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Aircraft Oxygen Bottles

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Ok Avbug, I know you know the answer to this one...

Given the information above, what are you going to do with STAL6's oxygen bottle?


Do you go with what the maintenance manual says?
- or -
Do you go with what the bottle manufacturer says?

Do you replace the bottle like the aircraft manufacturer states to do in their maintenance manual and buy another bottle?
 
Gatorman, I would have to replace the bottle, no doubt, but I would call the manufacture to see what can be done with the bottle after I've changed it out.

Stal6
 
Do you go with what the maintenance manual says?
- or -
Do you go with what the bottle manufacturer says?

Do you replace the bottle like the aircraft manufacturer states to do in their maintenance manual and buy another bottle?

Seems like you've added a lot of choices in there that weren't in STAL6's post. He didn't stipulate anything about what the bottle manufacturer stated, and you've given the same choice twice: compliance with the maintenance manual...but provided it as an "or" selection to appear as three choices.

We haven't even been provided with details as to which maintenance manual is in question, know nothing about additional STC's or AD's on the matter, or any other pertinent information. What would I do? I'd get more information, because whereas you've expanded on a question that didn't have information to begin with and introduced things that weren't there...we don't even know if STAL6's use of "maintenance manual" refers to the bottle manufacturer, aircraft manufacturer, or other data.

When I see maintenance manuals for aircraft on which I work, I see the airframe maintenance manuals, I see individual manuals for brakes by the brake manufacturer, and yes, even maintenance pubs for the oxygen system. Further, I may see manuals which need to be addressed separate from the airframe manufacturer because of optional or STC'd equipment...so rather than make a reply to your question which introduced material not even in the posters statement, how about we seek a little clarity?

The maintenance manual of the aircraft I'm currently working on says if the oxygen cylinder pressure drops below 50psi the cylinder must be replaced. It does not say what to do with it, so I would contact the manufacturer. I found that in ch. 12 servicing.

I know a lot of folks who use old O2 tanks for service bottles or shop air at reduced pressures. I've worked in several shops where WWII bottles wee still in use as portables for minor service work on the line. Personally I take compressed gasses and their handling and servicing quite seriously. A ruptured tank can do more than ruin your whole day.

This, of course, doesn't address the original posters comments or the discussion that thence ensued.
 
Gawd... with all that hot air, you should be a balloon mechanic.

Ya give the man a simple question and you provide the answer and he STILL doesn't answer it.

Years ago when I first came across this site, I had a lot of respect for you....


The answer is, you go with what the aircraft manufacturer's maintenance manual says. If it is not aircraft manual, you then go to the next level - who installed it.
Who ever installed it in the aircraft has to have gone by the bottle manufacturer's specifications.

Example:
If the bottle manufacturer tells you to replace it with a new one every 12 years and the aircraft manufacturer tells you to replace it every 10 years - you replace it every 10 years.
 
You failed to give a simple question. And you expected an answer to a items you made up and introduced. Are you not able to stick to the facts?

Fact: STAL6 didn't state which manual he used (aircraft manual could refer to any number of the).

Fact: STAL6 didn't state what other documents might be applicable.

Fact: STAL6 didn't state if he meant the airframe manufacturer or the bottle manufacturer.

Fact: We don't even know if the bottle that's in the aircraft is original equipment, or if additional documentation might apply.

The answer is, you go with what the aircraft manufacturer's maintenance manual says.

No. You go with the what the component manufacturer's approved publications and data have to say on the subject. The airframe manufacturer may or may not have anything to say about a bottle manufactured by someone else. Where a conflict exists on life limits, yes, the most conservative provision applies. However, simply because an item or appliance is installed in a particular airframe does not mean that the documentation or instruction ends with the airframe manufacturers data. It doesn't.

A common example is a powerplant, in which the airframe serves as the customer to the powerplant. Want engine data? Go to the engine manufacturer.

Want to know what to do with Cleveland wheels or BF Goodrich brakes? Go to their publications. Want to know about an airborne pump? You can't just look to the airframe manufacturer; yo go to the appliance or component manufacturers data, too. Which is precisely why I said we needed more information to answer a question which lacked any semblance of information in the first place.

If it is not aircraft manual, you then go to the next level - who installed it.

Absolutely NOT. The installer doesn't set the parameters for the product that's been installed. I can't install an item, for example, and then establish the airworthiness limitations and components life limits merely because I installed it.

If an item has been installed by a supplemental type certificate, then the STC should spell out either the limitations themselves, or point to the approved data where that information will be located. In many cases, STC's ammend what's published in the airframe manufacturer's data, requiring additional mx manuals, additional publications, and additional data.

I didn't complicate anything; the issue is more complex than a vague reference to a "maintenance manual" with the hope of gleaning somethin definitive from that reference alone. You know this. Or you should.

Who ever installed it in the aircraft has to have gone by the bottle manufacturer's specifications.

That really has no bearing on the life limits or other constraints which might be imposed by AD, STC, bottle or airframe official publications and data. That the installer may or may not have adhered to the bottle manufacturer's requirements is subject to what you see when you inspect the system, and whether the installer did it correctly or not, you're responsible for all previous work when you return that component to service. If you accept what's been done before and don't re-do it yourself, then you're now responsible for what others have done...regardless of whether they complied with any specific requirements or not.

