Page 11 of 17
Part Number
Description
Alternate
parts fairlead
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
a
t
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
,
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
parts fairlead
9010
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
-
4
0
0
a
,
a
t
-
4
0
2
,
-
4
0
2
a
,
-
4
0
2
b
,
-
5
0
2
,
-
5
0
2
b
,
-
5
0
3
)
View Item »
Part Number
Description
Alternate
pass-through block
Modification Parts
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
&
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
pass-through block
Modification Parts
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
&
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
pass-through block
Modification Parts
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
&
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
phenolic sheet
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
a
t
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
,
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
phenolic sheet
9020
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
-
4
0
0
a
,
a
t
-
4
0
2
,
-
4
0
2
a
,
-
4
0
2
b
,
-
5
0
2
,
-
5
0
2
b
,
-
5
0
3
)
View Item »
Part Number
Description
Alternate
pin
AP177-16, SB177-01600, ES-177-16 PIN, 0177-01600
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
8
0
2
)
,
c
e
s
s
n
a
(
3
4
0
,
4
0
2
,
4
0
2
a
,
4
0
2
b
,
4
0
2
c
,
4
0
4
,
4
1
1
,
4
1
4
,
4
1
4
a
,
4
2
1
a
,
4
2
1
b
,
4
2
1
c
,
4
2
5
)
,
d
e
h
a
v
i
l
l
a
n
d
(
d
c
h
2
m
k
1
,
d
c
h
2
m
k
2
,
d
c
h
3
m
k
3
)
,
e
m
b
r
a
e
r
e
m
p
r
e
s
a
(
e
m
b
3
1
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
6
t
)
,
g
u
l
f
s
t
r
e
a
m
(
5
0
0
s
e
r
i
e
s
,
6
8
1
,
6
8
5
,
6
9
0
,
6
9
5
)
,
m
i
t
s
u
b
i
s
h
i
(
m
u
2
b
,
-
1
0
,
-
1
5
,
-
2
0
,
-
2
5
,
-
2
6
,
-
2
6
a
,
-
3
0
,
-
3
5
,
-
3
6
,
-
3
6
a
,
-
4
0
,
-
6
0
)
,
p
i
p
e
r
(
p
a
-
3
1
3
5
0
,
p
a
3
1
t
,
p
a
3
1
-
3
5
0
,
p
a
3
1
p
-
3
5
0
,
p
a
3
1
p
-
4
2
5
,
p
a
3
1
t
,
p
a
3
1
t
2
,
p
a
-
4
2
,
p
a
4
2
-
7
2
0
)
,
r
a
y
t
h
e
o
n
(
b
e
e
c
h
)
(
d
1
8
c
,
d
1
8
s
,
6
5
,
6
5
-
8
0
,
6
5
-
b
8
0
,
6
5
-
8
8
,
6
5
-
a
8
0
,
6
5
-
a
9
0
-
1
,
6
5
a
9
0
-
4
,
7
0
,
c
9
0
,
c
9
0
a
,
f
9
0
3
n
,
3
n
m
,
3
t
m
)
View Item »
Part Number
Description
Alternate
placard
50-006-3
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
5
0
2
)
View Item »
Part Number
Description
Alternate
plate
50-018-23
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
5
0
2
)
View Item »
Part Number
Description
Alternate
plate, closure
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
&
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
plate, plenum side
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
-
4
0
0
a
,
-
4
0
2
,
-
4
0
2
a
,
-
4
0
2
b
,
-
5
0
2
,
-
5
0
2
b
&
-
5
0
3
)
View Item »
Part Number
Description
Alternate
plate, plenum side
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
&
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
plate, reinforcement
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
0
,
-
3
0
1
,
-
3
0
2
,
-
4
0
0
,
-
4
0
0
a
,
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
&
-
4
0
2
b
)
View Item »
Part Number
Description
Alternate
plenum assembly
PT32300
