T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(ii) Service required when red band
visible
Sg 6, fr 44
(b) HYD 2 reservoir indicator
Left Side External
Locator
(i)
Indicates quantity of HYD 2
reservoir
(ii) Quantity will vary according to
temperature of fluid and pressure
in system
(iii) Calibrated 0 to 340 cubic inches in
10 cubic-inch increments and
labeled every100 cubic inches
c.
Aircraft interfaces
(1) Inputs
(a) Electrical system: all WCP lights, HYD
2 RESET button, and system solenoid
valves supplied by 28 VDC essential
services bus
(b) Engine accessory gearbox: provides
mechanical power to drive two
hydraulic pumps
(2) Outputs
(a) HYD 1
(i)
Power supply pkg; Priority valve
directs pressure to:
•
Flight controls supplied
continuously
- Ailerons
- Stabilator
(9-98) Original
Page 27-63
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