AM.III.B.K8

From the FAA library

• Pilot Guide: Flight in Icing Conditionsp. 21
  Chapter 3. ICING EFFECTS, PROTECTION, AND DETECTION › 3-5. ANTI-ICING SYSTEMS › a. Bleed Air Systems

  Bleed Air Systems. Bleed air systems are used for larger areas of the aircraft, such as engine nacelles and wing leading edges. Bleed air from turbine engines is the most common type of anti-icing protection for engine nacelles ... anti-ice systems on, higher-than-normal power settings may be required to ensure sufficient bleed air is being supplied to the anti-ice system, and to prevent engine surges/stalls (see the particular AFM for the appropriate settings.) In addition…

• Pilot's Handbook of Aeronautical Knowledgep. 7-30
  Chapter 7: Aircraft Systems › Heating System › Bleed Air Heating Systems

  higher-pressure air outside the chamber would travel into the chamber and out the exhaust. Bleed Air Heating Systems Bleed air heating systems are used on turbine-engine aircraft. Extremely ... compressor bleed air is ducted into a chamber where it is mixed with ambient or re-circulated air to cool the air to a useable temperature. The air mixture is then ducted into the cabin. This type of system contains…

• 14 CFR Part 135 — Operating Requirements: Commuter and on Demand Operations and Rules Governing Persons on Board Such AircraftOpen
  14 CFR Part 135, Appendix A to Part 135—Additional Airworthiness Standards for 10 or More Passenger Airplanes

  means to indicate to appropriate flight crewmembers the functioning of the powerplant ice protection system. 49. Turbine engine bleed air systems. Turbine engine bleed air systems of turbopropeller powered airplanes must be investigated to determine— (a) That no hazard ... duct can occur anywhere between the engine port and the airplane bleed service; and (b) That, if the bleed air system is used for direct cabin pressurization, it is not possible for hazardous contamination of the cabin air system…