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
8
0
2
,
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
plenum assembly
PT22300
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
6
0
2
)
View Item »
Part Number
Description
Alternate
pm501 panel mounted intercom
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
1
,
-
4
0
1
a
,
-
4
0
1
b
,
-
4
0
2
,
-
4
0
2
a
,
-
4
0
2
b
,
-
5
0
1
,
-
5
0
2
,
-
5
0
2
a
,
-
5
0
2
b
,
-
5
0
3
,
-
5
0
3
a
,
-
5
0
4
,
-
8
0
2
,
-
8
0
2
a
,
-
6
0
2
)
View Item »
Part Number
Description
Alternate
pma parts kit (for installation of model 10000 floats)
Modification Parts
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
pma parts kit (for installation of model 10000 floats)
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
8
0
2
,
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
pma parts kit (for installation of vortex generators)
Modification Parts
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
power cable
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
)
View Item »
Part Number
Description
Alternate
power cable
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
,
a
t
-
8
0
2
,
a
t
-
4
0
0
a
,
a
t
-
4
0
2
a
,
a
t
-
4
0
2
b
,
a
t
-
5
0
2
a
,
a
t
-
5
0
2
b
,
a
n
d
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
pressure cable
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
)
View Item »
Part Number
Description
Alternate
pressure cable
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
,
a
t
-
8
0
2
,
a
t
-
4
0
0
a
,
a
t
-
4
0
2
a
,
a
t
-
4
0
2
b
,
a
t
-
5
0
2
a
,
a
t
-
5
0
2
b
,
a
n
d
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
pressure plate
Cleveland 063-01300
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
3
0
1
,
a
t
-
3
0
2
,
a
t
-
4
0
0
,
a
t
-
4
0
0
a
,
a
t
-
4
0
2
,
a
t
-
5
0
1
,
a
t
-
5
0
2
,
a
t
-
5
0
3
,
a
t
-
5
0
3
a
)
t
h
r
u
s
h
a
i
r
c
r
a
f
t
,
i
n
c
.
(
s
n
o
w
,
r
o
c
k
w
e
l
l
,
a
y
r
e
s
)
(
s
2
r
,
s
2
r
-
r
1
3
4
0
,
s
2
r
-
r
1
8
2
0
,
s
2
r
-
t
1
1
,
s
2
r
-
t
1
5
,
s
2
r
-
t
3
4
,
s
2
r
-
t
6
5
,
s
2
r
h
g
-
t
6
5
)
t
h
r
u
s
h
a
i
r
c
r
a
f
t
,
i
n
c
.
(
s
n
o
w
,
r
o
c
k
w
e
l
l
,
a
y
r
e
s
)
(
s
t
c
s
a
1
6
2
g
l
)
(
s
2
r
)
w
e
a
t
h
e
r
l
y
(
6
2
0
a
,
6
2
0
b
,
6
2
0
t
p
)
View Item »
Part Number
Description
Alternate
pressure plate
Cleveland Wheels & Brakes 063-02500
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
1
,
a
t
-
4
0
1
a
)
a
l
l
i
e
d
a
g
c
a
t
p
r
o
d
u
c
t
i
o
n
s
,
i
n
c
.
(
g
-
1
6
4
c
,
g
-
1
6
4
d
,
g
-
1
6
4
d
w
i
t
h
7
3
w
i
n
g
g
a
p
)
e
m
a
i
r
(
m
u
r
r
a
y
a
i
r
)
(
m
a
-
1
b
)
g
r
u
m
m
a
n
(
s
2
f
-
3
t
)
p
a
c
i
f
i
c
a
e
r
o
s
p
a
c
e
l
i
m
i
t
e
d
(
7
5
0
x
l
)
q
u
e
s
t
(
k
o
d
i
a
k
1
0
0
)
t
e
x
t
r
o
n
a
v
i
a
t
i
o
n
i
n
c
.
(
2
0
8
,
2
0
8
b
)
t
h
r
u
s
h
a
i
r
c
r
a
f
t
,
i
n
c
.
(
s
n
o
w
,
r
o
c
k
w
e
l
l
,
a
y
r
e
s
)
(
s
2
r
)
View Item »
Part Number
Description
Alternate
pressure plate assy
Cleveland Wheels & Brakes 073-02600
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
1
,
a
t
-
4
0
1
a
)
a
l
l
i
e
d
a
g
c
a
t
p
r
o
d
u
c
t
i
o
n
s
,
i
n
c
.
(
g
-
1
6
4
c
,
g
-
1
6
4
d
,
g
-
1
6
4
d
w
i
t
h
7
3
w
i
n
g
g
a
p
)
e
m
a
i
r
(
m
u
r
r
a
y
a
i
r
)
(
m
a
-
1
b
)
g
r
u
m
m
a
n
(
s
2
f
-
3
t
)
t
h
r
u
s
h
a
i
r
c
r
a
f
t
,
i
n
c
.
