Page 51 of 110
Part Number
Description
Alternate
impulse coupling assy (cw 20 deg)
TCM/Bendix 10-400311 when used in TCM Bendix Magneto 10-682555 -14, & -141
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
3
2
0
-
h
1
a
d
,
o
-
3
2
0
-
h
2
a
d
,
o
-
3
2
0
-
h
3
a
d
,
l
o
-
3
6
0
-
a
1
g
6
d
,
o
-
3
6
0
-
e
1
a
6
d
,
l
o
-
3
6
0
-
a
1
g
6
d
)
View Item »
Part Number
Description
Alternate
impulse coupling assy (cw 20 deg.)
TCM/Bendix 10- 400311 When used in TCM Bendix Magneto 10-682555-14 &-141
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
3
2
0
-
h
1
a
d
,
o
-
3
2
0
-
h
2
a
d
,
h
3
a
d
l
o
-
3
6
0
-
a
1
g
6
d
o
-
3
6
0
-
e
1
a
6
d
)
View Item »
Part Number
Description
Alternate
impulse coupling assy.
Champion Aerospace/Unison/ Slick M3529
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
c
1
,
-
c
2
a
,
-
c
2
c
,
-
j
2
a
,
o
-
2
9
0
-
d
2
,
-
d
2
b
,
-
d
2
c
,
o
-
3
2
0
-
a
2
a
,
-
a
2
b
,
-
a
3
a
,
-
a
3
b
,
-
b
1
a
,
-
b
2
a
,
-
b
2
b
,
-
b
2
d
,
-
b
2
e
,
-
b
3
b
,
-
d
1
a
,
-
d
1
f
,
-
d
2
a
,
-
e
1
f
,
-
e
2
a
,
-
e
2
c
,
-
e
2
f
,
i
o
-
3
2
0
-
b
1
a
,
-
c
1
a
,
-
d
1
a
,
-
d
1
b
,
-
e
1
a
,
-
e
2
a
,
a
e
i
o
-
3
2
0
-
d
1
b
,
-
d
2
b
,
o
-
3
6
0
-
a
1
a
,
-
a
1
f
6
,
-
a
1
g
6
,
-
a
1
h
,
-
a
1
h
6
,
-
a
1
p
,
-
a
2
a
,
-
a
2
f
,
-
a
2
g
,
-
a
3
a
,
-
a
4
a
,
-
a
4
g
,
-
a
4
j
,
-
a
4
m
,
-
b
2
a
,
-
b
2
c
,
-
c
1
a
,
-
c
1
g
,
-
c
2
a
,
i
o
-
3
6
0
-
b
1
e
,
-
b
1
f
,
-
b
1
g
6
,
-
b
2
e
,
-
b
4
a
,
m
1
b
,
a
e
i
o
-
3
6
0
-
a
1
b
6
,
-
a
1
e
,
-
b
1
f
,
-
b
1
h
,
-
b
2
f
,
-
b
4
a
)
View Item »
Part Number
Description
Alternate
impulse coupling assy.
Champion Aerospace/Unison/ Slick M3163
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
c
2
c
,
-
h
2
c
,
-
n
2
c
,
o
-
3
2
0
-
a
2
d
,
-
b
2
b
,
-
d
1
a
,
-
d
1
d
,
-
d
1
f
,
-
d
2
a
,
-
d
2
g
,
-
d
2
j
,
-
d
3
g
,
-
e
1
f
,
-
e
2
d
,
-
e
2
g
,
-
e
3
d
,
i
o
-
3
2
0
-
e
1
b
,
-
e
2
b
,
a
e
i
o
-
3
2
0
-
e
1
b
,
-
e
2
b
,
o
-
3
6
0
-
a
1
a
,
-
a
1
f
6
,
-
a
4
k
,
-
a
4
m
,
-
a
4
n
,
-
a
4
p
,
-
c
1
e
,
-
c
1
f
,
-
c
1
g
,
-
c
2
e
,
-
c
4
f
,
-
c
4
p
,
-
f
1
a
6
,
i
o
-
3
6
0
-
c
1
c
,
-
l
2
a
,
-
m
1
b
,
a
e
i
o
-
3
6
0
-
a
1
b
6
,
-
b
1
g
6
,
-
h
1
a
,
-
h
1
b
)
s
u
p
e
r
i
o
r
a
i
r
p
a
r
t
s
(
i
o
-
3
6
0
-
2
5
d
e
g
r
e
e
,
o
-
3
6
0
-
2
5
d
e
g
r
e
e
)
View Item »
Part Number
Description
Alternate
impulse coupling assy.
