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WINGS (Cont'd)
NOSE GEAR (Cont'd)
12.
Leading
edge
wiring
and plumbing
4.
Doors and
linkage
13.
Flaps and actuators
5.
Shimmy
dampener
14.**Wing bolts
6.
Retract
mechanism
15.
Aileron and trim tab controls
(when
installed)
16.
Boost pumps
*MAIN GEAR AETRACTION
17.
Fuel
strainers
18.
Aileron
trim tab end play inspection
l.
Doors
2.
Position
lights
NACELLES
3.
Warning horn
4.
Uplock
cable tension
1. Skin
5.
Uplock
rollers
2.
Structure
6.
Safety
switch
3.
Electrical
wiring
and equipment
7.
Emergency
extension
4.
Propeller
accumulators
8.
Downlock
tension
5.
Plumbing
9.
Strut fluid
level
6.
Engine
controls
10.
General
operation
MAIN GEAR AND BRAKES
*NOSE GEAR RETRACTION
1.
Brake lining
and dises
1. Doors
2.
Wheels and tires
2.
Visual indicator
3.
Landing gear strut
3.
Nose gear up tension
4.
Gear doors
and
linkage
4.
Assist step
(when
installed)
5.
Retract
mechanism
5.
Downlock
tension
6.
Strut fluid
level
NOSE GEAR
GENERAL
1. Wheel and tire
2.
Landing
gear strut
1. Aircraft
cleaned and serviced
3.
Retract
rod ends
2.
Aircraft
lubricated
*
First 100 hours and every
200
hours thereafter,
place the airplane
jacks
and cycle the
landing
gear
while
checking to ascertain
that the position
lights
switches
operate
in conjunction
with
the landing gear position.
Check
condition
and operation
of
complete
landing gear system.
**
Check
the
wing
bolts for
proper torque at the first 100 hour inspection
or at the
first
100 hour inspection
after a
wing
has
been
installed.
Refer to the
Shop Manual for
torque
values
and procedures.
C3
7-3
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Troubleshooting
