My God, there are some desperate folks in this forum.
More like disbelief than desperation - as you continue your "obsolete cursade", despite countless opinions that beg to differ, without any substantial evidence to back it up.
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The loss rate of the 109 in landing accidents is documented. If you happen to own "JG53 Pik As" Series by Jochen Prien or "JG26 War Diaries" you can follow the 109's accident rate as the pilot training deteriorates in the Luftwaffe.
And is that a result of trainees lacking practical training being prematurely sent into a field of battle to return home after a stressful fight, or is it a result of a design flaw?
Landing accidents and inherent dangers of such action is common in virtually all aircraft and yet, such unfriendly characteristics alone is never a basis for claiming something to be obsolete - as practically no plane is ever "user-friendly" enough. From what you are implying it seems your standards of "user-friendliness" would be more suited modern-day planes with tricycle landing gears and electronic aviation, rather than a WW2 era tail-dragger.
Again, according to your standards, the inherent problems infesting some late-war US airframes also never really went away. The "Ensign Eliminator", as the F4U called was the most notorious Navy aircraft of them all. Not to mention the tendency to violently enter a spin during stall situations, which made this plane also very "user-unfriendly".
So, if we situate a simular comparison between a Fw190D and a F4U-4, with simular characteristics in performance specs and yet, hugely sensitive and unfriendly stall characteristics, inferior high speed handling, and potential dangers of landing accidents - is that alone enough for some of us to say "The F4U-4 was an obsolete design by 1945"?
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Their is no way to confirm the 11,000 quoted by Flight Journal nor is their anyway to confirm the 5,000 other sources quote. The Fact remains the 109 is known for it's high landing accident rate by those who flew it.
Why should it be so? Okay let's actually try counting the actual reasons: It's a light-weight, relatively fragile airframe compared to bulky US planes. The problem of line of sight, is an inherent problem in all tail-draggers. The plane has a power-engine with a large amount of torque. Narrow landing carriages are always tricky.
Okay, which plane should we compare? How about the Spitfire? Simular performance specs, also a light built-plane with even narrower landing carriages than a Bf109?
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Willy Messerschmitt designed the 109 landing gear with the intention of remove the drag cause by thick wing chords needed for wide track landing gear. The retracting mechanism for the 109's main landing gear was located in the fuselage giving the 109 a narrower wing profile at the fuselage. Tradeoff for this is a narrowtrack landing gear which decrease's the planes stability on landing making things more difficult for the pilot. The landing gear was splayed in an attempt to add stability. Angling the Gear means to maintain landing gear strength you have to have thicker material which is more weight.
Again, simular thing with basically anything with landing gears narrower than something like a P-47. The Spitfire steadily increased the width of the landing gears throughout development, but it never was wide as any other plane. So that should probably suggest the same sort of troubles as the 109 - except obviously no one seems to be wanting to drag this to the surface, or much better, no-one in their sane mind claims the Spitfire was "obsolete" due to its character quirks.
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The 109 was known for weak landing gear, weak brakes, and an affinity for groundlooping. All these characteristics add up to increased landing and takeoff accidents.
How about this one? From a guy flew 109s decades after the Luftwaffe of the Third Reich went out of business?
"In summary, the Bf109G is a demanding aircraft to fly. The workload is high maintaining directional control on take-off and landing, although in flight the stalling and pitch characteristics are god. I would advise anyone planning to fly a '109 to get lots of experience and confidence in other large piston-engined taildraggers first.
However, if its peculiarities are understood and the take-off and landing limits are strictly adhered to the '109 can be operated perfectly safely. I treat the '109 with greater respect than anything else that I fly, but the challenge of trying to fly it well gives me greater satisfaction and enjoyment than probably any other aircraft. But I am never satisfied- I now have an ambition to fly an Emil; the Bf109E." - Dave Southwood
Initially every aircraft has about equal amount of characteristics flaws. How about the Mustang's flawed design to shed its wings upon high speed maneuvering? The gun-jammin at high Gs? The Typhoon's notorious fame for losing its tail? The difficulties of the Corsair in vicious stalls and dangerous landings?
Name any WW2 plane you think is "not obsolete", and I'll bet we can find a design flaw, or a characteristic quirk that manifests as a potential problem. P-38? P-51? P-47? You name it, we'll deliver.
But unlike you, we have no intention of branding a certain plane "obsolete" due to its problems. Because clearly we know how to draw a line in "relative inferiority" and "absolute obseleteness".
So far what have you come up with?
1) Problems in control stiffness
2) Characteristic quirks during landings and take-offs
Come on, name any plane which you consider "not obsolete" by your own standards. Let's see if it doesn't have any "character flaw" of its own.
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I would have thought so many "109" experts would have known this. I see what we have in reality is a bunch of "my plane is perfect and how dare you say it isn't".
You got it all wrong dude. It's "your plane sucks" vs "why is that?", which evidently the former doesn't seem to come with anything substantial.
Besides, this is an interesting question I'll bet - the landing/take-off difficulties was inherent in all 109s regardless of the timeline. How in the world is that going to help you prove that during a certain point the 109 started to become obsolete, when that 'problem' existed throughout the entire history of the airframe?
And that quirks, you seem to suggest, is such a problem that despite this plane(okay, granted the Bf109G-10 and K-4 shall not be used as a comparison. So, how about a G-6/AM or a G-6/AS? G-14?) gains superiority in number of performance attributes, it's still obsolete?
No, this is not about defending 'my plane'. It's about smacking a biased opinion that has no basis.