Page 1 of 3
Part Number
Description
Alternate
filter element, lube
038088-08 P-1050
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
)
a
g
u
s
t
a
(
a
1
0
9
a
i
i
)
b
e
l
l
(
4
7
,
4
7
b
,
4
7
b
3
,
4
7
d
,
(
u
s
a
f
h
-
1
3
b
)
,
4
7
d
1
(
u
s
a
f
h
-
1
3
d
,
h
-
1
3
e
,
n
a
v
y
h
t
l
-
4
,
-
5
)
,
4
7
e
(
n
a
v
y
h
t
l
-
3
)
,
4
7
g
(
u
s
a
f
h
-
1
3
g
)
,
4
7
g
-
2
a
,
-
2
a
-
1
,
4
7
-
g
2
(
u
s
a
f
h
-
1
3
h
)
,
-
3
(
o
h
-
1
3
h
)
,
-
3
b
,
-
3
b
-
1
(
t
h
-
1
3
t
)
,
-
3
b
-
2
,
-
3
b
-
2
a
,
-
4
,
-
4
a
,
-
5
,
-
5
a
,
4
7
h
-
1
,
4
7
j
,
-
2
,
-
2
a
,
4
7
k
)
b
e
l
l
c
a
n
a
d
a
(
2
0
6
,
2
0
6
a
,
2
0
6
a
-
1
,
(
o
h
-
5
8
a
)
,
2
0
6
b
,
2
0
6
b
-
1
,
2
0
6
l
,
2
0
6
l
-
1
,
2
0
6
l
-
3
,
2
0
6
l
-
4
)
e
u
r
o
c
o
p
t
e
r
f
r
a
n
c
e
(
a
s
-
3
5
0
b
,
-
3
5
0
b
1
,
-
3
5
0
b
2
,
-
3
5
0
b
3
,
-
3
5
0
b
a
,
-
3
5
0
c
,
-
3
5
0
d
,
-
3
5
0
d
1
)
e
u
r
o
c
o
p
t
e
r
d
e
u
t
s
c
h
l
a
n
d
(
b
o
-
1
0
5
a
,
-
1
0
5
c
,
-
1
0
5
l
s
a
1
,
-
1
0
5
s
)
h
i
l
l
e
r
(
u
h
-
1
2
d
(
a
r
m
y
u
h
-
2
3
d
)
)
m
d
h
e
l
i
c
o
p
t
e
r
(
3
6
9
(
a
r
m
y
y
o
h
-
6
a
)
,
3
6
9
a
(
a
r
m
y
o
h
-
6
a
)
,
3
6
9
d
,
3
6
9
e
,
3
6
9
f
,
3
6
9
f
f
,
3
6
9
h
,
3
6
9
h
e
,
3
6
9
h
m
,
3
6
9
h
s
,
5
0
0
n
)
s
i
k
o
r
s
k
y
(
s
-
7
6
a
,
s
-
7
6
b
,
s
-
7
6
c
)
View Item »
Part Number
Description
Alternate
filter element, lube
038088-08
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
)
a
g
u
s
t
a
(
a
1
0
9
a
i
i
)
b
e
l
l
(
4
7
,
4
7
b
,
4
7
b
3
,
4
7
d
,
(
u
s
a
f
h
-
1
3
b
)
,
4
7
d
1
(
u
s
a
f
h
-
1
3
d
,
h
-
1
3
e
,
n
a
v
y
h
t
l
-
4
,
-
5
)
,
4
7
e
(
n
a
v
y
h
t
l
-
3
)
,
4
7
g
(
u
s
a
f
h
-
1
3
g
)
,
4
7
g
-
2
a
,
-
2
a
-
1
,
4
7
-
g
2
(
u
s
a
f
h
-
1
3
h
)
,
-
3
(
o
h
-
1
3
h
)
,
-
3
b
,
-
3
b
-
1
(
t
h
-
1
3
t
)
,
-
3
b
-
2
,
-
3
b
-
2
a
,
-
4
,
-
4
a
,
-
5
,
-
5
a
,
4
7
h
-
1
,
4
7
j
,
-
2
,
-
2
a
,
4
7
k
)
b
e
l
l
c
a
n
a
d
a
(
2
0
6
,
2
0
6
a
,
2
0
6
a
-
1
,
(
o
h
-
5
8
a
)
,
2
0
6
b
,
2
0
6
b
-
1
,
2
0
6
l
,
2
0
6
l
-
1
,
2
0
6
l
-
3
,
2
0
6
l
-
4
)
e
u
r
o
c
o
p
t
e
r
f
r
a
n
c
e
(
a
s
-
3
5
0
b
,
-
3
5
0
b
1
,
-
3
5
0
b
2
,
-
3
5
0
b
3
,
-
3
5
0
b
a
,
-
3
5
0
c
,
-
3
5
0
d
,
-
3
5
0
d
1
)
e
u
r
o
c
o
p
t
e
r
d
e
u
t
s
c
h
l
a
n
d
(
b
o
-
1
0
5
a
,
-
1
0
5
c
,
-
1
0
5
l
s
a
1
,
-
1
0
5
s
)
h
i
l
l
e
r
(
u
h
-
1
2
d
(
a
r
m
y
u
h
-
2
3
d
)
)
m
d
h
e
l
i
c
o
p
t
e
r
(
3
6
9
(
a
r
m
y
y
o
h
-
6
a
)
,
3
6
9
a
(
a
r
m
y
o
h
-
6
a
)
,
3
6
9
d
,
3
6
9
e
,
3
6
9
f
,
3
6
9
f
f
,
3
6
9
h
,
3
6
9
h
e
,
3
6
9
h
m
,
3
6
9
h
s
,
5
0
0
n
)
s
i
k
o
r
s
k
y
(
s
-
7
6
a
,
s
-
7
6
b
,
s
-
7
6
c
)
View Item »
Part Number
Description
Alternate
filter element, lube
038088-08 P-1050
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
)
a
g
u
s
t
a
(
a
1
0
9
a
i
i
)
b
e
l
l
(
4
7
,
4
7
b
,
4