Champion Aerospace/Unison/ Slick M3100
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
k
2
b
,
-
k
2
c
,
-
l
2
a
,
-
l
2
c
,
-
n
2
a
,
i
o
-
3
6
0
-
a
1
b
,
-
a
1
b
6
,
-
a
1
d
,
-
a
2
b
,
-
c
1
c
,
-
c
1
c
6
,
-
c
1
d
6
,
-
c
1
e
6
,
-
c
1
f
,
a
e
i
o
-
3
6
0
-
a
1
b
,
-
a
1
d
,
-
a
1
e
)
View Item »
Part Number
Description
Alternate
impulse coupling assy.
Champion Aerospace/Unison/ Slick M3689
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
i
o
-
3
6
0
-
c
1
e
6
)
View Item »
Part Number
Description
Alternate
impulse coupling assy.
Champion Aerospace/Unison/ Slick M3333
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
a
1
b
5
,
-
a
4
a
5
,
-
b
2
c
5
e
4
c
5
,
-
g
1
a
5
,
-
g
2
a
5
,
h
2
a
5
,
-
j
3
a
5
,
i
o
-
5
4
0
-
a
1
b
5
,
-
c
4
d
5
,
d
4
b
5
,
-
g
1
d
5
,
-
k
1
a
5
,
-
k
1
b
5
,
-
k
1
e
5
,
-
k
1
g
5
,
-
k
1
h
5
,
k
1
k
5
,
-
l
1
c
5
,
-
m
1
c
5
,
t
4
b
5
,
-
v
4
a
5
,
-
w
1
a
5
,
a
a
1
b
5
,
-
a
b
1
a
5
,
-
a
c
1
a
5
,
a
f
1
a
5
,
a
e
i
o
-
5
4
0
-
d
4
b
5
,
-
l
1
b
5
,
l
1
d
5
,
t
i
o
-
5
4
0
-
w
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
)
View Item »
Part Number
Description
Alternate
impulse coupling assy.
Champion Aerospace/Unison/ Slick M3635
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
a
1
a
5
,
-
a
1
b
5
,
a
1
c
5
,
b
2
b
5
,
-
b
4
b
5
,
-
e
4
b
5
)
View Item »
Part Number
Description
Alternate
induction air box
Modification
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
e
4
a
5
)
View Item »
Part Number
Description
Alternate
installation of fuel injector nozzle
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
i
o
-
5
4
0
-
a
c
1
a
5
p
/
n
g
l
1
0
a
n
d
g
l
t
2
0
t
i
o
-
5
4
0
-
a
f
1
b
,
-
a
j
1
a
p
/
n
g
l
t
2
0
o
n
l
y
)
View Item »
Part Number
Description
Alternate
installation of modified fuel injector nozzle
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
a
i
o
-
3
6
0
-
a
1
a
,
a
2
a
,
a
1
b
,
a
2
b
,
b
1
b
,
l
i
o
-
3
6
0
-
c
1
e
6
,
l
h
i
o
-
3
6
0
-
a
1
a
,
c
1
b
,
f
1
a
d
,
a
e
i
o
-
3
6
0
-
a
1
a
,
a
1
b
,
a
1
b
6
,
a
1
c
,
a
1
d
,
a
1
e
,
a
1
e
5
,
a
2
a
,
a
2
b
,
a
2
c
,
h
1
a
,
h
1
b
,
b
1
b
,
b
1
d
,
b
1
f
,
b
2
f
,
b
4
a
,
b
1
f
6
,
b
2
f
6
,
b
1
g
6
,
i
v
o
-
3
6
0
-
a
1