(
s
n
o
w
,
r
o
c
k
w
e
l
l
,
a
y
r
e
s
)
(
s
2
r
)
View Item »
Part Number
Description
Alternate
pressure probe
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
)
View Item »
Part Number
Description
Alternate
pressure probe
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
,
a
t
-
8
0
2
,
a
t
-
4
0
0
a
,
a
t
-
4
0
2
a
,
a
t
-
4
0
2
b
,
a
t
-
5
0
2
a
,
a
t
-
5
0
2
b
,
a
n
d
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
pressure probe mounting
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
)
View Item »
Part Number
Description
Alternate
pressure probe mounting
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
,
a
t
-
8
0
2
,
a
t
-
4
0
0
a
,
a
t
-
4
0
2
a
,
a
t
-
4
0
2
b
,
a
t
-
5
0
2
a
,
a
t
-
5
0
2
b
,
a
n
d
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
probe float
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
)
View Item »
Part Number
Description
Alternate
probe float
Modification Part
Applicable aircraft models: a
i
r
t
r
a
c
t
o
r
(
a
t
-
4
0
0
,
a
t
-
4
0
2
,
a
t
-
5
0
2
,
a
t
-
6
0
2
,
a
t
-
8
0
2
,
a
t
-
4
0
0
a
,
a
t
-
4
0
2
a
,
a
t
-
4
0
2
b
,
a
t
-
5
0
2
a
,
a
t
-
5
0
2
b
,
a
n
d
a
t
-
8
0
2
a
)
View Item »
Part Number
Description
Alternate
propeller de-icer
Modification Part
Applicable aircraft models: 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
/
h
c
-
b
3
t
n
-
5
c
/
-
5
m
/
-
3
d
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
t
h
r
u
s
h
a
i
r
c
r
a
f
t
(
s
2
r
-
t
1
1
(
t
c
a
4
s
w
)
w
/
h
c
-
b
3
t
n
-
3
c
/
-
3
d
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
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
/
s
t
c
s
a
2
2
0
4
w
e
w
/
h
c
-
b
3
t
n
-
5
c
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
,
t
-
3
4
c
(
t
c
a
2
6
c
e
)
w
/
h
c
-
b
3
t
n
-
3
h
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
,
6
5
-
9
0
,
6
5
-
a
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
(
t
c
3
a
2
0
)
w
/
h
c
-
b
3
t
n
-
3
b
,
-
3
m
,
-
2
b
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
,
f
9
0
(
t
c
a
3
1
c
e
)
w
/
h
c
-
b
4
t
n
-
3
a
,
-
3
b
(
t
c
p
4
0
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
,
9
9
,
9
9
a
,
a
9
9
,
a
9
9
a
(
t
c
a
1
4
c
e
)
w
/
h
c
-
b
3
t
n
-
3
b
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
,
b
9
0
,
c
9
0
,
e
9
0
,
h
9
0
(
t
c
3
a
2
0
)
w
/
h
c
-
b
3
t
n
-
3
b
,
-
3
m
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
r
a
y
t
h
e
o
n
(
c
9
9
,
1
0
0
(
t
c
a
1
4
c
e
)
w
/
h
c
-
b
3
t
n
-
3
b
,
-
3
m
(
t
c
p
1
5
e
a
)
,
a
1
0
0
,
a
1
0
0
a
,
a
1
0
0
-
1
(
t
c
a
1
4
c
e
)
w
/
h
c
-
b
4
t
n
-
3
,
-
3
a
(
t
c
p
1
5
e
a
)
,
2
0
0
,
2
0
0
c
,
2
0
0
c
t
,
2
0
0
t
,
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
/
h
c
-
b
3
t
n
-
3
g
,
-
3
n
(
t
c
p
1
5
e
a
)
,
b
1
0
0
(
t
c
a
1
4
c
e
)
w
/
h
c
-
b
4
t
n
-
5
c
,
-
5
f
(
t
c
p
4
0
e
a
)
,
j
r
b
-
6
(
t
c
a
-
7
6
5
)
w
/
s
t
c
s
a
1
1
7
1
w
e
w
/
h
c
-
b
3
t
n
-
5
c
(
t
c
p
4
0
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
b
r
i
t
i
s
h
a
e
r
o
s
p
a
c
e
(
h
p
.
1
3
7
m
k
.