7
b
3
,
4
7
d
,
(
u
s
a
f
h
-
1
3
b
)
,
4
7
d
1
(
u
s
a
f
h
-
1
3
d
,
h
-
1
3
e
,
n
a
v
y
h
t
l
-
4
,
-
5
)
,
4
7
e
(
n
a
v
y
h
t
l
-
3
)
,
4
7
g
(
u
s
a
f
h
-
1
3
g
)
,
4
7
g
-
2
a
,
-
2
a
-
1
,
4
7
-
g
2
(
u
s
a
f
h
-
1
3
h
)
,
-
3
(
o
h
-
1
3
h
)
,
-
3
b
,
-
3
b
-
1
(
t
h
-
1
3
t
)
,
-
3
b
-
2
,
-
3
b
-
2
a
,
-
4
,
-
4
a
,
-
5
,
-
5
a
,
4
7
h
-
1
,
4
7
j
,
-
2
,
-
2
a
,
4
7
k
)
b
e
l
l
c
a
n
a
d
a
(
2
0
6
,
2
0
6
a
,
2
0
6
a
-
1
,
(
o
h
-
5
8
a
)
,
2
0
6
b
,
2
0
6
b
-
1
,
2
0
6
l
,
2
0
6
l
-
1
,
2
0
6
l
-
3
,
2
0
6
l
-
4
)
e
u
r
o
c
o
p
t
e
r
f
r
a
n
c
e
(
a
s
-
3
5
0
b
,
-
3
5
0
b
1
,
-
3
5
0
b
2
,
-
3
5
0
b
3
,
-
3
5
0
b
a
,
-
3
5
0
c
,
-
3
5
0
d
,
-
3
5
0
d
1
)
e
u
r
o
c
o
p
t
e
r
d
e
u
t
s
c
h
l
a
n
d
(
b
o
-
1
0
5
a
,
-
1
0
5
c
,
-
1
0
5
l
s
a
1
,
-
1
0
5
s
)
h
i
l
l
e
r
(
u
h
-
1
2
d
(
a
r
m
y
u
h
-
2
3
d
)
)
m
d
h
e
l
i
c
o
p
t
e
r
(
3
6
9
(
a
r
m
y
y
o
h
-
6
a
)
,
3
6
9
a
(
a
r
m
y
o
h
-
6
a
)
,
3
6
9
d
,
3
6
9
e
,
3
6
9
f
,
3
6
9
f
f
,
3
6
9
h
,
3
6
9
h
e
,
3
6
9
h
m
,
3
6
9
h
s
,
5
0
0
n
)
s
i
k
o
r
s
k
y
(
s
-
7
6
a
,
s
-
7
6
b
,
s
-
7
6
c
)
View Item »
Part Number
Description
Alternate
flex drive assembly standard
Rosemount 2317M-2-79
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
2
s
,
n
2
4
a
)
View Item »
Part Number
Description
Alternate
flex drive assembly standard
Rosemount 2317M-2-61
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
2
s
,
n
2
4
a
)
View Item »
Part Number
Description
Alternate
headliner & duct system
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
g
a
f
n
2
4
a
a
e
r
o
n
o
m
a
d
)
View Item »
Part Number
Description
Alternate
headliner duct system
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
4
a
)
View Item »
Part Number
Description
Alternate
lamp, incandescent
GE 305
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
4
)
,
c
e
s
s
n
a
(
3
1
0
,
3
2
0
,
3
3
6
,
3
4
0
,
3
4
0
a
,
4
0
4
,
4
2
1
c
,
4
4
1
)
,
d
a
s
s
a
u
l
t
a
v
i
a
t
i
o
n
(
f
a
n
j
e
t
f
a
l
c
o
n
,
f
a
l
c
o
n
2
0
,
f
a
l
c
o
n
5
0
)
,
e
m
b
r
a
e
r
e
m
p
r
e
s
a
(
e
m
b
r
a
e
r
e
m
b
-
1
1
0
p
1
,
p
2
)
,
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
2
6
-
a
t
,
-
t
,
-
t
c
)
,
f
o
k
k
e
r
(
f
.
2
7
,
f
.
2
8
)
,
l
e
a
r
j
e
t
(
2
3
)
,
m
c
d
o
n
n
e
l
l
d
o
u
g
l
a
s
(
d
c
-
8
,
d
c
-
9
-
1
1
,
-
1
2
,
-
1
3
,
-
1
5
,
-
2
1
,
-
3
1
,
-
3
2
,
-
3
2
f
,
-
3
3
f
,
-
3
4
,
-
3
4
f
,
-
4
1
,
-
5
1
,
-
8
1
,
-
8
2
,
-
8
3
,
-
8
7
,
m
d
-
8
8
)
View Item »
Part Number
Description
Alternate
lamp, incandescent
GE 1683
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
4
)
,
b
e
e
c
h
(
r
a
y
t
h
e
o
n
)
(
2
0
0
,
c
9
0
,
e
9
0
,
f
3
3
a
)
,
b
e
l
l
(
2
0
6
a
,
2
0
6
b
,
2
0
6
l
-
1
,
2
0
6
l
,
2
1
2
,
2
2
2
)
,
b
o
m
b
a
r
d
i
e
r
,
i
n
c
.
