cockpit..........
Note that the recent turbine accident is not yet even listed in the NTSB
monthly report files:
Thoughtful speculation and discussion helps me think about things I should
or shouldn't be doing, just like virtual "duh" training.
Scott Krueger
AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL (KARR)
A man
has got to know his limitations.