a
,
t
i
o
-
3
6
0
-
a
1
a
,
a
2
b
,
a
3
b
6
,
c
1
a
6
d
,
i
o
-
3
6
0
-
a
1
a
,
a
1
b
,
a
1
b
6
,
a
1
b
6
d
,
a
1
c
,
a
1
d
,
a
1
d
6
,
a
1
d
6
d
,
a
2
a
,
a
2
b
,
a
2
c
,
a
3
b
6
,
a
3
b
6
d
,
a
3
d
6
d
,
b
1
a
,
b
1
b
,
b
1
c
,
b
1
d
,
b
1
e
,
b
1
f
,
b
1
f
6
,
b
2
e
,
b
2
f
,
b
2
f
6
,
b
4
a
,
c
1
a
,
c
1
b
,
c
1
c
,
c
1
c
6
,
c
1
d
6
,
c
1
e
6
,
c
1
e
6
d
,
c
1
f
,
d
1
a
,
e
1
a
,
f
1
a
,
j
1
a
d
,
j
1
a
6
d
,
k
2
a
,
l
2
a
,
l
t
i
o
-
5
4
0
-
f
2
b
d
,
j
2
b
,
j
2
b
d
,
k
1
a
d
,
n
2
b
d
,
r
2
a
d
,
u
2
a
,
v
2
a
d
,
w
2
a
t
i
v
o
-
5
4
0
-
a
2
a
i
o
-
7
2
0
-
a
1
a
,
a
1
b
,
a
1
b
d
,
b
1
a
,
b
1
b
,
b
1
b
d
,
c
1
b
,
d
1
b
,
d
1
c
,
c
1
b
d
,
d
1
b
d
,
d
1
c
d
,
i
o
-
5
4
0
-
a
1
a
5
,
a
a
1
a
5
,
a
a
1
b
5
,
a
b
1
a
5
,
b
1
a
5
,
b
1
b
5
,
b
1
c
5
,
c
1
b
5
,
c
1
c
5
,
c
2
c
,
c
4
b
5
d
,
c
4
c
5
,
c
4
d
5
,
c
4
b
5
,
c
4
d
5
d
,
d
4
a
5
,
d
4
b
5
,
d
4
c
5
,
e
1
b
5
,
e
1
a
5
,
e
1
c
5
,
g
1
a
5
,
g
1
b
5
,
g
1
c
5
,
g
1
d
5
,
g
1
e
5
,
g
1
f
5
,
j
4
a
5
,
k
1
g
5
d
,
k
1
a
5
d
,
k
1
g
5
,
k
1
a
5
,
k
1
j
5
,
k
1
f
5
,
k
1
b
5
,
k
1
b
5
d
,
k
1
c
5
,
k
1
d
5
,
k
1
e
5
,
k
1
e
5
,
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
a
1
a
d
,
a
b
1
a
d
,
a
e
2
a
,
a
f
1
a
,
c
1
a
,
e
1
a
,
f
2
b
d
,
g
1
a
,
h
1
a
,
j
2
b
,
j
2
b
d
,
k
1
a
d
,
n
2
b
d
,
r
2
a
d
,
s
1
a
d
,
t
2
a
d
,
u
2
a
,
v
2
a
d
,
w
2
a
,
k
1
f
5
d
,
k
1
h
5
,
k
1
j
5
d
,
k
1
k
5
,
k
2
a
5
,
l
1
a
5
,
l
1
a
5
d
,
l
1
b
5
d
,
l
1
c
5
,
m
1
a
5
,
m
1
a
5
d
,
m
1
b
5
d
,
m
1
c
5
,
m
2
a
5
d
,
n
1
a
5
,
p
1
a
5
,
r
1
a
5
,
s
1
a
5
,
t
4
a
5
d
,
t
4
b
5
,
t
4
b
5
d
,
t
4
c
5
d
,
u
1
a
5
d
,
u
1
b
5
d
,
v
4
a
5
d
,
w
1
a
5
d
,
w
3
a
5
d
,
i
v
o
-
5
4
0
-
a
1
a
,
,
i
o
-
3
2
0
-
a
1
a
,
a
2
a
,
b
1
a
,
b
1
b
,
b
1
c
,
b
1
d
,
b
2
a
,
c
1
a
,
d
1
a
,
d
1
b
,
e
1
a
,
e
1
b
,
e
2
a
,
e
2
b
,
f
1
a
,
a
i
o
-
3
2
0
-
a
1
a
,
a
1
b
,
a
2
a
,
a
2
b
,
b
1
b
,
c
1
b
,
l
i
o
-
3
2
0
-
b
1
a
,
c
1
a
,
a
e
i
o
-
3
2
0
-
e
1
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,
)
View Item »
Part Number
Description
Alternate
installation of modified fuel injector nozzle kit no gl10
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
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g
(