Moreover, I've seen plenty of work done by mechanics and installers in the past which was incorect. Sometimes grossly so. As assumption that anybody properly complied in the past is a very dangerous one to make indeed. Especially when your fingerprints are now on the work, too. You know better than to assume.

What others did to comply in the past is also really quite irrelevant, so long as you're working on the product, because your job is to ensure that it's compliant now, and that when it leaves your hands, with your signature intact, it's 100% compliant with ALL relevant data. Not merely the airframe manufacturers, and not merely the bottle manufacturers. You may have additional relevant data with which to comply which doesn't apply to either one, such as the manufacturer of the regulator which is attached to the bottle etc.

Data is often applicable by effectivity only, segregated by serial number or part number. It may be applicable to one bottle, or one bottle type and not the next, and this information may be found in only one of the several sources discussed above. It's just not as simple as going to chapter 12 and being done with the matter...and it's CERTAINLY not as simple as referencing the installer of the equipment.

Years ago when I first came across this site, I had a lot of respect for you....

I suppose that's very sweet, but I really don't care.

Ya give the man a simple question and you provide the answer and he STILL doesn't answer it.

You didn't do that, of course. You provided a question regarding STAL6's post, then proceded to introduce things that weren't in his post in a nonsensical manner which served only to muddy what should have been a rhetorical question in the first place. It was neither a simple nor a correct question, and deserved only the reply it received.

You've argued throughout the thread falsehoods and assertions which are incorrect. You showed us references to "Uncle Fed" which weren't really accurate, difinitive, nor regulatory, and suggested throwing out the baby with the bathwater just to be on the safe side.

If you want to get specific, then let's do so. But use real data, and all the data, and quit making things up. You'll fare much better.
 
Gulfstream G-550
Maintenance Manual
Rev 10
Oct 15, 2007
Chapter/Section 12-19-00
Replenishing: Oxygen System
Servicing Page 301
1. A. (2) Aircraft Preparation
Note: Replace Oxygen Cylinder if Oxygen Pressure becomes less than 50 PSI.

Operating under FAR 91.409(f)(3)

That is all the AIRCRAFT maintenance manual says about it. The AIRCRAFT maintenance manual does not give any relief. So if the cylinder goes below 50 psi the cylinder MUST be replaced, no ifs ands or buts about it. It is that simple.
 
That is not correct as a general rule. Certain systems may have this as a requirement, but this is not a standard practice with all oxygen systems.

AC 43.13-1B Acceptable Methods Techniques, and practice - Aircraft Inspection and Repair

CH 9
Section 3. Emergency Equipment
9-51. Service Oxygen Cylinders Requirements
a.(1)(c) If the cylinder is completely empty DO NOT CHARGE. A EMPTY CYLINDER MUST BE REMOVED, INSPECTED,AND CLEANED BEFORE CHARGING.

With no other data available I would use this reference as standard practice.

STAL6
 
Oh NO!!!
You did not just quote out of the AC43.13!!!
 
Last edited:
Wait for it....
....listen....
....here it comes...
 
So long as you're quoting AC43.131B, regarding an earlier discussion about the use of soap solutions for leak detection:

(d) When oxygen is being lost from a
system through leakage, a sequence of steps
may be necessary to locate the opening. Leakage
may often be detected by listening for the
distinct hissing sound of escaping gas. If this
check proves negative, it will be necessary to
soap-test all lines and connections with a castile
soap and water solution or specially compounded
leak-test material. Make the solution
thick enough to adhere to the contours of the
fittings. At the completion of the leakage test,
remove all traces of the soap and water.

Again, 43.131B-2B is a standard practice fallback in lieu of specific direction from the manufacturer in approved documentation.

Whereas an airframe manufacturer may provide general guidance, often several bottles may be offered as choices, or a variety of bottles may have been installed at the factory, or in the field by means of STC or direct replacement. In such cases, the bottle manufacturers approved data is also relevant, as well as STC data, or any effective AD's.

43.13 does not preclude any of the above, and serves as a standard practice guide in lieu of other information.

With no other data available I would use this reference as standard practice.

As would be SOP. You have stipulated, however, that the only data available for your aircraft is the airframe manufacturers maintenance manual. You have not indicated if you have looked for maintenance publications for the bottle manufacturer. However, whereas the airframe manufacturer has required in approved documentation the removal and replacement of the bottle, other in-situ attention isn't relevant.

The assertion made throughout much of this thread that a bottle must automatically be removed or sent away for inspection when pressure drops below 50 PSI, or to zero, is incorrect.
 
The assertion made throughout much of this thread that a bottle must automatically be removed or sent away for inspection when pressure drops below 50 PSI, or to zero, is incorrect.

Since we have not heard from STAL6 in regards to his aircraft's maintenance manual and the disposition of the empty oxygen bottle....
AC 43.13-1B Acceptable Methods Techniques, and practice - Aircraft Inspection and Repair

CH 9
Section 3. Emergency Equipment
9-51. Service Oxygen Cylinders Requirements
a.(1)(c) If the cylinder is completely empty DO NOT CHARGE. A EMPTY CYLINDER MUST BE REMOVED, INSPECTED,AND CLEANED BEFORE CHARGING.

...applies.

Oh, and don't forget...
Again, 43.131B-2B is a standard practice fallback in lieu of specific direction from the manufacturer in approved documentation.
 

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