Britpilot
Gear Lifter
- Joined
- Apr 23, 2002
- Posts
- 849
But regardless, we all know what most likely occurred.
No, not all of us. Some of us think it may be something less obvious.
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But regardless, we all know what most likely occurred.
On just about every page of this thread someone chimes in with "We shouldn`t speculate about this, wait for the official report". I`m here to tell you that we are pilots, and speculation is what we do. I have said it before: this web site is an electronic version of a ready room or pilot lounge. Pilots gather, pilots BS, pilots speculate. Get use to it and get over it. Retired Guy out....
But regardless, we all know what most likely occurred.
I haven't got the foggiest what occured, the initial report does not mention fuel starvation, they simply mention that thrust did not increase when commanded.
All indications were normal untill 600' AGL. There was a significant amount of fuel spilled on the ground, but thankfully no fire.
At this brief moment in time, it appears the pilots may have saved the day, the future will show if this holds true, but let's hope it does.
Wasn't there a 767 on the way to Hawaii a few years ago that had a dual engine flame-out due to some fuel pump/ transfer procedure or something? They re-lite of course.
Sorry Heavy but it is true. The Boeing FCTM states that the AT's should be used for all landings, hand flown or AL. This is a departure from thre B757/767. I don't have my manuals in front of me at this hour but I can quote Chapt. and verse out of the FCTM later today if need be.
Normal landing flaps are 30. Alternate landing flaps are 25. 1 EO flaps are 20 but if you have already gone to 30 and then lose the engine you can do a 30 flap landing. AL are done with 30 only. The airplane is capable of AL with an engine out. BTW, I don't any of this has anything to do with the BA accident.
Lots of conclusion jumping going on here.
First, you presume the engines failed, or were failing. There's nothing in the AAIB prelim that even hints at the engines failing. Not responsive to a thrust lever input is not the same as failing.
Second, where do you get the idea that the A/T system failed? The prelim clearly states that the A/T were calling for an appropriate increase in thrust that didn't materialize. The A/T is just a servo (or two) that moves the throttle lever to specified angle based upon the inputs from a bunch of different sources. If the power to drive the servos quits(which has not yet been proven in this case), then big deal, you just move the T/L by hand as you've always done. No A/T doesn't mean no engines.
Wth that said, an electronic glitch that impedes the ability of the engine EEC's to meter the proper amount of fuel based on the T/L angle is a different story.
Finally got to the books and the statement in the Boeing 777 FCTM, page 1.33, dated Oct 31, 2007 says the following. Auto Throttles; "Autothrottle use is recommended during all phases of flight. When in manual flight, autotrotlte use is also recommended, however manual thrust control may be used to maintain pilot proficiency." So there you have it. Not exactly carved in stone, but pretty darn close in Boeing speak.
Hope this helps more than it hurts.
Thanks for digging that up.
It's a bit different, as you pointed out, than the Boeing 75/76 guidance.
Does it specify that the A/T's must be disconnected prior to a manual landing ? Or does the 77 mirror the Bus in that they are armed and active until touchdown?
Just curious.
Computer system suspected in Heathrow 777 crash
experts have suggested that the simultaneous failure of both engines of the BA 777 which last week crash-landed at Heathrow must have been caused by a computer glitch, the Times reports.