At 11:00 AM 4/05/2012, you wrote:


There is nothing in this statement from Mike B that contradicts what I wrote. It is not I that misunderstands the certification process or the politics surrounding it. I think that Mike B does too, but objects to some of the consequences of the process and the politics.


Like more expensive aircraft which then sell in fewer numbers and an industry that consequently isn't as large and vibrant as it should be that continues to make obsolescent stuff because re certifying is too expensive. Established manufacturers won't complain too much because new entrants find it difficult to begin. Not to mention the odd bit of corruption or ridiculous events like the then DCA requiring the removal of the stick pusher from the first Learjets in Australia making the aircraft less safe by the time they had finished "certifying"it. My BD-4 was built under the old Amateur Built 101.28 rules. It was tested by a CASA/CAA/DoT test pilot (whatever they were called then) and remained in that condition until I bought it. It was marginally dangerous in my opinion. Once it was Experimental a couple of minor tweaks made it far safer and actually quite civilized and 5 knots faster on less fuel burn.

A South African manufacturer elected to certify to the European standard, to gain a type certificate issued by the South African authority.


AFAIK the European Authorities encouraged them to get SA certification to give them some experience and ease the path to European Certification. So they lied. Jonkers are up against another Euro non tariff barrier.



Many people rail against "certification" for gliders and say we do not need it. Would they likewise say that we should all be able to go out and buy a car that had not been shown to meet the Australian Design Rules? I doubt it, as the liability issues are far greater with a car because of the number of "innocent bystanders" they expose is a much bigger number.

I've driven cars overseas that don't meet Australian design rules and it bothered me not one whit. There are older cars on our roads that don't meet current rules either. In any case a car manufacturer has a much larger production run over which to amortise the certification costs.

All of which has exactly nothing to do with the requirement to certify pieces of sporting equipment. Certification of gliders is a historical accident. If they were invented today gliders would likely have certification similar to LSA aircraft or even none at all given their limited appeal and relatively small numbers.


So what does certification do? It identifies that the individual airframe conforms to a known and proven standard, giving at least a partial guarantee that it has no known design defects and will presumably be able to be sold to someone else in future without leaving the seller with any residual responsibility.

I suspect you presume wrong. As Mark said "What's a partial guarantee".

(Most experimental aeroplanes in the US are never sold to a second owner - even if perfectly serviceable they are simply abandoned when the owner/builder retires either themself or the aircraft from flying.)

Seems there's a good trade in used Experimental aircraft though and I have yet to hear of it having any effect on glider sales there. Don't know if it extends to 51% but so what? Certainly there's a lot of buying and selling going on on the BD-4 newsgroup. There's also quite a few people willing to buy Experimental aircraft who don't or can't build them themselves - hence the various "builder assist" programs or you simply ask someone to build you one and buy it from him afterwards. This did lead to a problem as the builder gets the repairman certificate which lets him sign out the Annual Condition Inspection. Some builders' contributions to the build were limited to being photographed with the partially completed aircraft. This could be fixed by a course to get the Repairman qualification - for that aircraft only while you own it. Canada has for some time has owner maintenance of simple light aircraft IIRC.


It also provides protection to the original buyer that the manufacturer takes responsibility for the design and is required by law to report any known problems and issue service bulletins to resolve them - these form the basis for Airworthiness Directives to legally enforce carrying out the work to fix the problem, as well as providing a maintenance schedule to keep the aircraft in its original (or at least within tolerances of that) for as long as possible.

Meaning it is kept in a state where it cannot take advantage of new technology. I wouldn't trade my LightSpeed electronic ignitions for magnetos and aircraft plugs ever. For starters fuel burn is 15% better with the electronic ignitions, the engine runs smoother particularly at altitude and seems to pull a little better manifold pressure for takeoff. My sparkplugs cost $5 each. Bought an aircraft plug lately ? In any case anyone owning a certified German self launching glider would know what the certification is worth as far as the motor is concerned. Nothing.


It is a sad fact that certification costs money (especially when the certifying authority is EASA, as a 27-nation organisation has the overheads of large bureaucracy without any particular advantage for small or recreational aircraft).

None , I'd say.

The advantages accrue to the large aircraft operated by airlines, and unless they find an acceptable process for light aircraft (and this still costs to develop a suitable standard and process) then EASA may never be a suitable certification authority for these aircraft. They have not yet accepted the LSA standards that cover most glider designs quite adequately, except that they restrict the approval of modifications to the original manufacturer rather than to a competent engineer - even to the kind of radio fitted in some cases!

And this helps safety how?



And yet ultralights have escaped this which is why there are a number of very nice ultralight gliders in Europe. Some Euro countries don't have an ultralight glider category so the designers put in an engine and called it an ultralight aircraft. UL regulation has remained with individual countries. It was beyond the wit of the gliding bodies to resist assimilation by EASA. Funny thing is that the ultralight gliders are not as strong or robust as CS22 gliders. 4g limit loads instead of 5.3g. Much lower rough air and Vne speeds.


Another problem with a certified product is that the engineer who approves a modification has to take responsibility for that modification, which in these times involves product liability insurance or the risk of being sued under an imperfect legal system. Again this raises costs.

Another good case for Experimental where the operator is responsible for the safe operation of the aircraft.


It all depends on how much responsibility you are willing, or are permitted by society, to assume on your own shoulders - and society is often unnecessarily restrictive on the individual in an effort to protect the majority against the very few who would be classed as psychopaths, or even those who exploit the weaknesses of others to an unreasonable extent for personal gain. The problem is defining what is reasonable!!!


The main problem is protecting ourselves against bureaucrats and politicians who are psychopaths. They exploit the big lie that they are protecting people in order to gain votes and keep their jobs.

I have no problem with some design standards. Outfits like the old NACA and RAE and others codified the operational experience of early aircraft and developed design standards which designers could use. This is quite reasonable and is good for the designers as they don't have to try to figure out just how many g the limit loads ought to be and where the corners of the V - n diagram ought to be. Any competent engineer can then design a structure to meet this requirement. What costs is putting the damn thing on a fatigue rig and then breaking one. After 50+ composite glider wing designs, all of which are built essentially in one of two ways with no fatigue found, this is stupid. Nobody nowadays is going to build a non ultralight glider that isn't designed to CS22 although there are things in CS22 that over design gliders particularly for countries like Australia where cloud flying is banned. *Proving* to a bunch of bureaucrats that it meets these requirements is where the expense is. I'd be happy with a statement by the factory that the glider was designed to CS 22 and after factory testing meets those requirements except in the following ways... Certification DOES NOT protect the manufacturer from any liability claims. Just ask Cessna, Beech(Hawker Beechcraft is about to go into Chapter 11 bankruptcy), Piper, Frank Robinson etc. What it does do is prevent innovation, prevent the entry of new participants, cost heaps of money and generally kills the industry. As the guy said in that FlightGlobal article "we have created a monster".

Mike




Borgelt Instruments - design & manufacture of quality soaring instrumentation since 1978
www.borgeltinstruments.com
tel:   07 4635 5784     overseas: int+61-7-4635 5784
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Borgelt Instruments - design & manufacture of quality soaring instrumentation since 1978
www.borgeltinstruments.com
tel:   07 4635 5784     overseas: int+61-7-4635 5784
mob: 042835 5784                :  int+61-42835 5784
P O Box 4607, Toowoomba East, QLD 4350, Australia  
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