Landing Gear Transfer Unit

Hydraulic System B pressure is available for raising the landing gear through the landing gear transfer unit. Hydraulic System B supplies the volume of hydraulic fluid required to raise the landing gear at the normal rate when all of the following conditions exist:

  • Airborne
  • No. 1 Engine RPM drops below a limit value
  • LANDING GEAR Lever is positioned UP
  • Either main landing gear is not up and locked.

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