Raytheon Beech Baron E55 - Page 128

RBYtheon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
LUBRICA
TION
SCHEDULE
Chart
4
Lubrication
Chart
TC-1
and
After;
TE-1 and After
(Ref.
Figure
6)
TH-1 and
After
(Ref. Figures
7
and
8)
ITEM"
LOCATION LUBRICANT
INTERVAL
1.
Control
column
linkage
(18)’"
Detail
A
SAE
20
or
SAE
10W30
100
hrs.
2.
Controlcolumn
head(6)’0
Detail A
SAE
20
or
SAE
10W30 100
hrs.
3.
Control
column
aileron
link
(3)
’O
Detail A
SAE
20
or
SAE
10W30
100
hrs.
1.
Doorhandle(l)
Detail B
SAE
20
or
SAE
10W30 100
hrs,
2.
Doorlatch(2)
Detail
B
SAE
20
or
SAE
10W30
100
hrs.
3.
Doorlatch
(1)’
Detail B
SAE
20
or
SAE
10W30
100
hrs.
1.
Rudderpedals
(8)
Detail
C SAE
20
or
SAE
10W30
100
hrs.
1.
Landing
gear
motor
gear
box
(1)
Detail
D
MIL´•G-813229
IMW)hrS.
2.
Landing
gear
actuator
gear
box
(1)
Detail
D
MIL-PRF-2105
Grade
75
300
hrs.
NOTE:
Check
oil level
by
engaging
and
turning
the
emergency
hand
crank
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.
3.
Landing
gear
retract
arms
(14)
Detail
D
SAE
10W30
I
100 hrs.
4.
Nose
landing
gear
retract
arm
(1)’
Detail D
SAE
10W30
i 100
hrs.
1.
Mainlanding
geardoorhinges(l0)
Detail E SAE
20
or
SAE
10W30 100
hrs.
1.
Doorlatch
mechanism
(3)
13
Detail
F
Aeroshell
17
100
hrs.
2.
Doorhandle(l)l3
DetailF
Aeroshell
17
100 hrs.
3.
Doorhinges
(2)
Detail
F
MIL-M-7866
100
hrs.
1.
Rudder
trim tab
actuator
(1)
Detail G
MIL-G-23827
9
900
hrs.
or
5
jyears
2.
Rudder trim
tab
hinge
(1)
Detail
G
VV-L-BOOA
(Preferred)
100
hrs.
LPS-1
CRC
3-36
WD-40
3.
Ruddertrim
tab
clevis
(1)
Detail
G
VV-L-800A
(Preferred)
100
hrs.
LPS-1
CRC
3-36
WD-40
E23
SECTION
2
Dec
31f04Fags
43