(
c
l
6
0
0
)
,
d
a
s
s
a
u
l
t
a
v
i
a
t
i
o
n
(
f
a
l
c
o
n
2
0
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
h
c
-
6
-
3
0
0
,
d
h
c
-
7
)
,
e
m
b
r
a
e
r
e
m
p
r
e
s
a
(
e
m
b
-
1
1
0
p
1
,
p
2
)
,
e
u
r
o
c
o
p
t
e
r
d
e
u
t
s
c
h
l
a
n
d
(
m
b
b
b
o
-
1
0
5
)
,
g
u
l
f
s
t
r
e
a
m
(
g
1
5
9
,
g
1
1
5
9
a
)
,
h
i
l
l
e
r
a
v
i
a
t
i
o
n
(
f
h
1
1
0
0
)
,
l
e
a
r
j
e
t
(
2
3
,
2
4
,
2
5
,
2
8
,
2
9
,
3
5
,
3
6
,
5
5
)
,
l
o
c
k
h
e
e
d
(
1
3
2
9
-
2
5
(
j
e
t
s
t
a
r
i
i
)
)
,
m
d
h
e
l
i
c
o
p
t
e
r
s
,
i
n
c
.
(
m
d
h
i
)
(
3
6
9
d
)
,
p
i
p
e
r
(
p
a
-
3
1
-
3
5
0
)
,
s
c
h
w
e
i
z
e
r
(
2
6
9
c
)
,
s
h
o
r
t
b
r
o
t
h
e
r
s
(
s
d
-
3
-
3
0
)
,
s
i
k
o
r
s
k
y
(
s
-
7
6
)
View Item »
Part Number
Description
Alternate
lavatory extinguisher
Boeing Commercial Airplane Group 30100033-4
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
a
t
r
4
2
-
3
0
0
,
-
3
2
0
,
a
t
r
7
2
-
1
0
1
,
-
2
0
1
,
-
1
0
2
,
-
2
0
2
)
,
b
o
e
i
n
g
(
7
5
7
-
2
0
0
s
e
r
i
e
s
)
View Item »
Part Number
Description
Alternate
lead harness
Goodrich P/N4E1889-2 RAPCO P/NRA4E1889-2
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
,
n
2
2
s
)
b
o
m
b
a
r
d
i
e
r
,
i
n
c
.
(
d
h
c
-
6
-
1
,
-
1
0
0
,
-
2
0
0
.
-
3
0
0
)
b
r
i
t
i
s
h
a
e
r
o
s
p
a
c
e
(
j
e
t
s
t
r
e
a
m
s
c
r
i
e
s
2
0
0
m
o
d
i
f
i
e
d
w
i
t
h
s
t
c
s
a
2
2
9
3
s
w
)
c
e
s
s
n
a
(
4
4
1
)
c
o
n
s
t
r
u
c
c
i
o
n
e
s
(
c
a
s
a
)
(
c
-
2
1
2
-
c
b
,
c
-
2
1
2
-
c
c
)
e
m
b
r
a
e
r
e
m
p
r
e
s
a
(
e
m
b
-
1
1
0
p
1
,
e
m
b
-
1
i
0
p
2
)
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
6
-
a
t
.
s
a
2
2
6
-
t
,
s
a
2
2
6
-
a
t
,
s
a
2
2
6
-
t
(
b
)
,
s
a
2
2
6
-
t
c
)
h
a
r
b
i
n
(
y
1
2
i
v
)
i
s
r
a
e
l
(
a
r
a
v
a
1
0
1
,
a
r
a
v
a
1
0
1
b
)
m
i
t
s
u
b
i
s
h
i
(
m
u
-
2
b
-
1
0
,
-
1
5
,
-
2
0
,
-
2
5
,
-
2
6
,
-
3
0
,
-
3
5
,
-
3
6
)
p
i
l
a
t
u
s
a
i
r
c
r
a
f
t
(
p
c
-
6
/
b
-
h
2
,
p
c
-
6
/
b
1
-
h
2
,
p
c
-
6
/
b
2
-
h
2
,
p
c
-
6
/
b
2
-
h
4
)
p
i
p
e
r
(
p
a
-
3
1
t
,
p
a
-
3
1
t
1
,
p
a
-
3
1
t
2
,
p
a
3
1
t
3
,
p
a
-
4
2
,
p
a
-
4
2
-
7
2
0
)
r
a
y
t
h
e
o
n
(
6
5
-
9
0
,
c
9
0
a
.
h
9
0
,
6
5
-
a
9
0
-
1
,
6
5
-
a
9
0
-
2
,
6
5
-
a
9
0
-
3
,
6
5
-
a
9
0
-
4
,
9
9
.
9
9
a
9
9
(
f
a
c
h
)
,
a
9
9
,
a
9
9
a
.
b
9
9
,
c
9
9
,
1
0
0
,
b
1
0
0
,
2
0
0
.