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3
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)
View Item »
Part Number
Description
Alternate
installation of modified fuel injector nozzles kit
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
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g
(
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o
-
5
4
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2
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o
n
l
y
)
View Item »
Part Number
Description
Alternate
installation of modified fuel injector nozzles kit
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
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g
(
h
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)
View Item »
Part Number
Description
Alternate
installation of modified fuel injector nozzles kit
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
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o
-
3
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4
a
5
d
,
w
1
a
5
d
,
w
3
a
5
d
,
,
i
v
o
-
5
4
0
-
a
1
a
,
i
o
-
7
2
0
-
a
1
a
,
a
1
b
,
a
1
b
d
,
b
1
a
,
b
1
b
,
b
1
b
d
,
c
1
b
,
d
1
b
,
d
1
c
,
c
1
b
d
,
d
1
b
d
,
d
1
c
d
,
i
o
-
3
2
0
-
a
1
a
,
a
2
a
,
b
1
a
,
b
1
b
,
b
1
c
,
b
1
d
,
b
2
a
,
c
1
a
,
d
1
a
,
d
1
b
,
e
1
a
,
e
1
b
,
e
2
a
,
e
2
b
,
f
1
a
,
a
i
o
-
3
2
0
-
a
1
a
,
a
1
b
,
a
2
a
,
a
2
b
,
b
1
b
,
c
1
b
,
l
i
o
-
3
2
0
-
b
1
a
,
c
1
a
,
a
e
i
o
-
3
2
0
-
e
1
a
,
e
1
b
,
e
2
a
,
e
2
b
,
,
i
v
o
-
3
6
0
-
a
1
a
,
i
o
-
5
4
0
-
a
1
a
5
,
a
a
1
a
5
,
a
a
1
b
5
,
b
1
a
5
,
b
1
b
5
,
b
1
c
5
,
c
1
b
5
,
c
1
c
5
,
c
2
c
,
c
4
c
5
,
c
4
d
5
,
c
4
b
5
,
c
4
d
5
d
,
d
4
a
4
,
d
4
b
5
,
e
1
b
5
,
e
1
a
5
,
e
1
c
5
,
g
1
a
5
,
g
1
b
5
,
g
1
c
5
,
g
1
d
5
,
g
1
e
5
,
g
1
f
5
,
j
4
a
5
,
k
1
g
5
d
,
k
1
a
5
d
,
k
1
g
5
,
k
1
a
5
,
k
1
j
5
,
k
1
f
5
,
k
1
b
5
,
k
1
b
5
d
,
,
h
i
o
-
3
6
0
-
a
1
a
,
b
1
a
,
b
1
b
,
c
1
a
,
c
1
b
,
d
1
a
,
e
1
a
d
,
e
1
b
d
,
f
1
a
d
,
a
i
o
-
3
6
0
-
a
1
a
,
a
2
a
,
a
1
b
,
a
2
b
,
b
1
b
,
l
i
o
-
3
6
0
-
c
1
e
6
,
l
h
i
o
-
3
6
0
-
a
1
a
,
c
1
b
,
f
1
a
d
,
a
e
i
o
-
3
6
0
-
a
1
a
,
a
1
b
,
a
1
b
6
,
a
1
c
,
a
1
d
,
a
1
e
,
a
2
a
,
a
2
b
,
a
2
c
,
h
1
a
,
b
1
b
,
b
1
d
,
b
1