1
(
t
c
a
2
1
e
u
)
w
/
s
t
c
s
a
2
2
9
3
s
w
&
h
c
-
b
3
t
n
-
3
d
(
t
c
p
1
5
e
a
)
&
s
t
c
s
a
8
1
2
n
e
)
,
c
o
n
s
t
r
u
c
c
i
o
n
e
s
(
c
a
s
a
)
(
c
2
1
2
-
1
0
0
a
v
i
o
c
a
r
(
t
c
a
4
3
e
u
)
w
/
h
c
-
b
4
t
n
-
5
e
l
(
t
c
p
1
5
e
a
)
&
s
t
c
s
a
8
1
2
n
e
)
,
c
e
s
s
n
a
(
4
4
1
(
t
c
a
2
8
c
e
)
w
/
h
c
-
b
3
t
n
-
5
e
,
-
5
m
(
t
c
p
1
5
e
a
)
&
s
t
c
s
a
8
1
2
n
e
)
,
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
/
h
c
-
b
3
t
n
-
3
,
-
3
b
,
-
3
b
y
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
b
o
m
b
a
r
d
i
e
r
,
i
n
c
.
(
d
h
c
-
6
-
3
0
0
(
t
c
a
9
e
a
)
w
/
h
c
-
b
3
t
n
-
3
(
d
)
(
y
)
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
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
(
t
c
a
2
1
s
o
)
w
/
h
c
-
b
3
t
n
-
3
c
,
-
3
d
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
f
a
i
r
c
h
i
l
d
a
i
r
c
r
a
f
t
(
s
a
2
2
6
-
a
t
,
s
a
2
2
6
-
t
(
t
c
a
5
s
w
)
w
/
h
c
-
b
3
t
n
-
5
(
)
(
t
c
p
1
5
e
a
)
,
s
a
2
2
6
-
t
c
(
t
c
a
8
s
w
)
w
/
s
t
c
s
a
3
4
4
g
l
,
w
/
h
c
-
b
3
t
n
-
5
(
)
(
t
c
p
1
5
e
a
)
,
s
a
2
2
6
-
t
c
(
t
c
a
8
s
w
)
,
w
/
h
c
-
b
4
t
n
-
5
(
)
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
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
/
h
c
-
a
3
v
f
-
7
,
-
7
b
(
t
c
p
6
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
t
w
i
n
c
o
m
m
a
n
d
e
r
(
a
e
r
o
c
o
m
m
a
n
d
e
r
6
9
0
,
6
9
0
a
,
6
9
0
b
(
t
c
2
a
4
)
w
/
h
c
-
b
3
t
n
-
5
(
)
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
i
s
r
a
e
l
(
1
0
1
a
r
a
v
a
,
1
0
1
b
a
r
a
v
a
(
t
c
a
3
2
e
u
)
w
/
h
c
-
b
3
t
n
-
3
d
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
a
e
r
o
p
l
a
n
e
s
(
g
-
2
1
e
,
g
-
2
1
g
(
t
c
4
a
2
4
)
w
/
h
c
-
b
3
t
n
-
3
d
y
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
m
i
t
s
u
b
i
s
h
i
(
m
u
-
2
b
,
m
u
-
2
b
-
1
0
(
t
c
a
2
p
c
&
a
1
0
s
w
)
)
w
/
h
c
-
b
3
t
n
-
5
(
)
(
t
c
p
1
5
e
a
)
,
m
u
-
2
b
-
1
5
,
m
u
-
2
b
-
2
0
,
m
u
-
2
b
-
3
0
(
t
c
a
2
p
c
)
w
/
h
c
-
b
3
t
n
-
5
(
t
c
p
1
5
e
a
)
,
m
u
-
2
b
-
2
5
,
m
u
-
2
b
-
2
6
,
m
u
-
2
b
-
3
5
,
m
u
-
2
b
-
3
6
(
t
c
a
2
p
c
)
w
/
h
c
-
b
3
t
n
-
5
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
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
/
h
c
-
b
3
t
n
-
3
c
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
p
i
p
e
r
(
p
a
-
3
1
t
,
p
a
-
3
1
t
1
(
t
c
a
8
e
a
)
w
/
h
c
-
b
3
t
n
-
3
b
(
t
c
p
1
5
e
a
)
,
p
a
-
4
2
,
p
a
-
4
2
-
7
2
0
(
t
c
a
2
3
s
o
)
w
/
h
c
-
b
3
t
n
-
3
b
,
-
3
k
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
s
h
o
r
t
b
r
o
t
h
e
r
s
(
s
c
-
7
s
e
r
i
e
s
3
v
a
r
i
a
n
t
2
0
0
(
t
c
a
1
5
e
u
)
w
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h
c
-
b
3
t
n
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(
)
(
t
c
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1
5
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)
,
s
c
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7
s
e
r
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e
s
3
v
a
r
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a
n
t
2
0
0
(
t
c
a
1
5
e
u
)
w
/
s
t
c
s
a
0
2
0
5
9
a
k
w
/
h
c
-
b
4
t
n
-
5
(
t
c
p
1
5
e
a
)
w
/
s
t
c
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a
8
1
2
n
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)
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a