2
0
0
c
,
2
0
0
c
t
,
2
0
0
t
,
b
2
0
0
s
e
r
i
a
l
s
b
b
-
1
4
3
9
.
b
b
-
1
4
4
4
&
a
f
t
e
r
,
e
x
c
e
p
t
b
b
-
1
4
6
3
.
a
2
0
0
(
c
-
1
2
a
)
.
a
2
0
0
(
c
-
1
2
c
)
.
a
2
0
0
c
(
u
c
-
1
2
b
)
,
a
2
0
0
c
t
(
c
-
1
2
d
)
,
a
2
0
0
c
t
(
f
w
c
-
1
2
d
)
.
a
2
0
0
c
t
(
c
-
1
2
f
)
.
a
2
0
0
c
t
(
r
c
-
1
2
d
)
.
a
2
0
0
c
t
(
r
c
-
1
2
g
)
,
a
2
0
0
c
t
(
r
c
-
1
2
h
)
,
b
2
0
0
c
(
c
-
1
2
f
)
.
b
2
0
0
c
(
u
c
-
i
2
m
)
.
b
2
0
0
c
(
c
-
1
2
r
)
.
b
2
0
0
c
(
u
c
-
i
2
f
)
,
b
2
0
0
c
s
e
r
i
a
l
s
b
l
-
1
3
9
&
a
f
t
e
r
a
n
d
b
w
-
1
&
a
f
t
e
r
)
s
h
o
r
t
b
r
o
t
h
e
r
s
(
s
c
-
7
s
e
r
i
e
s
2
.
s
c
-
7
s
e
r
i
e
s
3
)
t
w
i
n
c
o
m
m
a
n
d
e
r
(
6
9
0
.
6
9
0
a
.
6
9
0
b
)
View Item »
Part Number
Description
Alternate
link assembly
Rosemount 2314M-13-24
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
2
s
,
n
2
4
a
)
View Item »
Part Number
Description
Alternate
locknut, terminal screw
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
(
t
c
a
7
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
a
3
v
f
-
7
/
v
1
0
1
3
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
2
,
a
t
-
4
0
0
(
t
c
a
9
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
g
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
y
r
e
s
(
s
2
r
-
t
1
1
(
t
c
a
3
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
b
r
i
t
i
s
h
a
e
r
o
s
p
a
c
e
(
h
a
n
d
l
e
y
p
a
g
e
1
3
7
m
k
.
1
(
t
c
a
2
1
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
p
e
r
s
t
c
2
2
9
3
s
w
)
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
h
c
-
2
m
k
.
i
i
i
(
t
c
a
-
8
0
6
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
d
h
c
-
6
-
3
0
0
(
t
c
a
9
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
6
-
a
t
(
t
c
a
5
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
b
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
i
s
r
a
e
l
(
a
r
a
v
a
1
0
1
,
1
0
1
b
(
t
c
a
3
2
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
m
c
k
i
n
n
o
n
(
g
-
2
1
e
,
g
-
2
1
g
(
t
c
4
a
2
4
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
m
i
t
s
u
b
i
s
h
i
(
m
u
-
2
b
-
2
5
,
-
2
6
,
-
3
5
,
-
3
6
(
t
c
a
1
0
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
m
u
-
2
b
,
-
1
0
,
-
1
5
,
-
2
0
,
-
2
5
,
-
2
6
,
-
3
5
,
-
3
6
(
t
c
a
2
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
p
i
l
a
t
u
s
a
i
r
c
r
a
f
t
(
p
c
-
6
/
b
-
h
2
,
p
c
-
6
/
b
1
-
h
2
,
p
c
-
6
/
c
-
h
2
,
p
c
-
6
/
c
1
-
h
2
(
t
c
7
a
1
5
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
c
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
5
c
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
p
i
p
e
r
(
p
a
-
4
2
,
p
a
-
4
2
-
7
2
0
(
t
c
a
2
3
s
o
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
b
,
k
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
p
a
-
3
1
t
,
p
a
-
3
1
t
1
,
p
a
-
3
1
t
2
(
t
c
a
8
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
b
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
s
c
-
7
s
e
r
i
e
s
3
(
t
c
a
1
5
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
r
a
y
t
h
e
o
n
(
6
5
-
9
0
,
-
a
9
0
,
-
a
9
0
-
1
,
-
a
9
0
-
2
,
-
a
9
0
-
3
,
b
9
0
,
c
9
0
,
e
9
0
,
h
9
0
(
t
c
3
a
2
0
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
2
(
b
)
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
3
(
b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
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t
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c
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a
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l
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d
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f
9
0
(
t
c
a
3
1
c
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)
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t
h
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t
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e
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l
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n
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a
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1
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s
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t
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t
c
s
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5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
View Item »
Part Number
Description
Alternate
mounting
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
2
2
b
a
n
d
2
4
a
)
View Item »
Part Number
Description
Alternate
mounting assembly
Lord Corp LM-206-SA8-1
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
2
2
b
a
n
d
2
4
a
)
View Item »
Part Number
Description
Alternate
mounting assembly
Lord Corp LM-206-SA8-1
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
2
2
b
a
n
d
2
4
a
)
View Item »
Part Number
Description
Alternate
pin
AP177-3, SB177-00300, ES-177-3 PIN, 0177-00300
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
4
a
)
,
a
m
e
r
i
c
a
n
c
h
a
m
p
i
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n
(
8
g
c
b
c
)
,
b
r
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t
t
e
n
n
o
r
m
a
n
(
b
n
2
,
b
n
2
a
,
b
n
2
b
,
b
n
2
t
,
b
n
2
a
m
k
1
1
1
,
b
n
2
a
m
k
1
1
1
-
2
,
b
n
2
a
m
k
1
1
1
-
3
,
b
n
2
a
2
,
b
n
2
a
2
0
,
b
n
2
a
2
1
,
b
n
2
a
2
6
,
b
n
2
a
2
6
,
b
n
2
a
2
7
,
b
n
2
a
3
,
b
n
2
a
6
,
b
n
2
a
8
,
b
n
2
a
9
,
b
n
2
b
2
0
,
b
n
2
b
2
1
,
b
n
2
b
2
6
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2
b
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7
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b
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2
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b
n
2
b
,
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k
1
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2
,
m
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1
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1
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3
,
)
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c
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2
1
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3
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3
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7
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,
)
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g
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2
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f
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f
2
2
b
,
f
2
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c
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2
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3
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3
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3
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2
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4
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a
6
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6
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6
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h
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c
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4
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a
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5
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b
5
5
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b
5
5
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5
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c
5
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5
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)
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s
o
c
a
t
a
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t
b
3
0
)
View Item »
Part Number
Description
Alternate
pod fairing stub wing
Aerospace Technologies of Australia (ASTA) 1/N-11-617 & 1/N-11-818
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
a
s
t
a
n
2
2
s
e
r
i
e
s
)
View Item »
Part Number
Description
Alternate
propeller de-icer
AeroSpace Technologies of Australia P/N 4E1188-5
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
(
t
c
a
7
p
c
)
)
View Item »
Part Number
Description
Alternate
propeller de-icer
6975-11
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
p
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r
s
t
c
s
a
8
1
2
n
e
,
o
n
f
o
l
l
o
w
i
n
g
a
i
r
c
r
a
f
t
:
n
2
2
b
,
n
2
4
a
h
c
-
a
3
v
f
-
7
,
-
7
b
,
)
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a
i
r
t
r
a
c
t
o
r
(
p
e
r
s
t
c
s
a
8
1
2
n
e
,
o
n
f
o
l
l
o
w
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g
a
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r
c
r
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f
t
:
a
t
-
3
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2
,
-
4
0
0
h
c
-
b
3
t
n
-
5
c
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5
m
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3
