FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 25 > Section 1123 - Exhaust piping
section 25.1121 |
section 25.1125

For powerplant and auxiliary power unit installations, the following apply:
(a) Exhaust piping must be heat and corrosion resistant, and must have provisions to prevent failure due to expansion by operating temperatures.
(b) Piping must be supported to withstand any vibration and inertia loads to which it would be subjected in operation; and
(c) Piping connected to components between which relative motion could exist must have means for flexibility.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-40, 42 FR 15044, Mar. 17, 1977]
  
Current page: FARs > Part 25 > Section 1123 - Exhaust piping
section 25.1121 |
section 25.1125

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