T-45C TS, ADV & IUT ENG-09
Many components of the T-45C are hydraulically operated. The
ailerons and stabilator are totally dependent on hydraulic power.
Your knowledge of the hydraulic system is critical.
For the T-45C, you will describe the purpose and functional
characteristics of--and location of controls and indicators for--the
hydraulic system as well as the interfaces between the hydraulic
and other T-45C systems.
Engineering 09 will cover the following:
T-45C hydraulic system overview
Hydraulic system no. 1 (HYD 1)
Hydraulic system no. 2 (HYD 2)
Emergency hydraulic system
This lesson builds on information presented previously. In
particular, remember that the:
T-45C engine accessory gearbox drives the two hydraulic
T-45C hydraulic system supplies hydraulic pressure to the
ailerons, arresting hook, flaps, slats, landing gear, launch bar,
NWS, speed brakes, stabilator, and wheel brakes (including
Emergency Hydraulic System provides backup emergency
hydraulic pressure to the flight controls only