d
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)
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a
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(
p
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8
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f
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:
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2
r
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t
1
1
h
c
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3
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n
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3
c
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3
d
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)
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b
r
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p
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e
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p
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r
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c
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8
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2
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f
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p
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1
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1
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t
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a
2
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3
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c
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b
3
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n
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3
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)
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c
e
s
s
n
a
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p
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s
t
c
s
a
8
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2
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n
f
o
l
l
o
w
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n
g
a
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c
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f
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:
4
4
1
,
h
c
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b
3
t
n
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5
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,
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5
m
,
)
,
c
o
n
s
t
r
u
c
c
i
o
n
e
s
(
c
a
s
a
)
(
p
e
r
s
t
c
s
a
8
1
2
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e
,
o
n
f
o
l
l
o
w
i
n
g
a
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r
c
r
a
f
t
:
c
a
s
a
c
2
1
2
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1
0
0
a
v
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o
c
a
r
h
c
-
b
4
t
n
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5
e
l
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)
,
d
e
h
a
v
i
l
l
a
n
d
(
p
e
r
s
t
c
s
a
8
1
2
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e
,
o
n
f
o
l
l
o
w
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a
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d
h
c
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2
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k
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i
i
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h
c
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3
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n
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3
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3
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3
b
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d
h
c
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6
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3
0
0
h
c
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3
t
n
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3
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d
)
(
y
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,
)
,
e
m
b
r
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e
m
p
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a
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p
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r
s
t
c
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a
8
1
2
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,
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n
f
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l
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w
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a
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c
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m
b
1
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h
c
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n
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3
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3
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f
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g
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8
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f
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w
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c
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:
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e
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m
m
a
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d
e
r
6
9
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6
9
0
a
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h
c
-
b
3
t
n
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5
f
l
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)
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i
s
r
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e
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8
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n
f
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l
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o
w
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a
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:
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b
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r
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h
c
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b
3
t
n
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3
d
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)
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m
c
k
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n
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n
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p
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8
1
2
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,
o
n
f
o
l
l
o
w
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c
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:
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g
r
u
m
m
a
n
g
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)
g
-
2
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&
g
-
2
1
g
h
c
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3
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n
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3
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y
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)
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m
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b
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(
p
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8
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c
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n
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3
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3
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c
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3
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n
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)
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p
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p
c
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b
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2
&
b
1
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h
2
h
c
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b
3
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View Item »
Part Number
Description
Alternate
propeller de-icer
Goodrich 4E1188-5
Applicable aircraft models: a
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View Item »
Part Number
Description
Alternate
propeller de-icer
AeroSpace Technologies of Australia 4E1188-5
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View Item »
