Now to the hypothetical:
Are there any other methods (aside from the blacklight) to measure/test hydrocarbons? The byproducts we form may not all be visible by the black light but how does that compare to the contaminants potentially placed into the tank from cleaning (we can't all be perfect)? We are given a specific amount of acceptable hydrocarbons (less than 2.5 mi i think) but how can we determine whether or not a tank or inspection removes that much? In other words, how effective is the O2 clean process for non-visible hydrocarbons (although it is obviously safer than not cleaning)? These are questions which I would really like some technical answers to that I haven't found too much in agency literature. I wouldn't mind calling PSI/PCI or any of the other agencies if no one can come up with where to look...
There are ways to pretty conclusively measure for hydrocarbon residue but they are too expensive to utilized in our arena. That's why following the cleaning protocol is so important. If you've followed all the steps carefully there shouldn't be any testing necessary, though the protocol does call for visual inspection in visible and ultraviolet along with smear and water break tests.
In the world of scuba, no amount of detectable hydrocarbons are acceptable when oxygen servicing equipment, if you find any when testing the standard is to start over again from scratch. NASA testing is more intense and they will allow some hydrocarbons in some instances.
How effective is the scuba oxygen cleaning protocol when measured against an absolute? I don't know the answer to that, the folks at PSI might be able to give you an answer.
Here is some extracted information from one NASA unit that might be of interest...
NASA Glenn Research Center Glenn Safety Manual
Chapter 5 - Oxygen
BMS Document GRC-M8300.001
Revision Date: 2/05
5.15 APPENDIX B - CLEANLINESS SPECIFICATION FOR GASEOUS/LIQUID OXYGEN SERVICE IN GLENN TEST FACILITY SYSTEMS
5.15.2 Requirements
Materials: All materials used shall have been previously determined to be compatible with oxygen and should be widely accepted throughout the aerospace industry. All materials shall be approved by the Glenn Assurance Management Office and/or the Area Safety Committee.
Lubricants: Liquid oxygen is a powerful oxidizing agent, so a petroleum-based lubricant must not be used. Special lubricants such as the fluorolubes or the perfluorocarbons, which have been tested and found suitable for oxygen service, may be used. All lubricants shall be approved by the Glenn Assurance Management Office and/or the Area Safety Committee.
Cleanliness: All component parts shall be free of burrs, chips, scale, slag, or foreign matter and shall be cleaned prior to assembly. Inspection for cleanliness shall consist of the following.
Visual inspection: Visible contamination shall require recleaning of the surface. Discoloration due to welding will be permitted, providing no scale or rust is associated with the discoloration. Visual inspection aided by an ultraviolet light source (3200 to 3800 angstrom wavelength) shall show no evidence of fluorescence from contamination.
White cloth inspection: Surfaces shall be rubbed in two directions with a clean, lint-free white cloth. Any evidence of oil, rust, stain, scale, or foreign matter will be cause for rejection. The cloth may be examined under natural or ultraviolet light. Use of ultraviolet light (3200 to 3800 angstrom wavelength) shall show no evidence of fluorescence from contamination.
Solvent rinse: Sufficient quantities of solvent rinse shall be used so as to yield 100-milliliters/square foot of internal surface area. The solvent rinse shall be performed by either sloshing or agitating the fluid around the inside surface of the components and straining it through a 5-micron, or finer, filter. Further instructions are found in ASTM MNL 36, January 2000.
CONTAMINATION LIMITS
a. Solid Particles
Particle size, microns Maximum number per 100-ml sample (Millipore test)
<100 = Unlimited
100 to 250 = 93
251 to 300 = 3
>300 = 0
b. Fibers
Fiber length (up to 25 um diameter), microns Maximum number of 100-ml sample (Millipore test)
0 to 500 = 20
501 to 1000 = 3
1001 to 1875 = >1875 None
c. Nonvolatile residue
Maximum residue, mg/square foot 1.0
d. Hydrocarbon limit
Ultraviolet Light = No fluorescence
Infrared spectrophotometer = 5 ppm hydrocarbon
e. Total solids and fibers
25 mg/square foot (maximum)
Cleaning: Cleaning shall consist of the typical cleaning, rinsing, and drying procedures used throughout the aerospace industry:
a. Cleaning shall consist of a thorough flushing of all surfaces with aqueous detergent solutions.
b. Rinsing shall consist of a thorough rinsing and flushing with de-mineralized water, followed by rinsing and flushing with isopropyl alcohol.
c. Drying shall consist of blowing dry with filtered gaseous nitrogen or oil-free air.
Inspection: Inspection of cleaned components shall be performed by the solvent rinse method where possible. (This is generally done during the final cleaning stages and just prior to the drying operation.) The solvent shall be used at a rate of 100 milliliters per square foot of internal wetted surface area. (For all components having less than one square foot of internal wetted surface area, use 100 ml of solvent.) The solvent rinse shall be performed by either sloshing or agitating the fluid around the inside surface of the component to ensure dislodgment of particles. The rinse shall be poured through a filter sized to detect all particles greater than 100 microns. The assembled component, or any part thereof, shall be recleaned if it fails to pass the inspection(s).