FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 27 > Section 1123 - Exhaust piping
section 27.1121 |
section 27.1141

(a) Exhaust piping must be heat and corrosion resistant, and must have provisions to prevent failure due to expansion by operating temperatures.
(b) Exhaust piping must be supported to withstand any vibration and inertia loads to which it would be subjected in operations.
(c) Exhaust piping connected to components between which relative motion could exist must have provisions for flexibility.
[Amdt. 27-11, 41 FR 55470, Dec. 20, 1976]
  
Current page: FARs > Part 27 > Section 1123 - Exhaust piping
section 27.1121 |
section 27.1141

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