Part Number
Description
Alternate
propeller de-icer
6975-11
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View Item »
Part Number
Description
Alternate
propeller de-icer detachable lead harness
BFGoodrich 4E1889-2
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View Item »
Part Number
Description
Alternate
propeller deicer
BFGoodrich 4E1188-5
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c
7
s
e
r
i
e
s
,
4
b
l
a
d
e
)
View Item »
Part Number
Description
Alternate
resistor power dropping heat sink case
Rosemount 2316M-9-1
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
2
s
,
n
2
4
a
)
View Item »
Part Number
Description
Alternate
rivet
AP105-2, SB105-0200, ES-105-2, 0105-0200
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
,
n
2
2
b
,
n
2
4
)
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a
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r
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s
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a
t
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1
0
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1
1
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1
2
5
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1
5
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1
8
0
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r
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1
1
0
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t
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1
6
0
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t
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1
8
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8
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2
2
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2
3
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l
6
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1
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7
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7
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1
8
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1
8
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1
8
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8
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3
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)
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c
h
a
p
a
r
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a
l
(
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h
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h
c
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a
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1
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m
a
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(
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a
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l
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a
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(
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r
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1
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r
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4
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a
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2
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0
8
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0
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c
t
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,
7
5
0
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l
)
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a
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6
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)
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a
1
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r
a
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t
h
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(
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)
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)
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n
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a
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r
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1
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a
1
8
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2
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a
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w
a
c
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(
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e
t
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v
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e
l
a
,
y
m
f
-
5
)
,
w
e
a
t
h
e
r
l
y
(
2
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6
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t
p
)
,
w
i
n
g
a
i
r
c
r
a
f
t
(
d
1
)
View Item »
Part Number
Description
Alternate
screw, fillister head block
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
(
t
c
a
7
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
a
3
v
f
-
7
/
v
1
0
1
3
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
2
,
a
t
-
4
0
0
(
t
c
a
9
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
g
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
y
r
e
s
(
s
2
r
-
t
1
1
(
t
c
a
3
s
w
)
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i
t
h
h
a
r
t
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l
l
h
c
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b
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n
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3
c
/
t
1
0
2
8
2
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r
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p
s
w
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t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
b
r
i
t
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s
h
a
e
r
o
s
p
a
c
e
(
h
a
n
d
l
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y
p
a
g
e
1
3
7
m
k
.
1
(
t
c
a
2
1
e
u
)
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i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
p
e
r
s
t
c
2
2
9
3
s
w
)
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
h
c
-
6
-
3
0
0
(
t
c
a
9
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
d
h
c
-
2
m
k
.
i
i
i
(
t
c
a
-
8
0
6
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
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View Item »
Part Number
Description
Alternate
screw, terminal
Modification Part
Applicable aircraft models: a
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View Item »
Part Number
Description
Alternate
terminal block
Modification Part
Applicable aircraft models: a
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b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
6
5
-
9
0
,
-
a
9
0
,
-
a
9
0
-
1
,
-
a
9
0
-
2
,
-
a
9
0
-
3
,
b
9
0
,
c
9
0
,
e
9
0
,
h
9
0
(
t
c
3
a
2
0
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
2
(
b
)
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
3
(
b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
d
1
8
c
,
d
1
8
s
,
e
1
8
s
-
9
7
0
0
,
c
-
4
5
g
,
c
-
4
5
h
,
t
c
-
4
5
g
,
t
c
-
4
5
h
,
t
c
-
4
5
j
(
t
c
a
-
7
6
5
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
1
7
8
p
r
o
p
s
p
e
r
s
t
c
s
a
2
2
0
4
w
e
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
s
h
o
r
t
b
r
o
t
h
e
r
s
(
s
c
-
7
s
e
r
i
e
s
3
(
t
c
a
1
5
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
View Item »
Part Number
Description
Alternate
vacuum pump assembly
Nichols-Airborne 241CC-13, Aero Accessories AA241CC-13, Federal Mogul (Champion) CH241CC-13
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
p
a
-
6
0
-
6
0
0
(
a
e
r
o
s
t
a
r
6
0
0
)
,
p
a
-
6
0
-
6
0
1
(
a
e
r
o
s
t
a
r
6
0
1
)
,
p
a
-
6
0
-
6
0
1
p
(
a
e
r
o
s
t
a
r
6
0
1
p
)
,
p
a
-
6
0
-
6
0
2
p
(
a
e
r
o
s
t
a
r
6
0
2
p
)
)
c
o
n
t
i
n
e
n
t
a
l
a
v
i
a
t
i
o
n
(
g
t
s
i
o
-
5
2
0
-
c
,
g
t
s
i
o
-
5
2
0
-
d
,
g
t
s
i
o
-
5
2
0
-
h
)
l
y
c
o
m
i
n
g
(
i
o
-
5
4
0
-
g
1
a
5
,
-
g
1
b
5
,
-
g
1
c
5
,
-
g
1
d
5
,
-
g
1
e
5
,
-
g
1
f
5
,
-
p
1
a
5
,
-
s
1
a
5
,
-
s
1
a
d
,
t
i
o
-
5
4
0
-
a
1
a
,
-
a
1
b
,
-
a
2
a
,
-
a
2
b
,
-
a
1
c
,
-
a
2
c
,
-
a
b
1
a
d
,
-
a
b
1
b
d
,
-
a
e
2
a
,
-
a
f
1
a
,
-
a
f
1
b
,
-
a
g
1
a
,
-
a
h
1
a
,
-
a
j
1
a
,
-
a
k
1
a
)
s
o
c
a
t
a
(
t
b
2
1
)
View Item »
Part Number
Description
Alternate
washer, spacer
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
(
t
c
a
7
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
a
3
v
f
-
7
/
v
1
0
1
3
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
2
,
a
t
-
4
0
0
(
t
c
a
9
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
g
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
y
r
e
s
(
s
2
r
-
t
1
1
(
t
c
a
3
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
b
r
i
t
i
s
h
a
e
r
o
s
p
a
c
e
(
h
a
n
d
l
e
y
p
a
g
e
1
3
7
m
k
.
