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Fatal Light Aircraft Crash Gundaroo North of Canberra 6 Oct 2023


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I think the only thing that will come out of this in wreckage is whether the rocket in the BRS got triggered, or not. 

Air services might also have access to might higher time resolution data than presented on flightradar / flightaware.

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Glen, if it had a glass panel there maybe data on a chip ( that’sa very big maybe though). I know ATSB has some skills at trying to recover data from chips burned and smashed because my brother did a course on this prior to retirement. He was amazed at what could be recovered.  Still there focus was on heavies and it’s most likely they won’t consider it worthwhile for a GA non-commercial flight.

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The spacing of the Isobars gives the best indication of wind speeds, whether it's a high or a Low  The properties of the Airmass will determine whether you get rain or  not as well but highs have descending air so tend to be colder and therefore dryer.  Tropical Maritime air masses tend to have the most water associated with them and therefore the most energy. (Cyclones).    Nev

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It's bad enough that the plane crashed killing the pilot, but losing the three children as well makes it particularly tragic.  I don't know how any family could cope with this.

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I used to  fly regularly in a mate's SR20. He told me that  no matter who the passenger or age, he made sure they knew when to and how to deploy the CAPS (chute) .  If they were too small to pull it, then they didnt fly...

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A poor workman blames his tools ???????

 

From this article: 

WWW.AVIATIONSAFETYMAGAZINE.COM

A series of accidents has tarred the reputation of what was supposed to be the safest GA airplane ever made. But is that an accurate picture? An honest look at the Cirrus accident record.

 

The high percentage of Cirrus accidents that are fatal appears to reflect how the airplanes are used-as all-weather, cross-country machines-by pilots not necessarily trained or experienced enough for that kind of operation. All the safety gadgets Cirrus has added, including the parachute, haven't proved capable of overcoming a lack of skill or basic errors in judgment by pilots, just as with all the airplanes flown before.

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It's very likely, but still a generalisation. I'm inclined to think Incapacitation in this case with icing. I think all of the plane came down together. I doubt we will ever CONCLUSIVELY KNOW.    Nev

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6 minutes ago, Jabiru7252 said:

I was under the impression that the Cirrus was difficult or impossible to recover once in a spin. 

 
My impressions are that the Cirrus are more spin resistant but once you get into a spin it is very difficult to get out of one.
(The opposite is also true, the planes that are easier to spin are easier to get out of the spin)

It is not good to spin an airplane at low altitudes (1000 feet or less is usually fatal).

From the below article

To link the rate of “fatal mishaps per year”, the NTSB database was used to find out, how many fatal accidents are stall/spin-related. For the period from 1999 – July 2008 the following numbers were determined for some types of aircraft.
Cessna C172 19%
Piper PA28 8%
Mooney M-20 16%
Cirrus SR20/22 26%
Percentage of stall/spin-related fatal accidents for some aircraft types it is evident that the amount of stall/spin related fatal accidents of the SR20/22 is considerably higher-than-average.

Assuming that the typical mission profiles of a Cessna 172 and an SR20/22 are equivalent (same flight time in low speed phases), and the SR20/22 complies with the requirements according FAR23.221(2), it must be ascertained a contradiction that the SR20/22, as the aircraft with a lower “tendency to spin”, has more than double the rate of “stall/spin-related fatal mishaps per year” than the Cessna 172 (see 6.2.4), as the aircraft which complies only with the spinning code but not with the FAA spin resistance option.

The article below also recommends the following depending on certification

A placard “AVOID STALL! DO NOT SPIN! Spin recovery has not been
demonstrated.” must be placed in a highly visible position at the instrument
panel.
Remarks: Most pilots are probably not aware that their aircraft is designed under a
principally different regulation as regards the stall and spin behaviour (e.g. the
difference between C350 and C400). As a result, they risk entering a flight state that
is not recoverable. Clearer information must be given to the pilot to prevent
intentional and unintentional spinning.

