Go Back  PPRuNe Forums > Flight Deck Forums > Tech Log
Reload this Page >

737 - Why is APU bleed connected to left pneumatic manifold

Wikiposts
Search
Tech Log The very best in practical technical discussion on the web

737 - Why is APU bleed connected to left pneumatic manifold

Thread Tools
 
Search this Thread
 
Old 11th Aug 2016, 11:56
  #1 (permalink)  
Thread Starter
 
Join Date: Mar 2008
Location: Vrsac
Age: 51
Posts: 28
Likes: 0
Received 0 Likes on 0 Posts
737 - Why is APU bleed connected to left pneumatic manifold

I just can not remember - but there must be a simple reason - why is that APU bleed is connected to left pneumatic manifold in Boeing 737?...

For the APU fuel feed I know it is connected to the left reservoir because there must always be some fuel in wing tanks (while center tank may be empty).

Thank you in advance
mirkoni
mirkoni is offline  
Old 16th Aug 2016, 18:32
  #2 (permalink)  
 
Join Date: Dec 2006
Location: belgium
Posts: 236
Likes: 0
Received 0 Likes on 0 Posts
Because the flight deck is connected to the left pack? The fuel could also be fed from the right wing tank, so I think it's more a design philosophy there.
Piper19 is offline  
Old 16th Aug 2016, 19:03
  #3 (permalink)  
 
Join Date: Jun 2012
Location: Glasgow
Age: 37
Posts: 88
Likes: 0
Received 0 Likes on 0 Posts
Just a theory..

Beacuse the HP ground connection is connected to the RH manifold?
(external services on A/C RHS)
Dougie_diesel is offline  
Old 17th Aug 2016, 16:36
  #4 (permalink)  
 
Join Date: Aug 2006
Location: France
Posts: 1
Likes: 0
Received 0 Likes on 0 Posts
Boeing philosophy I would say...
Everything "important" on the 73 is often on the "left" side ! Easy to remember : it is a captain's plane
lief is offline  
Old 17th Aug 2016, 18:36
  #5 (permalink)  
 
Join Date: Jun 2000
Location: last time I looked I was still here.
Posts: 4,507
Likes: 0
Received 0 Likes on 0 Posts
It's got to be connected to somewhere, and both is not necessary. Military thinking is left/right/left/right. Guess the lefts have it.
RAT 5 is offline  
Old 18th Aug 2016, 11:16
  #6 (permalink)  
Thread Starter
 
Join Date: Mar 2008
Location: Vrsac
Age: 51
Posts: 28
Likes: 0
Received 0 Likes on 0 Posts
Ground connection to the right manifold could be.
Is it maybe about always starting first the engine no 1, which is connected to the left manifold? Do they necessarily always start No 1 first?
mirkoni is offline  
Old 18th Aug 2016, 18:50
  #7 (permalink)  
 
Join Date: Jun 2000
Location: last time I looked I was still here.
Posts: 4,507
Likes: 0
Received 0 Likes on 0 Posts
Do they necessarily always start No 1 first?

Not in any airline I've worked for.
RAT 5 is offline  
Old 19th Aug 2016, 19:09
  #8 (permalink)  
 
Join Date: Apr 2008
Location: Nearer home than before!
Posts: 524
Likes: 0
Received 0 Likes on 0 Posts
Don't read too much into it. There is an APU bleed elbow on one side and the other is the external connection. In the middle is a low pressure air connection. It has to go somewhere!

Tradional to start right to left starting away from the steps/ pax. So the external air is on the side that means you start in an unusual order- as it's an unusual event ( well, on NGs it is)... So logical the layout is as it is.

Drawn up in 1965 from existing parts, it's quite a historical design anyway.
RVF750 is offline  
Old 23rd Aug 2016, 02:57
  #9 (permalink)  
 
Join Date: Oct 2013
Location: McHales Island
Age: 68
Posts: 180
Likes: 0
Received 1 Like on 1 Post
"there must be a simple reason"....... and there is


The APU bleed duct runs down the l/h side of the aircraft between the airframe skin and the rear cargo sidewall where there is plenty of room. Way too much redesign,weight gain etc involved to route the apu duct down the r/h side of the aircraft around/under/over the rear cargo door cutout. Hope this helps....


McHale.
Capt Quentin McHale is offline  
Old 23rd Aug 2016, 11:08
  #10 (permalink)  
 
Join Date: Oct 2013
Location: australia
Posts: 10
Likes: 0
Received 0 Likes on 0 Posts
BLEED AIR DUCTING --

As a licensed engineer on the b737 ----------- ,it is to do with the electric distrubition of the electrical system of the aircraft when you start the engines -------with no apu available ----------------------------- if you start the right first , if i remember correct--- some instrument transfers units to the capt side dont kick in automatically ----------------------------- on some aircraft starting procedure can depend on which engines are fitted with hydraulic pumps say the bae 146 for example -------------------- on the b737 , the external air cart is connected to the right side , boeing designed that the left engine is always --- normally---- started first-----------if you have apu air ,you wont it to go to the left engine and not to the right engine by having the bleed air crossfeed closed ----------------------------------- i have had one time the external starting air connection flapper failed and to get that engine started , external air cart was connected for start , and after starting the no 2 engine bleed and the crossfeed valve closed and both on mel [ not sure if there were pax ]
bigal cessna is offline  
Old 23rd Aug 2016, 16:41
  #11 (permalink)  
 
Join Date: Dec 2004
Location: Andalucia
Posts: 728
Received 0 Likes on 0 Posts
"there must be a simple reason"....... and there is
It's a Boeing, they have always done it that way why change ?
Wodrick is offline  

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are Off
Refbacks are Off



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.