SERVICE INFORMATION LETTER (SIL)

Repair and Overhaul Safety Information

For Components Used in High Pressure Oxygen Systems

Oxygen Cleaning Guide

OXYGEN – ATA CHAPTER 35

CAGE CODE: 04577

Introduction

This Service Information Letter (SIL) was released by Cobham (Carleton Technologies Inc.) to provide oxygen safety information that should be referred to when repairing Cobham oxygen components used in high pressure oxygen systems.

Visual cleanliness is not a sufficient criterion when dealing with oxygen components due to the hazards associated with contamination invisible to the naked eye. Components may collect contamination during storage, shipment or while installed on the aircraft. Therefore all contamination, seen or unseen must be removed prior to re-installation and system re-charge.

This SIL defines the cleaning requirements mandated by the air frame manufacturer and requires that all Cobham manufactured components installed on Boeing aircraft meet this cleanliness level.

It is the responsibility of the service provider and/or airline to ensure that all cleaning requirements are met.

This SIL will be incorporated into the next revision of all Chapter 35 CMMs under cage 04577.

A. SUBJECT

All Cobham oxygen components are manufactured to a Boeing specification. Referenced in all Boeing specifications is Boeing Part Specification BPS-O-100 which defines the cleaning requirements.

BPS-O-100 requires that all oxygen components in the high pressure stream meet the cleanliness level of Category 1. Components in Category 1 can be defined as components exposed to oxygen at pressures over 10 psi (68.9 kPa).

B. APPLICABILITY

This SIL is applicable to all Boeing aircraft where Cobham (Carleton) oxygen components are installed. Refer to the table below to review component application information.

Carleton P/NDescriptionModel Eligibility
1-6-05-19Regulator747-100
1-6-05-20Regulator747-100, -200, -300, -400, -SP, -SR,-100B, -100B SUD, -50D, -200B, -200C, -200F, -400D, -400F
15830ABRegulatorDC-9-31, -32, -32F, -33F, -34,-34F,-41,-51,-81,-82,-83,-87, MD-90-93, MD-88
15830LDiluter Demand Regulator737-100-200
15830MDiluter Demand Regulator737-200
15830PDiluter Demand Regulator737-200, 747-100, -200, -300
2239-0001-1ValveMD-11, DC-10-10,-10F,-15,-30,-30F,-40, MD-10-10F, -30F
2239-0001-3Valve767-200, -300, MD-10-10F, -30F
2239-0001-3ValveMD-11, DC-10-10,-10F,-15,-30,-30F,-40
2239-0001-5ValveMD-11
2279-001-1Valve747-200, -300, -SP, -100, -200B, -200C,-200F, -400, -400F
2279-002-1Valve727-200, 737-200, 747-100, -200
2279-003-1Valve727-200, 737-200
2279-003-11Valve737-200, -300. -400 757-200, 777-200, -300
2279-003-13Valve727-200, 757-200, -300, 737-200, -300, -500, -700, -800
2279-003-15Valve777-200, -300
2279-003-17Valve777-200, -300
2279-004-1Valve727-200
2279-005-1Valve727-200, 737-200
2279-006-1Valve737-200
B11174-1Valve737-200, -300, -400, -500, 757-200
B13500-1Valve737-200, -300
B14547-1Valve737-200
B19820-1Bleed Valve777-200, -300
B19820-3Bleed Valve777-200
B19925-1Regulator777-200, -300
B19925-3Regulator777-200LR
B42365-102 Cylinder and Hand Valve747, -400, -400F, 767-200, -300, -300F, -400ER 737-600, -700,-800,-900

C. REFERENCES

Repair and overhaul of all oxygen components must be done in accordance with document BPS-O-100, the applicable ATA Component Maintenance Manual issued by Cobham (Carleton Technologies Inc.) and MIL-PRF-27210 if needed.

The latest revision of Standard Practice Manual 20-90-01 may be used as a guide to meet the requirements of BPS-O-100.

DOCUMENT NUMBERDOCUMENT NAMEORDERING INFORMATION
BPS-O-100Oxygen System Components, Breathing, General Engineering RequirementsBoeing Commercial Aircraft Seattle, WA 98124 USA
MIL-PRF-27210Performance Specification, Oxygen, Aviator's Breathing, Liquid and GasUS Government Printing Office Washington, DC 20402 USA
20-90-01Standard Practice Manual Cleaning Process For Boeing Oxygen System ComponentsCobham (Carleton Technologies Inc.)