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r
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r
a
c
t
o
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(
a
t
-
3
0
2
,
a
t
-
4
0
0
(
t
c
a
9
s
w
)
w
/
h
c
-
b
3
t
n
-
5
c
/
-
5
m
/
-
3
d
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
,
t
h
r
u
s
h
a
i
r
c
r
a
f
t
(
s
2
r
-
t
1
1
(
t
c
a
4
s
w
)
w
/
h
c
-
b
3
t
n
-
3
c
/
-
3
d
(
t
c
p
1
5
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a
)
w
/
s
t
c
s
a
8
1
2
n
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)
,
r
a
y
t
h
e
o
n
(
d
1
8
c
,
d
1
8
s
,
e
1
8
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-
9
7
0
0
,
c
-
4
5
g
,
c
-
4
5
h
,
t
c
-
4
5
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,
t
c
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4
5
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,
t
c
-
4
5
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(
t
c
a
-
7
6
5
)
w
/
s
t
c
s
a
2
2
0
4
w
e
w
/
h
c
-
b
3
t
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-
5
c
(
t
c
p
1
5
e
a
)
w
/
s
t
c
s
a
8
1
2
n
e
)
View Item »
Part Number
Description
Alternate
propeller de-icer
Modification Part
Applicable aircraft models: 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
/
h
c
-
b
3
t
n
-
3
g
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
t
h
r
u
s
h
a
i
r
c
r
a
f
t
(
s
2
r
-
t
1
1
(
t
c
a
3
s
w
)
w
/
h
c
-
b
3
t
n
-
3
c
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
&
s
t
c
2
2
0
4
w
e
)
w
/
h
c
-
b
3
t
n
-
5
c
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
r
a
y
t
h
e
o
n
(
t
-
3
4
c
(
t
c
a
2
6
c
e
)
w
/
h
c
-
b
3
t
n
-
3
h
p
r
o
p
s
,
6
5
-
9
0
,
6
5
-
a
-
9
0
,
6
5
-
a
9
0
-
1
,
6
5
-
a
9
0
-
2
,
6
5
-
a
9
0
-
3
,
b
9
0
,
c
9
0
,
e
9
0
,
h
9
0
(
t
c
3
a
2
0
)
w
/
h
c
b
3
t
n
-
2
b
o
r
-
3
b
p
r
o
p
s
,
f
9
0
(
t
c
a
3
1
c
e
)
w
/
h
c
-
b
4
t
n
-
3
a
o
r
-
3
b
p
r
o
p
s
,
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
/
h
c
-
b
3
t
n
-
3
o
r
-
3
b
p
r
o
p
s
,
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
/
h
c
-
b
3
t
n
-
3
g
o
r
-
3
n
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
b
r
i
t
i
s
h
a
e
r
o
s
p
a
c
e
(
h
p
.
1
3
7
m
k
.
1
(
t
c
a
2
1
e
u
&
s
t
c
2
2
9
3
s
w
)
w
/
h
c
-
b
3
t
n
-
3
d
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
3
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
b
o
m
b
a
r
d
i
e
r
,
i
n
c
.
(
d
h
c
-
6
-
3
0
0
(
t
c
a
9
e
a
)
w
/
h
c
-
b
3
t
n
-
3
d
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
3
b
o
r
-
5
c
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
a
3
v
f
-
7
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
3
d
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
a
e
r
o
p
l
a
n
e
s
(
g
-
2
1
e
,
g
-
2
1
g
(
t
c
4
a
2
4
)
w
/
h
c
-
b
3
t
n
-
3
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
5
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
5
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
3
c
o
r
-
5
c
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
3
b
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
,
p
a
-
4
2
,
p
a
-
4
2
-
7
2
0
(
t
c
a
2
3
s
o
)
w
/
h
c
-
b
3
t
n
-
3
b
o
r
3
k
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
,
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
/
h
c
-
b
3
t
n
-
5
c
p
r
o
p
s
w
/
s
t
c
s
a
5
7
2
e
a
)
View Item »
