14 C.F.R. § 23.1111 Turbine engine bleed air system.
Title 14 - Aeronautics and Space
For turbine engine bleed air systems, the following apply: (a) No hazard may result if duct rupture or failure occurs anywhere between the engine port and the airplane unit served by the bleed air. (b) The effect on airplane and engine performance of using maximum bleed air must be established. (c) Hazardous contamination of cabin air systems may not result from failures of the engine lubricating system. [Amdt. 23–7, 34 FR 13095, Aug. 13, 1969, as amended by Amdt. 23–17, 41 FR 55465, Dec. 20, 1976]
Title 14: Aeronautics and Space
PART 23—AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES
Subpart E—Powerplant
Induction System
§ 23.1111 Turbine engine bleed air system.
