Cabinand Baggagecompartment - Raytheon BEECH BARON 58P Maintenance Manual

RaylIhean Aircraft
BEECH BARON 58P AND
BARON 58TC MAINTENANCE MANUAL
100-HOUR INSPECTION (CONTINUED)
D.
WINGS AND CARRY-THROUGH STRUCTURE (Continued) MECH INSP
L R
19.
NAVIGATION LIGHTS Check
for cracked
or
broken lenses and replace
bulbs
as necessary.
20.
LANDING LIGHTS Check
for
security and operation. Replace lens and
bulbs
as necessary.
21. FUEL
BOOST PUMPS AND FUEL LINES Check for condition, security
and leaks. Check lines for signs of chafing
or
cracks.
22.
FUEL SELECTOR VALVE Check for security, operation and leakage.
23.
FUEL STRAINERS Inspect and clean
as
outlined under the heading
ENGINE FUEL FILTERS AND SCREENS in Chapter 12-10-00 of this
Maintenance Manual.
24.
Perform the
INBOARD LEADING EDGE BAFFLED FUEL CELL FLAPPER
I
VALVE INSPECTION procedure. Refer to
Chapter 28-10-00.
E.
CABIN AND BAGGAGE COMPARTMENT
NIECH INSP
1.
SKIN Inspect skins for
deformation, cracks and loose
or
missing rivets. If
damage
is found, check adjacent structure.
2.
STRUCTURE Check for cracks and deformation.
Check
for loose
or
missing rivets and concealed damage.
3.
CONTROL CABLE SEALS (TJ-3 and After)
Check
for condition, security,
cleanliness and lubrication.
4.
CABLES AND PULLEYS
Check the flight
control
components,
cables and
pulleys. Replace control system components
(push rods, turnbuckles, end
fittings, castings, etc.) that have
bulges, splits, bends,
or
cracks. Check
control cables, pulleys,
and associated
equipment
for condition, attachment,
alignment,
clearance and proper operation. Replace cables that have
broken strands
or
evidence of corrosion. Check cables for
proper
tension.
5.
LANDING GEAR GEARBOX AND ACTUATING LINKAGE Check for
leakage,
wear,
condition and attachment. Check for unusual noise. Remove
I
the oil filler plug
and check oil level by engaging and turning the emergency
handcrank 1/2
turn to
determine that oil is
being picked
up on
the
worm gear.
The oil level should be maintained
no more
than necessary to
cover
1/2 of
the diameter of the
worm
gear. Install oil filler plug.
I
I
6.
PRESSURIZATION CONTROL VALVES (TJ-3
and After) Clean the cabin
pressurization
controller filter and orifice each 100 hours of operation and
the safety
valve filter and orifice each 500 hours of operation. Perform
a
functional test of the outflow and safety valves
every 500 hours of
operation
as
outlined in Chapter 21-30-00 of this Maintenance Manual.
7.
FLAP
MOTOR
AND
SHAFTS Check for condition, security and
wear
at
all
points.
Check cable housing for security and check jam nuts for
tightness.
~s
5-20-00
Jun
2 8 / 0 2 P a g e
209