Reference the tables below to identify which CMM to use for a particular Cobham top assembly part number.

Carleton P/NApplicable ATA CMMCarleton P/NApplicable ATA CMM
1-6-05-1935-11-052279-003-1335-09-03
1-6-05-2035-20-012279-003-1535-09-03
15830AB35-11-132279-003-1735-09-03
15830L35-11-112279-004-135-09-01
15830M35-11-112279-005-135-09-01
15830P35-11-072279-006-135-09-01
2239-0001-135-12-01B11174-135-09-03
2239-0001-335-12-01B13500-135-09-03
2239-0001-335-12-01B14547-135-09-05
2239-0001-535-12-03B19820-135-11-06
2279-001-135-09-01B19820-335-11-06
2279-002-135-09-01B19925-135-22-01
2279-003-135-09-01B19925-335-22-01
2279-003-1135-09-03B42365-135-22-02

D. ACTIONS

Repair and overhaul of oxygen components – all components requiring repair, overhaul or testing shall be fully disassembled, thoroughly cleaned IAW BPS-O-100, reassembled and tested in accordance with the applicable CMM.

Proper cleaning removes particles, films, greases, oils, loose scale, corrosion, dirt and dust which could prevent interference with component function and will reduce contamination which could cause ignition. It can not be assumed that components removed from an aircraft meet required cleanliness requirements due to system level contamination, general usage and handling. In-situ cleaning or flow through cleaning is not effective and therefore not recommended under any circumstances.

E. INSTRUCTIONS

IF THE APPROPRIATE LEVEL OF CLEANLINESS CANNOT BE ACHIEVED PER BPS-O-100 OR MAINTAINED WITHIN THE REPAIR/OVERHAUL FACILITY HANDLING THIS UNIT, IT IS STRONGLY RECOMMENDED THAT ALL SERVICING BE REFERRED BACK TO THE ORIGINAL MANUFACTURER.

A CLASS 100,000 CLEAN ROOM IS STRONGLY RECOMMENDED FOR TESTING AND/OR DISASSEMBLY PROCESSES. A CLASS 10,000 LAMINAR FLOW BENCH IS STRONGLY RECOMMENDED FOR ASSEMBLY PROCESSES.

  1. Prior to any repair, overhaul or test, use the appropriate CMM to disassemble and clean the oxygen component per BPS-O-100. The end result of proper cleaning for a Category 1 component shall be a non-volatile residue (NVR) level of 3.0 mg. or less per square foot.
  2. Inspect per requirements of BPS-O-100:
    • (a) Determine that contamination levels meet the 3 mg./sq. ft requirement as well as records showing the cleaning and filling process are statistically in control.
    • (b) Used cylinders (cylinders having been operated, not disassembled and not having been empty) must have their gas tested for MIL-PRF-27210 compliance as well as a visual inspection for cleanliness.
    • (c) Any cylinder being modified, hydrostatically tested or depleted requires Category 1 contamination measurement, gas inspection for the MIL-PRF-27210 requirement and a visual inspection for contamination.
  3. Data sheets shall be furnished with each shipment showing that compliance to the requirements of BPS-O-100 for each lot was met. The data sheet will show the quantitative results of compliance.

Data Sheet Requirements

Inspection data sheets shall be maintained to include the following information:

Per BPS-O-100 the airframe manufacturer has the right to audit for compliance.

Filling an Empty CFFC Cylinder and Valve Assembly

Ensure the CFFC Oxygen Cylinder & Valve Assembly is adequately secured without causing damage to the composite pressure vessel. Prepare the fill setup as shown in the appropriate CMM after verifying that it has been thoroughly cleaned, inspected, and purged with gaseous oxygen (refer to the CMM for cleaning/inspection requirements), has a valid hydrostatic test date on the composite pressure vessel, and that the CFFC Oxygen Cylinder & Valve Assembly with hand valve installed has been proof pressure tested since disassembly/re-assembly. Any cylinder that has been modified, hydrostatically tested, or depleted requires Category 1 contamination measurement IAW BPS-O-100. Oxygen gas inspection for all used cylinders shall show compliance to MIL-PRF-27210 for odor, purity and moisture. This includes cylinders that are unused, modified, hydrostatically tested and or previously depleted. Results shall be recorded on the data sheet.

F. CONTACT CARLETON TECHNOLOGIES

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