Go Back  PPRuNe Forums > PPRuNe Worldwide > Australia, New Zealand & the Pacific
Reload this Page >

Merged: Qantas 747 Engine failure. Returns to SFO

Wikiposts
Search
Australia, New Zealand & the Pacific Airline and RPT Rumours & News in Australia, enZed and the Pacific

Merged: Qantas 747 Engine failure. Returns to SFO

Thread Tools
 
Search this Thread
 
Old 1st Sep 2010, 04:03
  #21 (permalink)  
 
Join Date: Oct 2003
Location: Gweriniaeth Cymru
Posts: 577
Likes: 0
Received 0 Likes on 0 Posts
Offchocks,

certain, have crawled in and out and around them often enough....check my location we also operate the same donk on our 744's.

Brgd's

N1 Vibes
N1 Vibes is offline  
Old 1st Sep 2010, 04:08
  #22 (permalink)  
 
Join Date: Feb 1999
Location: The Orion Arm
Posts: 118
Likes: 0
Received 0 Likes on 0 Posts
Yes, in the case of an LP turbine failure, it would take a lot to gum up the works enough to stop the fan in its tracks. I had assumed for the purpose it was a failure in the gas turbine HP core...but interesting that it wasn't contained nevertheless. Yes, I did forget about El Al, too. Was that non-shear bolt added to just the 747 or did it go across 76 etc as well...
deadhead is offline  
Old 1st Sep 2010, 04:46
  #23 (permalink)  
 
Join Date: Jul 2007
Location: in the classroom of life
Age: 55
Posts: 6,864
Likes: 0
Received 1 Like on 1 Post
Indeed

I wonder if that is his usual line for sim sessions too!
Jabawocky is offline  
Old 1st Sep 2010, 04:57
  #24 (permalink)  
 
Join Date: Jun 2001
Location: Great Southern Land
Age: 73
Posts: 511
Likes: 0
Received 0 Likes on 0 Posts
N1 Vibes

Yep you are correct, I made the misstake by looking at the colour of the cowl......the RB211's are grey not like CF's white.
Lousy colour in the photo, I guess I should have looked further back at the exhaust!
Offchocks is offline  
Old 1st Sep 2010, 05:41
  #25 (permalink)  
 
Join Date: May 2005
Location: Downunder
Posts: 290
Likes: 0
Received 0 Likes on 0 Posts
Yep, 4 holer, no sweat.
You wouldn't want one of those in a 2 holer somewhere around Christmas Island. (The Pacific one).

Last edited by skol; 1st Sep 2010 at 08:41.
skol is offline  
Old 1st Sep 2010, 06:14
  #26 (permalink)  
 
Join Date: Jan 2008
Location: sydney
Posts: 468
Likes: 0
Received 0 Likes on 0 Posts
I think more importantly some boys from Sydney Base will get a few days in SFO to repair this aircraft.
Nice to do something different to keep the job interesting. Just hope the boss gives them a day or 2 RnR before returning home.
But make sure the @sshole managers in Sydney don't make you sign a contract for the away from home conditions.

Is it just me or since QF shut down their engine overhaul shop these type of dramas seem to be a bit more common.
another superlame is offline  
Old 1st Sep 2010, 07:27
  #27 (permalink)  
 
Join Date: Jul 2008
Location: AU
Posts: 44
Likes: 0
Received 0 Likes on 0 Posts
Yes is a RR engine

All OJ_ aircraft have RB's on them

All OE_ aircraft have CF6's

It was OJP in the video I saw
BigGun is offline  
Old 1st Sep 2010, 07:30
  #28 (permalink)  
 
Join Date: Oct 2007
Location: gold coast QLD australia
Age: 86
Posts: 1,345
Likes: 0
Received 0 Likes on 0 Posts
Just caught the news on channel 9. It would appear that the engine blew a large hole in the casing, was on fire for at least half a hour,???? and the PAX thought they were all going to die. QFs safety record is now in tatters (please note dear folk, I am repeating it word for word) and it has never happened to any other aircraft or any other airline (Dear God) so there you go, learn something every day. It finished off with how wonderful the pilot was and the cabin crew, so I suppose there is some praise there, the rest is pure crap. Yes it happened, the turbine obviously shat itself, shame about the cowling, still three donks. NEXT!
teresa green is offline  
Old 1st Sep 2010, 08:11
  #29 (permalink)  
 
Join Date: Jul 2007
Location: Germany
Posts: 556
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by SMOC
Lucky it wasn't a fan blade.
On the contrary. Fan blades are contained. That is a certification criterion.

Fan-blade-off looks spectacular, but is less dangerous than a failure of IP of HP parts, which rotate at much higher rpm. Energy rises with the square of rpm, but only linearly with radius.


