Originally Posted by drooz
(Post 9758638)
Slightly off-topic but what are your airline's policy in regards to the 'flight altitude' when requiring a step climb? Would you set the highest flight level anticipated or would you start with the initial cruise level and then increase it as you climb further?
My company suggests entering the initial cruise altitude and then changing it as you climb, to avoid unnecessary 'off-scheduled descent' warnings in case you forget to climb. However this means that you suddenly get a quite annoying pressurisation change in the middle of the cruise when the pressurisation logic changes from 7.8psi diff to 8.35psi (i.e changing cruise level from FL360 to FL380). Would be interesting to know other operators thoughts around this. If operating as per Boeing FCOM and FCTM, set the highest expected level. The descent checklist item AIR COND & PRESS should be used to catch it if not climbed to planned maximum. Worst case scenario you get an UNSCHEDULED DESCENT, a non-issue in most airlines these days. |
Originally Posted by Derfred
(Post 9758811)
So you're saying the gauge gets it's data from the same source as the auto controllers?
From the book. Physical Description Each CPC (there are two) has these items: • Cabin pressure sensor • BITE instruction plate • Two-line LED display • BITE control buttons. And I'm not "saying" anything. Just quoting the book. The chapter on the cabin altitude panel does not go any further than shown. |
Slightly off-topic but what are your airline's policy in regards to the 'flight altitude' when requiring a step climb? Would you set the highest flight level anticipated or would you start with the initial cruise level and then increase it as you climb further? Skyjob and I agreed to disagree in that thread. Furthermore, airline operators differ in their interpretations of Boeing's recommendations, and implement their own SOP's accordingly. Please re-kindle that thread if you wish to discuss it further rather than take this one off topic... |
Originally Posted by stator vane
(Post 9759207)
The chapter on the cabin altitude panel does not go any further than shown.
That cabin altitude/diff gauge is an interesting one. I recall a 737 incident where they did a rapid depressurisation and emergency descent after a window crack, and subsequently found themselves at a low altitude with the cabin altitude above 40,000'. Very confusing. Except that the cabin altitude wasn't above 40,000' of course, it was way below sea level. You see, they didn't actually have a rapid depressurisation. So they closed the outflow valve manually as per the checklist, descended as per the checklist, and consequently pressurised the cabin way below sea level. That gauge is capable of reading negative, but it doesn't have negative graduations. The needle just moves anti-clockwise until it shows a high cabin altitude. No mention of that in the manuals either. Hmmm. |
Surely diff pressure gives a bit of a clue?
|
Clue to Cabin Altitude
As well as the Differential Pressure being a clue Hoppy, I am sure the lack of any Cabin Altitude Warnings (Visual & Aural) as well as the lack of a "Rubber Jungle" in the cabin would/should have told them something ?
|
Yes, you would think. It's a while since I read the report. It was bit of an embarrasing read from memory, but the interesting point I got out of it was the behaviour of the gauge.
|
There is also a modification available from boeing which gives a higher differential and a lower cabin altitude , not sure on the differential numbers , but the cabin stays at around 6500 . Could be one of those .
|
Originally Posted by Minorite invisible
(Post 9757366)
Carry on. |
All times are GMT. The time now is 16:05. |
Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.