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Chris Scott
4th Sep 2008, 14:52
Recent discussions on VC10 and Concorde threads lead me again to wonder: has any competent airliner-type ever failed on account of being too large for the job? A quick search has not revealed any previous thread, but let me know if there is one.

I can think of several big aircraft that were slow to catch on; and some that inspired short-fuselage versions to improve range, perhaps only until more power became available.

Let’s think back as far as the 1920s: the basic rules haven’t changed. You can include freighters; rotor-wings, if you can think of one; and aeroplanes that operate from water.

There is just one in my mind that might fit the bill. It’ll be interesting to see if anyone agrees with me. In the meantime, “after you…”

broadreach
4th Sep 2008, 15:21
Brabazon comes to mind.

Btw, the VC-10 is no mirage!

chornedsnorkack
4th Sep 2008, 16:25
What is the better plane - Brabazon or XC-99?

Capot
4th Sep 2008, 16:40
What about the Howard Hughes monster, Spruce Goose?

Genghis the Engineer
4th Sep 2008, 17:20
But what was the payload?

Big can be good, big with small payload is useless for most purposes - certainly most commercial ones.

G

bluelearjetdriver
4th Sep 2008, 17:54
What about Rosanne Barr and Dawn French?

starshift10
4th Sep 2008, 18:28
There were only 56 Boeing 377's Stratocruisers built.

nippysweetie
4th Sep 2008, 21:06
Soviets built a couple of An-225 Cossacks to transport bits of space kit and one may still be flying. Wingspan was not far short of 300ft. That count?

HighHeeled-FA
4th Sep 2008, 21:53
The title of this thread is a classic.

And I'm either immature or have just been flying far too much and am suffering withdrawal symptoms from ...

Chris Scott
4th Sep 2008, 21:59
Hi guys,

I'm not in charge of this discussion; ;) but, for what it's worth, I did say competent... I'm not sure that the Brabazon and Princess quite achieve that soubriquet, due primarily to lack of power?

The weakness in my question may be that "failed" is a subjective term. For me, the starshift10-quoted 56 Stratocruisers (about the same number as the too-small VC10) is getting darn close. I suppose you have to compare it with the opposition, to some extent? Was the Stratocruiser really too big, or were there other problems?

Keep them coming,
Chris

Question_Answer
4th Sep 2008, 22:22
I think I'm with High Heeled - slightly confused about use of the word "competent" and "failed" in the same question. Surely, competent = fit for purpose = not a failure?
However, reading into what Chris is getting at I wonder about the A340-600. A successful aircraft but perhaps too big to get easily into a few awkward fields that it otherwise is ideally placed to serve (e.g. Iberia over run at Quito)

Chris Scott
4th Sep 2008, 22:38
OK:

"Competent" = It achieves the original objective, or - if you like - "what it says on the tin".

"Failed" = Airlines buy far more of at least one smaller aircraft that is available for the same mission; is otherwise no more "competent" than the big one; and is no less expensive per passenger seat.

Hope this helps.

porch monkey
5th Sep 2008, 00:35
They may have only built 56 Startocruisers, but didn't they build plenty more for the airforce as refuellers/transports? Dunno about competent tho, plenty of examples of prop/engine failures on them.

411A
5th Sep 2008, 04:05
Well...as I've actually flown the Stratocruiser (although it had been just slightly ahhh, enlarged from the original design:rolleyes:), it was a very nice flying aircraft, but rather complicated electrically...and then there were the engines, Pratt&Whitney R4360's...very smooth in operation (almost turbine-like) however extremely complicated bits of machinery (a supercharger and a turbosupercharger), that consumed enormous quantities of oil (never mind fuel) and, on some models, were fitted with Curtis-Electric propellors, the complexity of which would glaze over the eyes
of the most attentive of mere pilots...

Stratocruiser, the operation of which, best left to the Flight Engineer....and an old experienced one, at that:}

Genghis the Engineer
5th Sep 2008, 09:22
Hi guys,

I'm not in charge of this discussion; ;) but, for what it's worth, I did say competent... I'm not sure that the Brabazon and Princess quite achieve that soubriquet, due primarily to lack of power.