1
(
t
c
a
2
1
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
p
e
r
s
t
c
2
2
9
3
s
w
)
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
h
c
-
6
-
3
0
0
(
t
c
a
9
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
d
h
c
-
2
m
k
.
i
i
i
(
t
c
a
-
8
0
6
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
6
-
a
t
(
t
c
a
5
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
b
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
i
s
r
a
e
l
(
a
r
a
v
a
1
0
1
,
1
0
1
b
(
t
c
a
3
2
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
m
c
k
i
n
n
o
n
(
g
-
2
1
e
,
g
-
2
1
g
(
t
c
4
a
2
4
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
m
i
t
s
u
b
i
s
h
i
(
m
u
-
2
b
,
-
1
0
,
-
1
5
,
-
2
0
,
-
2
5
,
-
2
6
,
-
3
5
,
-
3
6
(
t
c
a
2
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
m
u
-
2
b
-
2
5
,
-
2
6
,
-
3
5
,
-
3
6
(
t
c
a
1
0
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
p
i
l
a
t
u
s
a
i
r
c
r
a
f
t
(
p
c
-
6
/
b
-
h
2
,
p
c
-
6
/
b
1
-
h
2
,
p
c
-
6
/
c
-
h
2
,
p
c
-
6
/
c
1
-
h
2
(
t
c
7
a
1
5
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
c
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
5
c
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
p
i
p
e
r
(
p
a
-
3
1
t
,
p
a
-
3
1
t
1
,
p
a
-
3
1
t
2
(
t
c
a
8
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
b
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
p
a
-
4
2
,
p
a
-
4
2
-
7
2
0
(
t
c
a
2
3
s
o
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
b
,
k
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
r
a
y
t
h
e
o
n
(
d
1
8
c
,
d
1
8
s
,
e
1
8
s
-
9
7
0
0
,
c
-
4
5
g
,
c
-
4
5
h
,
t
c
-
4
5
g
,
t
c
-
4
5
h
,
t
c
-
4
5
j
(
t
c
a
-
7
6
5
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
1
7
8
p
r
o
p
s
p
e
r
s
t
c
s
a
2
2
0
4
w
e
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
6
5
-
9
0
,
-
a
9
0
,
-
a
9
0
-
1
,
-
a
9
0
-
2
,
-
a
9
0
-
3
,
b
9
0
,
c
9
0
,
e
9
0
,
h
9
0
(
t
c
3
a
2
0
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
2
(
b
)
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
3
(
b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
2
0
0
,
2
0
0
c
,
2
0
0
c
t
,
2
0
0
t
,
a
1
0
0
-
1
,
a
2
0
0
,
a
2
0
0
c
,
a
2
0
0
c
t
,
b
2
0
0
,
b
2
0
0
c
,
b
2
0
0
c
t
,
b
2
0
0
t
(
t
c
a
2
4
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
g
,
n
)
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
t
-
3
4
c
(
t
c
a
2
6
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
h
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
9
9
,
9
9
a
,
a
9
9
,
a
9
9
a
,
c
9
9
,
1
0
0
,
a
1
0
0
,
a
1
0
0
a
(
t
c
a
1
4
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
b
)
/
t
1
0
1
7
3
o
r
h
c
-
b
4
t
n
-
3
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
f
9
0
(
t
c
a
3
1
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
4
t
n
-
3
(
a
,
b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
s
h
o
r
t
b
r
o
t
h
e
r
s
(
s
c
-
7
s
e
r
i
e
s
3
(
t
c
a
1
5
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
View Item »
Part Number
Description
Alternate
washer, terminal screw
Modification Part
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
,
n
2
4
a
(
t
c
a
7
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
a
3
v
f
-
7
/
v
1
0
1
3
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
2
,
a
t
-
4
0
0
(
t
c
a
9
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
g
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
a
y
r
e
s
(
s
2
r
-
t
1
1
(
t
c
a
3
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
b
r
i
t
i
s
h
a
e
r
o
s
p
a
c
e
(
h
a
n
d
l
e
y
p
a
g
e
1
3
7
m
k
.
1
(
t
c
a
2
1
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
p
e
r
s
t
c
2
2
9
3
s
w
)
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
h
c
-
2
m
k
.