Bernd
bsieker is offline  
Old 1st Sep 2010, 08:33
  #30 (permalink)  
 
Join Date: Oct 2003
Location: Gweriniaeth Cymru
Posts: 577
Likes: 0
Received 0 Likes on 0 Posts
And of course fan blade weight = 10kg, turbine disc weight = 100 kg
N1 Vibes is offline  
Old 1st Sep 2010, 08:40
  #31 (permalink)  
 
Join Date: May 2005
Location: Downunder
Posts: 290
Likes: 0
Received 0 Likes on 0 Posts
bsieker,

You obviously didn't graduate in physics.
skol is offline  
Old 1st Sep 2010, 10:15
  #32 (permalink)  

Bottums Up
 
Join Date: Feb 2000
Location: dunnunda
Age: 66
Posts: 3,440
Likes: 0
Received 1 Like on 1 Post
Originally Posted by blueloo
So flames that appear to be flames are not actually flames?
The footage I saw on ABC TV News looked more like the sparks from an angle grinder (a bluddy big one though), rather than a fire with flames.
Capt Claret is offline  
Old 1st Sep 2010, 11:28
  #33 (permalink)  
 
Join Date: Nov 2007
Location: On the chopping board.
Posts: 929
Likes: 0
Received 4 Likes on 2 Posts
Totally agree that uncontained engine failures are definately not a "non event". Anyone who saw the damage caused by the American Airlines 767 that let go of it's HPT, or the N1 failure of BAW in Sydney a few years back would agree (both uncontained).

As with OJK recently, luck has played an incredible part again in this incident.

Last edited by Ngineer; 1st Sep 2010 at 11:47.
Ngineer is offline  
Old 1st Sep 2010, 13:39
  #34 (permalink)  
 
Join Date: May 2002
Location: GC Paradise
Posts: 1,100
Likes: 0
Received 4 Likes on 3 Posts
skol
bsieker,

You obviously didn't graduate in physics.
Fan blade-off containment is a design requirement that needs to be demonstrated before certification of any engine.

However, I understand that turbine disc failure is impossible to contain due to the extremely high energy involved without crippling weight penalties, so the disc is designed so it can't fail.

A turbine disc failure is a monumental event in airline operations.

So I rather think that bsieker is spot on with his comment...
FlexibleResponse is offline  
Old 1st Sep 2010, 13:56
  #35 (permalink)  
 
Join Date: May 2004
Location: Melbourne
Posts: 704
Likes: 0
Received 0 Likes on 0 Posts
Interesting recording from KSFO ATC courtesy LIVE ATC here. Everybody seems to handle the whole affair very calmly. Love the dangerous goods discussion - "Fuhgeddaboudit!"
VH-Cheer Up is offline  
Old 1st Sep 2010, 16:39
  #36 (permalink)  
 
Join Date: Mar 2005
Location: Europe
Posts: 258
Likes: 0
Received 0 Likes on 0 Posts
If the cockpit was as calm and professional as it sounded on the radio then job well done. I suspect it was.

Interesting to listen to an event such as this from somewhere other than the hot seat. Several transmissions were interpereted incorrectly including the mix up over pan/emergency.
AnQrKa is offline  
Old 2nd Sep 2010, 01:14
  #37 (permalink)  
 
Join Date: Jun 2007
Location: West of Point Byron!!!
Posts: 27
Likes: 0
Received 0 Likes on 0 Posts
If the cockpit was as calm and professional as it sounded on the radio then job well done. I suspect it was.

Interesting to listen to an event such as this from somewhere other than the hot seat. Several transmissions were interpereted incorrectly including the mix up over pan/emergency.
I beg to differ. My first thought's after listening to the ATC thread was that it sounded quite the opposite. Certainly some parts of it sounded quite in order but for the most part I disagree.

You might want to look into the FAA procedure in regards to PAN/EMERGENCY! Maybe take a look at the FAR/AIM document as to what their procedures are.
Gunger is offline  
Old 2nd Sep 2010, 02:00
  #38 (permalink)  
 
Join Date: Aug 2002
Location: sydney
Posts: 136
Likes: 0
Received 0 Likes on 0 Posts
skol is right.

Assuming the rpm is constant (maybe a big assumption), blade velocity increases linearly with radius. Energy is proportional to velocity-squared, so longer blades (fans) have energy increasing more than linearly with radius increasing.

Of course, this is oversimplified, longer blades (fans) often have much lower rpm than shorter ones (turbine blades)....
Groaner is offline  
Old 2nd Sep 2010, 02:14
  #39 (permalink)  
 
Join Date: Oct 2002
Location: In Frozen Chunks (Cloud Cuckoo Land)
Age: 17
Posts: 1,521
Likes: 0
Received 0 Likes on 0 Posts
Gunger - the atc recording i heard (the link to live ATC) had several transmissions "stuck" together (so there is some obvious repetition where they overlap). Also some transmissions clearly havent been recorded.


Sounded very calm/professional to me from the bits I heard.

As for this bit
You might want to look into the FAA procedure in regards to PAN/EMERGENCY!
...is largely irrelevant - as Australian registered aircraft are approved to use their Flight Admin manual and procedures. The Jepp WWT (world wide text) outlines a summary of the main changes which are relevant (in addition to company Route Manual).

From what we have seen over the years the USA /FAA /ATC dont have a particularly good track record with Radio Voice Procedure. Its all a bit care free really.
blueloo is offline  
Old 2nd Sep 2010, 02:14
  #40 (permalink)  
 
Join Date: Dec 2002
Location: Not Syderknee
Posts: 1,011
Received 1 Like on 1 Post
Video - Cockpit audio as QF74 handles engine failure - The Sydney Morning Herald
Audio again.
This link doesn't require a login.
rmcdonal is offline  


Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.