APU Bleed and Electrical Load (max altitude)
10,000 feet
APU Bleed Load (max altitude)
17,000 feet
APU Electrical Load (max altitude)
41,000 feet
Use of Assumed Temperature Prohibited when…
Define “Icing Conditions” on the Ground
Ground Icing Conditions exist when
• The OAT is 10ºC or below; and
• Visible moisture in any form is present; or
• When operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on engines or nacelles
Define “Icing Conditions” in flight
Icing Conditions exist in flight (climb and cruise) when:
• The TAT is 10ºC or below; and
• The SAT is -40ºC or above; and
• Visible moisture in any form is present (clouds, fog, rain, snow, sleet, ice crystals)
Engine anti-ice must be on prior to and during descent in all Icing Conditions, including temperatures below -40ºC.
Minimum Oil Temperature for Engine Start
-40ºC
Minimum Fuel Temperature for Engine Start
Must not be less than -43ºC or 3ºC above the fuel freezing point temperature, whichever is higher
Engine Ignition Use in Flight
CONT for Moderate to Heavy Rain, Hail or Sleet
FLT for Severe Turbulence
Minimum Oil Temperature for Takeoff
31ºC
APU bleed valve must be closed when (3 items)
APU Start Attempts
After three consecutive aborted start attempts, a 15-minute cooling period is required.
Engine Ignition Use on Ground
Engine Starter Limits
Aborted Engine Start Parameters
APU as Bleed Air Source
Run the APU for two full minutes before using it as a bleed air source
Minimum Oil Pressure for Takeoff
17.4 psid