As most of the pilots are not aware of the conceptual difference between spin
recoverable aircraft and spin resistant aircraft, the wording of the placard must differ
from the standard placard. “Spins prohibited” is not appropriate for spin resistant
aircraft
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It's NOT spin certified. Thats why the BRS Chute is mandated.. Accident and fatalities are on record.  I haven't seen a comprehensive analysis of it's flight characteristics but the tail looks as if it is shielded more than some are.  Nev

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1 minute ago, facthunter said:

It's NOT spin certified. Thats why the BRS Chute is mandated.. Accident and fatalities are on record.  I haven't seen a comprehensive analysis of it's flight characteristics but the tail looks as if it is shielded more than some are.  Nev

i found the comment above with a quick search. lots of talk over the years on the subject.

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 You need to tell the aeroplane that spins are prohibited.  I don't agree with the statement about ease of getting into and out of a spin being directly related. it's more complex than what that statement would have you believe  There are obvious and tried  design  aspects/methods of making that plane better to be able to recover from spins so why hasn't that been attempted?   Nev

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To answer my own question It would appear that from a marketing approach the concept of the BRS chute has been "MADE" the answer. I'm not a fan of lawyers being involved vicariously but there would appear to be a possibility of a challenge  where a known "fault" in the handling is  taken care of by a safety device with usage  limitations as a policy.  . Nev

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I'd buy a Cirrus if I could....(except for lack of payload/baggage )  - the BRS - Would solve the flight at night over in hospitable terrain issue without needing a twin  and all the complications that go with a twin....

But.. engine kill  needs to be mandatory with chute deployment. Maybe it already does that.

A few 182s have BRS installed. Not a bad fit.... The Cirrus SR20 is a inexpensive plane per mile (after you've paid for it) - backed off, 238mL/nm at 135TAS... (My Archer  is 260mL/nm at 120TAS @ 11k'

But, baggage capacity, for me is a bit of a not starter. 130lbs max. and a puny baggage door. My Archer is a load hauler , 200 lbs in the back...plus what I can fit when rear seats are removed (another 300 lbs) . (cant easily do either in the Cirrus) . My next plane is an Arrow4.

 

Edited by RFguy
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and a fire in a composite plane is no good... I'm surprised if a well maintained  aircraft would catch fire in flight.  (not really saying much, I think we'd all be surprised if our aircraft caught fire). 

The 120 kts to the ground though isnt all that fast in controlled flight for that aircraft . So I dunno about a fire.....would have though pilot would adopt the inflight fire suggestion in the POH.  (which is get down as fast as possible) .  

So I am discounting a fire in probability.  and that the aircraft looks like it was in one piece when it 'landed' vertically.

 

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The "fires" I'm talking of relate to  POST crashes.   Fire is not the Cause in that circumstance.   Vertical speed  RoD to contact above say 60 MPH are where it's usually fatal. Some spinning aircraft achieve that. (light Aircraft).  Nev

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44 minutes ago, RFguy said:

and a fire in a composite plane is no good... I'm surprised if a well maintained  aircraft would catch fire in flight.  (not really saying much, I think we'd all be surprised if our aircraft caught fire). 

The 120 kts to the ground though isnt all that fast in controlled flight for that aircraft . So I dunno about a fire.....would have though pilot would adopt the inflight fire suggestion in the POH.  (which is get down as fast as possible) .  

So I am discounting a fire in probability.  and that the aircraft looks like it was in one piece when it 'landed' vertically.

 

Go on ATSB; I can remember several from just leaving the oil cap off, and looking at the wiring of some of the home builds there's room for a few shrts as well. There's a long thread on it here after some fires.

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Given we know little, bar the impact it could have been a fire but a big maybe.

 

The dire need to get to ground and out of the aircraft means a pilot can easily exceed vne and jam / wreck controls. Can easily lead to airframe failure or even just loss of control. Given the destruction it could have been burning in flight but post crash is more likely.

 

Weather or health related or pilot error or any combination are possible, as is mechanical failure. 

 

Sadly a tragedy we may never truly understand.

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