From a number of fascinating conversations with the late Dick Stratton, who was flight engineer on the Princess (and went on to FTE some equally impressive projects) the basic problem with the Princess was that it was a big seaplane, at the time when the world was building runways around the world and seaplanes were becoming superfluous. As an aeroplane, and within the available technology of the 1950s, it seems to have been pretty effective.

Dick did tell me once that he believed he had the world record for simultaneous engine failures - 6 !

G

chornedsnorkack
5th Sep 2008, 17:34
Dick did tell me once that he believed he had the world record for simultaneous engine failures - 6 !

G

Dubious. There is that other ten engine plane, with hundreds of frames in service. What has been the absolute record for simultaneous engine failures out of those 6 turning 4 burning?

starshift10
7th Sep 2008, 14:47
Stratocruiser, the operation of which, best left to the Flight Engineer....and an old experienced one, at that

Interesting respose 411A. I know this is off thread, but I am sure it would be of interest
to readers - How many flight crew and cabin crew did the B377 carry and what were their titles/duties? I assume your flying on them was with an American carrier as your location is posted as the beautiful state of Arizona. :confused:

411A
7th Sep 2008, 17:25
How many flight crew and cabin crew did the B377 carry and what were their titles/duties?

Normal crew complement...eight.

Capt
F/O
F/E
Navigator

Purser
3 CC

Some Stratocruisers had a statemoom at the aft end, beds and all.

All of my flying was on freighters, however.

Chris Scott
8th Sep 2008, 17:40
Quote from Post #1:
…has any competent airliner-type ever failed on account of being too large for the job?
I can think of several big aircraft that were slow to catch on; and some that inspired short-fuselage versions to improve range, perhaps only until more power became available.
[Unquote]

411A, it looks as if your Stratocruiser may well be an exception that proves the normal rule: that airliners can never be too big, provided they are technically sound (and not underpowered or underfuelled).

My crew experience does not include the post-war large pistons, although their magic qualities hooked me into aviation as a boy, and I flew in several types as SLF. But think it’s safe to say that, by the mid-to-late 1950s, some of the big radials had achieved a state of power and sophistication that reintroduced alarming levels of unreliability. Did the Stratocruiser engines fall into this category? If so, was that why the Stratocruiser failed to sell in large numbers, compared to the DC6s and L1049s? Bars and bedroom areas do hint that the cabin might have been too large in volume, but is it possible that there was a payload or payload-range problem as well?

What sort of payload-range was available for your freighter (Guppy?), and was the P&W R4360 the same engine as the airliner and military transports had (unlike the Super Guppy)?

411A
1st Oct 2008, 12:39
But think it’s safe to say that, by the mid-to-late 1950s, some of the big radials had achieved a state of power and sophistication that reintroduced alarming levels of unreliability. Did the Stratocruiser engines fall into this category? If so, was that why the Stratocruiser failed to sell in large numbers, compared to the DC6s and L1049s? Bars and bedroom areas do hint that the cabin might have been too large in volume, but is it possible that there was a payload or payload-range problem as well?


The Stratocruiser piston engines were nearly at the top of the chain for complexity, topped only by the CurtisWright turbocompound series, which I also flew...on 1649 Constellations.

Excessive oil consumption was a rather large problem, but was overcome by a central fuselage oil tank, which could supply each 38 gallon engine tank.
Another problem was propellers...aircraft destined to Northwest were equipped with Curtis Electric props, which had hollow steel blades.
Corrosion was a big problem with these steel blades, often originating under the de-ice boot.
Blade departs...engine departs...goodbye airplane, was the scenario.
Later on, all of these Curtis props were retired, and the fleet standardized with the Hamilton Standard aluminum bladed propeller.
The Stratocruiser was quite a complicated electric airplane.
The landing gear was electrically operated, and sometimes, during gear retraction, all engine driven DC generators would trip offline, the ships battery would then be not able to complete gear retraction...at this point, if an engine was to fail, continued positive climb would be impossible...in fact, the battery may well have been quickly drained of capacity with a failed gear retraction, then no power was left for the feather pump, to complete feathering of the offending propeller...goodbye airplane.
Hydraulic boost was provided for the rudder, and this was the beginning of rudder boost problems for Boeing...which later on carried over to the B707 and B737.
Not many were built mainly because there were not that many customer airlines that a) could have afforded to operate the beast, b)needed it for very long range flights, and c)had the expertise to keep this mechanical nightmare in the air.

