T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(4) Loss of fluid in both systems would render
aircraft unflyable
V.
Hydraulic Subsystems
Sg 7, fr 1
Landing Gear/
Doors Operation
A.
Landing gear system
Fig 9: Main Landing
1.
Major components
Gear (MLG) Major
Components
a.
Main landing gear (MLG)
Fig 10: Nose Landing
b.
Nose landing gear (NLG)
Gear (NLG) Major
Components
2.
Controls and indicators
a.
LDG GEAR UP/DN handle
(1) Location: left forward console, both
cockpits
(2) Purpose: UP raises gear, DN lowers gear;
(3) Function: to raise and lower landing gear;
light in handle indicates handle position and
gear position do not agree, one or more of
the gear are not down and locked, or up
selected and all doors not fully closed
b.
EMER GEAR handle
(1) Location: left forward console, both
cockpits
(2) Purpose: rotated clockwise and pulled, it
unlocks gear/doors and activates
emergency gear extension
CAUTION: If the landing gear is
emergency extended, hydraulic
pressure will not be supplied to the nose
wheel steering and the system will be
inoperative.
(9-98) Original
Page 27-67
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