T-45C TS, ADV & IUT ENG-09
Hydraulic System
c.
HYD 1 and HYD 2 filter indicators
NOTE: Each of these systems will be discussed in detail
LESSON NOTES
Use the T-45C cockpit and aircraft cutaway view wall charts to
identify controls, indicators, and components during this lesson.
Emphasize component functional descriptions.
II.
Hydraulic system no. 1 (HYD 1) 1.4.8.3.1
Sg 2, fr 2
Lesson Organization
A. Description:
HYDRAULIC SYSTEM
* T-45C hydraulic system overview
The HYD 1 reservoir supplies fluid to the HYD 1 engine-
* Hydraulic system
driven pump (EDP) that, in turn, produces hydraulic
no. 1 (HYD 1)
pressure to power the flight controls and general
* Hydraulic system no. 2 (HYD 2)
services.
* Emergency hydraulic system
* Aircraft interfaces
NOTE: Control of the rudder is strictly mechanical.
Sg 2, fr 3, p 1
Fig. 3: Hydraulic
System Block Diagram
(7 Overlays)
Figure 3: HYDRAULIC SYSTEM BLOCK DIAGRAM
(9-98) Change 1
Page 9-6
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