| Landing Gear The airplane has two main landing gear and a single nose gear. Each main gear
is a conventional two-wheel landing gear unit. The nose gear is a conventional steerable
two-wheel unit.
Hydraulic power for retraction, extension, and nose wheel steering is normally supplied by Hydraulic System A. A Manual Landing Gear Extension System and an altemate source of hydraulic power for nose wheel steering are also provided. The normal brake system is powered by Hydraulic System B. The Alternate Brake System is powered by Hydraulic System A. Antiskid protection is provided on both brake systems, but the Autobrake System is available only with the normal brake system. |