T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
b.
Control surface components
(1) Slat panels
(2) Slat actuators
(3) Pressure/thermal relief valves
c.
Cockpit controls/switches/indicators
d.
FLAPS/SLATS lever
(1) UP: slats retracted
(2) 1/2 or DOWN: slats fully extended
e.
SLAT position indication: SLATS caution light
illuminated when slats not in selected position,
split slats, slat extension attempted above
217 KIAS, or when accelerating to above
217 KIAS with slats extended
Sg 8, fr 40
f.
Operating characteristics/limitations
Slats Normal
Operation
(1) Slats raised and lowered by HYD 1
powered actuators in each wing that drive
rods linked to the inner and outer slat
segments
(2) Normal operation of actuators maintains
slats symmetrical during extension/
retraction
(3) Backup synchro cable between actuators if
normal system fails
(4) No system to extend slats with HYD 1
failure
(5) Full extension of slats is 15 degrees
(6) Speed restriction for deployment: 200
KIAS
(9-98) Original
Page 27-82
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