Yes, I flew the piston-powered Guppy.
Can't remember the payload possible, but the airplane was restricted to 250 knots TAS, mainly to keep the quite large front end, just above the FD, from structurally failing...which it did on one occation.
A very big 'dent'.
Not pretty....:ooh:

BelArgUSA
1st Oct 2008, 13:14
In my PanAm days, I flew with number of ex DC-6/DC-7 captains and flight engineers.
Even some B-377 guys as well...
xxx
One time, I asked them how to recognize a DC-6 from a DC-7.
On the ramp, easy, the DC-6 had 3 blades propellers, the DC-7 had 4 blades...
But when they are flying...?
xxx
They told me -
"If one is landing with a feathered engine, has to be a Seven...!"
Apparently, the R-2800 was a great engine, but the R-3350 was another story.
xxx
:)
Happy contrails

Torquelink
1st Oct 2008, 15:21
At the risk of interrupting this exchange of nostalgia but getting back on-thread - how about the 757-300 and 767-400ER. Both competent stretches of existing competent aircraft. Both sold in handfuls?

Would also argue that while the A340-600 may be technically competent it's not as technically and, most importantly, financially competent as the 773ER.

411A
2nd Oct 2008, 00:11
A simple innovatory solution to a long standing aviation problem!


There was a mechanical gust lock, just at the rear of the pedistal, as I recall, that worked OK.
Hot, on sunny days?
Oh yes, in spades.
But welcome on colder days, as the FD heating was practically non-existant.
The Stratocruiser was a 'Flight Engineers dream'...they 'operated' it, the pilots just more or less pointed it in the right direction.:}
Pilots seat entry was from the outboard side, plenty of room.
And as for nose wheel steering, that big round tiller was designed for a ship, I think..
The Guppy conversion was stretched twenty feet, all behind the wing.
It needed to be landed three-point, least you dragged the aft end on the pavement.
The first turbine powered version, the Guppy 201, powered by Allison 501-D22C engines (similar to the Electra and C-130) pumped out 4300 SHP...the airplane, dispite its size, was a good performer.
Sadly, during certification testing, one crashed at Edwards. I lost two very good friends that day, the Chief Pilot and Chief Flight Engineer.
Pitch lock on one of the Aeroproducts propellors at rotation ain't good.:{

All in all, the 'ole Startocruiser was a delight to fly.

Chris Scott
2nd Oct 2008, 11:40
Fascinating, 411A (and others). Just for the record, the standard entry to the pilots’ seats on the VC10 is also from the outside. Is that why the fuel flows are higher than on the B707/KC135? ;)

Looks like 411A has established the B377 Stratocruiser as a strong candidate. But we don’t yet have a definitive reason for it not selling in larger numbers. Was it simply too big? Or was it the technical impracticality and unreliability?

Quote:
Not many were built mainly because there were not that many customer airlines that a) could have afforded to operate the beast, b)needed it for very long range flights, and c)had the expertise to keep this mechanical nightmare in the air.
[Unquote]

Bearing in mind that this was an era of unreliability, particularly in the propulsion compartment, maybe the B377 was competent for its day?


Moving on reluctantly from this delicious piston nostalgia, can I propose another candidate from a different era? Suspect that 411A might prefer the sophisticated Lockheed, but mine is the VC9.

Was it too big a jump in size from the Viscount?
Am currently hampered by the limitations of a dial-up connection, but don’t think the (one?) structural failure and consequent pressurisation restrictions come soon enough to affect sales in the early years.
Don’t recall any initial problems with the excellent RR Tyne, although the waves of de-synchronous vibration that slowly swept the length of the cabin could be unnerving.
Was its payload-range sufficient?
Was it eclipsed from 1965 by the much smaller − and only slightly faster − BAC OneEleven because of the latter’s passenger appeal, because it was too big, or for some other reason?

Any Vanguard drivers/engineers out there?

Rainboe
2nd Oct 2008, 12:23
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