14 C.F.R. § 23.1453 Protection of oxygen equipment from rupture.
Title 14 - Aeronautics and Space
(a) Each element of the oxygen system must have sufficient strength to withstand the maximum pressure and temperature, in combination with any externally applied loads arising from consideration of limit structural loads, that may be acting on that part of the system. (b) Oxygen pressure sources and the lines between the source and the shutoff means must be: (1) Protected from unsafe temperatures; and (2) Located where the probability and hazard of rupture in a crash landing are minimized. [Doc. No. 27806, 61 FR 5170, Feb. 9, 1996]
Title 14: Aeronautics and Space
PART 23—AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
Subpart F—Equipment
Miscellaneous Equipment
§ 23.1453 Protection of oxygen equipment from rupture.
