T-45C TS, ADV & IUT ENG-13
Flight Control System
D.
Electrical system
1.
28 VDC generator bus powers
a.
Aileron trim
b.
Rudder trim
c.
Trim indicators and stabilator position indicators
d.
Standby stabilator trim
2.
28 VDC essential services bus powers
a.
Primary stab trim
b.
Flaps/slats
c.
Emergency flaps
d.
Speed brakes
PROGRESS CHECK
Question 2 -- 1.4.19.2.1
If HYD 1 has failed, which flight control(s) will not remain
operative?
ANSWER: Speed brakes, slats
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(9-98) Original
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