CS 25.1453 Protection of oxygen equipment from rupture

• ED Decision 2007/020/R found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

CS 25.1453 Protection of oxygen equipment from rupture ED Decision 2007/020/R (a) Each element of the system, excluding chemical oxygen generators, must have sufficient strength to withstand the maximum working pressures and temperatures in combination with any externally applied load, arising from consideration of limit structural loads that may be acting on that part of the system in service. (1) The maximum working pressure must include the maximum normal operating pressure, the transient and surge pressures, tolerances of any pressure limiting means and possible pressure variations in the normal operating modes. Transient or surge pressures need not be considered except where these exceed the maximum normal operating pressure multiplied by 1·10. (2) Account must be taken of the effects of temperature up to the maximum anticipated temperature to which the system may be subjected. (3) Strength demonstration using proof pressure and burst pressure coefficients specified in Table 1 is acceptable, unless higher stresses result when elements are subjected to combined pressure, temperature and structural loads. (i) The proof and burst factors in Table 1 must be applied to maximum working pressure obtained from sub-paragraph (a)(1) with consideration given to the temperature of sub-paragraph (a)(2). (ii) Proof pressure must be held for a minimum of 2 minutes and must not cause any leakage or permanent distortion. (iii) Burst pressure must be held for a minimum of 1 minute and must not cause rupture but some distortion is allowed. TABLE 1 <table border="1" cellpadding="0" cellspacing="0" width="454"><tr><td valign="top" width="189"><p><b>Systems Element</b></p></td><td valign="top" width="132"><p><b>Proof Factor</b></p></td><td valign="top" width="132"><p><b>Burst Factor</b></p></td></tr><tr><td valign="top" width="189"><p>Cylinders (i.e. pressure vessels)</p></td><td valign="top" width="132"><p>1·5</p></td><td valign="top" width="132"><p>2·0</p></td></tr><tr><td valign="top" width="189"><p>Flexible hoses</p></td><td valign="top" width="132"><p>2·0</p></td><td valign="top" width="132"><p>4·0</p></td></tr><tr><td valign="top" width="189"><p>Pipes and couplings</p></td><td valign="top" width="132"><p>1·5</p></td><td valign="top" width="132"><p>3·0</p></td></tr><tr><td valign="top" width="189"><p>Other components</p></td><td valign="top" width="132"><p>1·5</p></td><td valign="top" width="132"><p>2·0</p></td></tr></table> (b) Oxygen pressure sources and tubing lines between the sources and shut-off means must be – (1) Protected from unsafe temperatures; and (2) Located where the probability and hazard of rupture in a crash landing are minimised. (c) Parts of the system subjected to high oxygen pressure must be kept to a minimum and must be remote from occupied compartments to the extent practicable. Where such parts are installed within occupied compartments they must be protected from accidental damage. (d) Each pressure source (e.g. tanks or cylinders) must be provided with a protective device (e.g. rupture disc). Such devices must prevent the pressure from exceeding the maximum working pressure multiplied by 1·5. (e) Pressure limiting devices (e.g. relief valves), provided to protect parts of the system from excessive pressure, must prevent the pressures from exceeding the applicable maximum working pressure multiplied by 1·33 in the event of malfunction of the normal pressure controlling means (e.g. pressure reducing valve). (f) The discharge from each protective device and pressure limiting device must be vented overboard in such a manner as to preclude blockage by ice or contamination, unless it can be shown that no hazard exists by its discharge within the compartment in which it is installed. In assessing whether such hazard exists consideration must be given to the quantity and discharge rate of the oxygen released, the volume of the compartment into which it is discharging, the rate of ventilation within the compartment and the fire risk due to the installation of any potentially flammable fluid systems within the compartment. [Amdt 25/4]