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Boeing vs. Airbus

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Old 07-29-2011, 05:59 AM
  #61  
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Originally Posted by KC10 FATboy View Post
The A380 wing failed 3% BELOW the 1.5 X Ultimate Load requirement.
Premature structural failure is no criteria on which to judge an aircraft.

Did you hear about the tray table???!!
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Old 07-29-2011, 06:22 AM
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Originally Posted by Boomer View Post
Premature structural failure is no criteria on which to judge an aircraft.

Did you hear about the tray table???!!
And you get a free beret to wear and a lifetime supply of baguettes!
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Old 07-29-2011, 07:11 AM
  #63  
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Originally Posted by Spicy McHaggis View Post
Good thing no one would do that in a Boeing product...

oh wait...


Nice!!!!!
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Old 07-29-2011, 09:14 AM
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Originally Posted by sailingfun View Post
The Airbus series of aircraft from the A320 on only operate with the autopilot on with the exception of the transitions in TO and Landing where the aircraft is in Direct Law for a few moments below 50 feet.. You can shift the autopilot operation to the sidestick however you are still in CSS mode. (Control Stick Steering for Boeing guys, airbus calls it flying). In that mode you simply command a given pitch and bank angle for the aircraft. The autopilot maintains your pitch and bank commands regardless of airspeed or varibles. You can get the same effect on a Boeing by selecting CSS. The airbuses only revert to Direct Law if a major series of malfunctions occur that would disable the autoflight system.



Do you actually fly a Boeing ? You've proven that you know very little about Airbus already.

It's called Control Wheel Steering (CWS) in a Boeing. You can easily identify the buttons. They're labeled "CWS" ....

Too much union work and not enough flying Sailing ?

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Old 08-03-2011, 06:21 PM
  #65  
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Originally Posted by RCD73 View Post
Do you actually fly a Boeing ? You've proven that you know very little about Airbus already.

It's called Control Wheel Steering (CWS) in a Boeing. You can easily identify the buttons. They're labeled "CWS" ....

Too much union work and not enough flying Sailing ?

Hey RCD73;.... Would you mind showing me where that there "CWS" button is on a Boeing 757, 767 or 777. I've been looking all week-end and can't find 'em. Just flew a "Triple" back across the pond and none of us could locate that damn button ! Hmmm.

The only "CWS" I've ever seen on a Boeing was on the 737-200, which actually did have Control Wheel Steering.

I think you've been listening to the wrong group of friends or just don't know jack...

Good Luck in aviation, and G'Day
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Old 08-03-2011, 07:30 PM
  #66  
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Originally Posted by johnso29 View Post
Nice!!!!!
That was at Kai Tek, I think most all of the wingtip/engine contact here was due to the crazy turn on short final. Plenty of these type pics on airliners.net of all aircraft types at Kai Tek.

Does anybody no when they finally closed that place down?
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Old 08-03-2011, 07:31 PM
  #67  
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Wink

above post was referencing the pic, screwed up on the quote button.
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Old 08-04-2011, 06:29 AM
  #68  
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CWS thoughts FWiW.

Practical uses for CWS [Archive] - PPRuNe Forums
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Old 08-22-2011, 01:21 PM
  #69  
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the rivet spacing is nebulous since boeing uses larger stringers and Longerons than airbus. the majority of the Boeing problmes were Manually induced when the paint shops used box cutters rather than phenolic scrapers to remove the sealant at ovelaping joints when the airplanes were re-painted so that particular problem should be coming to a sreeching halt. I've been a Maint controller for 9+ years on the 737 and 4+years on the A320/A319, The problems are particular to each airplane and either make them a Joy or a Pain in the A%$!! The Airbus is more highly monitored for faults than the Boeing so a pilot telling me something that's not backed up BY a fault is rare. On the Boeings Faults could happen more through pilot Mishandling of the airplane and the systems than by real faults though they do happen. The airbus has more faults for monitoring and everything displayed as a fault is not necessarily what it seems to be. Rather than an Autopilot fault, the primary flight display indicates "1FD1" for a #2 FMGC/Autopilot being inop or "2FD2" for a #1 A/P-FMGC inop, Air Ground Faults are neither straight forward nor easily recognized, Generator faults take many forms as well due to the airbus philosopy of NOT turning them off when flutting down which causes the Gen Control Unit to fail on a more frequent basis than on a boeing. United used the sunstrand APS2000 apu where Continental uses the Honewell/Garret GTCP98 . The Airbus uses the APS3200 apu which i think after working with both is pretty near Excellent until compared with the B747-400 Pratt apu which is essentially the PT6-50 engine which is as GOOD as one can get in my opinion. Airbus and the boeing have their own characteristics Faults and Flaws
I would fly EITHER most anyhere in the world. It's Not the airplane, it's the operator that makes a difference.
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Old 08-26-2011, 08:28 AM
  #70  
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Kai Tak closed summer of 98. All kinds of airplanes dragged pods there on the checker board arrival. That particular runway has nothing to do with aircraft manufacturer......
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