i
i
i
(
t
c
a
-
8
0
6
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
c
-
6
-
3
0
0
(
t
c
a
9
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
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a
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n
s
t
a
l
l
e
d
)
,
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
6
-
a
t
(
t
c
a
5
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
b
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
i
s
r
a
e
l
(
a
r
a
v
a
1
0
1
,
1
0
1
b
(
t
c
a
3
2
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
d
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
m
c
k
i
n
n
o
n
(
g
-
2
1
e
,
g
-
2
1
g
(
t
c
4
a
2
4
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
m
i
t
s
u
b
i
s
h
i
(
m
u
-
2
b
,
-
1
0
,
-
1
5
,
-
2
0
,
-
2
5
,
-
2
6
,
-
3
5
,
-
3
6
(
t
c
a
2
p
c
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
m
u
-
2
b
-
2
5
,
-
2
6
,
-
3
5
,
-
3
6
(
t
c
a
1
0
s
w
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
p
i
l
a
t
u
s
a
i
r
c
r
a
f
t
(
p
c
-
6
/
b
-
h
2
,
p
c
-
6
/
b
1
-
h
2
,
p
c
-
6
/
c
-
h
2
,
p
c
-
6
/
c
1
-
h
2
(
t
c
7
a
1
5
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
c
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
5
c
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
p
i
p
e
r
(
p
a
-
3
1
t
,
p
a
-
3
1
t
1
,
p
a
-
3
1
t
2
(
t
c
a
8
e
a
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
b
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
p
a
-
4
2
,
p
a
-
4
2
-
7
2
0
(
t
c
a
2
3
s
o
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
b
,
k
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
r
a
y
t
h
e
o
n
(
2
0
0
,
2
0
0
c
,
2
0
0
c
t
,
2
0
0
t
,
a
1
0
0
-
1
,
a
2
0
0
,
a
2
0
0
c
,
a
2
0
0
c
t
,
b
2
0
0
,
b
2
0
0
c
,
b
2
0
0
c
t
,
b
2
0
0
t
(
t
c
a
2
4
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
g
,
n
)
/
t
1
0
1
7
8
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
6
5
-
9
0
,
-
a
9
0
,
-
a
9
0
-
1
,
-
a
9
0
-
2
,
-
a
9
0
-
3
,
b
9
0
,
c
9
0
,
e
9
0
,
h
9
0
(
t
c
3
a
2
0
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
2
(
b
)
/
t
1
0
1
7
3
o
r
h
c
-
b
3
t
n
-
3
(
b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
9
9
,
9
9
a
,
a
9
9
,
a
9
9
a
,
c
9
9
,
1
0
0
,
a
1
0
0
,
a
1
0
0
a
(
t
c
a
1
4
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
(
b
)
/
t
1
0
1
7
3
o
r
h
c
-
b
4
t
n
-
3
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
f
9
0
(
t
c
a
3
1
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
4
t
n
-
3
(
a
,
b
)
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
d
1
8
c
,
d
1
8
s
,
e
1
8
s
-
9
7
0
0
,
c
-
4
5
g
,
c
-
4
5
h
,
t
c
-
4
5
g
,
t
c
-
4
5
h
,
t
c
-
4
5
j
(
t
c
a
-
7
6
5
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
1
7
8
p
r
o
p
s
p
e
r
s
t
c
s
a
2
2
0
4
w
e
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
,
t
-
3
4
c
(
t
c
a
2
6
c
e
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
3
h
/
t
1
0
1
7
3
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
,
s
h
o
r
t
b
r
o
t
h
e
r
s
(
s
c
-
7
s
e
r
i
e
s
3
(
t
c
a
1
5
e
u
)
w
i
t
h
h
a
r
t
z
e
l
l
h
c
-
b
3
t
n
-
5
c
/
t
1
0
2
8
2
p
r
o
p
s
w
i
t
h
s
t
c
s
a
5
7
2
e
a
i
n
s
t
a
l
l
e
d
)
View Item »
Part Number
Description
Alternate
wire harness
BF Goodrich 4E1889-2
Applicable aircraft models: a
e
r
o
s
p
a
c
e
t
e
c
h
n
o
l
o
g
i
e
s
(
n
2
2
b
)
,
c
e
s
s
n
a
(
4
4
1
w
i
t
h
(
h
c
-
b
3
t
n
-
5
)
p
r
o
p
e
l
l
e
r
)
,
c
o
n
s
t
r
u
c
c
i
o
n
e
s
(
c
a
s
a
)
(
c
-
2
1
2
-
c
b
w
i
t
h
4
b
l
a
d
e
p
r
o
p
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
h
c
-
6
-
3
0
0
w
i
t
h
(
h
c
-
b
3
t
n
-
5
)
p
r
o
p
e
l
l
e
r
)
,
e
m
b
r
a
e
r
e
m
p
r
e
s
a
(
e
m
b
-
1
1
0
p
1
,
e
m
b
-
1
1
0
p
2
)
,
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
2
6
-
t
,
s
a
2
2
6
-
a
t
,
s
a
2
2
6
-
t
c
)
,
i
s
r
a
e
l
(
a
v
a
r
a
1
0
1
)
,
j
e
t
s
t
r
e
a
m
(
h
.
p
.
1
3
7
j
e
t
s
t
r
e
a
m
m
k
.
1
)
,
m
i
t
s
u
b
i
s
h
i
(
m
u
-
2
b
,
m
u
-
2
b
-
1
0
,
m
u
-
2
b
-
1
5
,
m
u
-
2
b
-
2
0
,
m
u
-
2
b
-
2
5
,
m
u
-
2
b
-
2
6
,
m
u
-
2
b
-
3
0
,
m
u
-
2
b
-
3
5
,
m
u
-
2
b
-
3
6
w
i
t
h
(
h
c
-
b
3
t
n
-
5
)
p
r
o
p
e
l
l
e
r
)
,
p
i
l
a
t
u
s
a
i
r
c
r
a
f
t
(
p
c
-
6
)
,
p
i
p
e
r
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View Item »
Part Number
Description
Alternate
wire harness
Goodrich P/N 4E1889-2
Applicable aircraft models: a
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View Item »