f
,
b
2
f
,
b
4
a
,
b
1
f
6
,
b
2
f
6
,
b
1
g
6
,
)
View Item »
Part Number
Description
Alternate
installation of turbocharger
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
i
o
-
3
6
0
-
a
1
b
6
,
i
o
-
3
6
0
-
a
1
b
6
d
)
View Item »
Part Number
Description
Alternate
intake hose
LYCOMING P/N 69603
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
y
c
o
m
i
n
g
o
-
3
2
0
-
a
2
b
,
a
2
c
,
a
2
d
,
a
3
b
,
b
2
b
,
b
2
c
,
b
3
b
,
d
1
a
,
d
1
d
,
d
1
f
,
d
2
a
,
d
2
b
,
d
2
c
,
d
2
g
,
d
2
j
,
d
3
g
,
e
1
a
,
e
1
f
,
e
2
a
,
e
2
b
,
e
2
c
,
e
2
d
,
e
2
f
,
e
2
g
,
e
2
h
,
e
3
d
,
e
3
h
,
o
-
3
6
0
-
a
2
a
,
a
3
a
,
a
1
c
,
a
1
d
,
a
2
d
,
a
2
e
,
b
2
a
,
c
2
a
,
c
2
c
,
c
2
d
,
d
2
a
,
d
2
b
,
i
o
-
3
6
0
-
b
1
a
,
b
1
b
,
h
i
o
-
3
6
0
-
b
1
a
,
o
-
5
4
0
-
f
1
b
5
)
View Item »
Part Number
Description
Alternate
intake hose
LYCOMING P/N STD-1196
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
y
c
o
m
i
n
g
o
-
3
2
0
-
a
2
a
,
a
2
b
,
a
2
c
,
a
2
d
,
a
3
a
,
a
3
b
,
a
3
c
,
b
2
a
,
b
2
b
,
b
3
a
,
b
3
b
,
b
3
c
,
i
o
-
3
2
0
-
e
2
a
)
View Item »
Part Number
Description
Alternate
intake hose
LYCOMING P/N STD-1792
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
y
c
o
m
i
n
g
i
g
o
-
5
4
0
,
i
g
s
o
-
5
4
0
)
View Item »
Part Number
Description
Alternate
intake hose clamp
LYCOMING P/N STD-1530
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
y
c
o
m
i
n
g
o
-
3
2
0
-
a
2
b
,
a
2
c
,
a
2
d
,
a
3
b
,
b
2
b
,
b
2
c
,
b
3
b
,
d
1
a
,
d
1
d
,
d
1
f
,
d
2
a
,
d
2
b
,
d
2
c
,
d
2
g
,
d
2
j
,
d
3
g
,
e
1
a
,
e
1
c
,
e
1
f
,
e
2
a
,
e
2
b
,
e
2
c
,
e
2
d
,
e
2
f
,
e
2
g
,
e
2
h
,
e
3
d
,
e
3
h
,
i
o
-
3
2
0
-
b
1
a
,
b
1
c
,
c
1
a
,
d
1
a
,
l
i
o
-
3
2
0
-
b
1
a
,
c
1
a
,
o
-
3
6
0
-
a
2
a
,
a
3
a
,
a
1
c
,
a
1
d
,
a
2
d
,
a
2
e
,
b
2
a
,
c
2
a
,
c
2
c
,
c
2
d
,
d
2
a
,
d
2
b
,
i
o
-
3
6
0
-
b
1
a
,
b
1
b
,
b
1
a
,
b
1
b
,
h
i
o
-
3
6
0
-
b
1
a
,
o
-
5
4
0
-
f
1
b
5
,
i
g
o
-
5
4
0
,
i
g
s
o
-
5
4
0
)
View Item »
Part Number
Description
Alternate
intake hose clamp
LYCOMING P/N STD-1269, OR LW-15592-8-98
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
y
c
o
m
i
n
g
o
-
3
2
0
-
a
2
a
,
a
2
b
,
a
2
c
,
a
2
d
,
a
3
a
,
a
3
b
,
a
3
c
,
b
2
a
,
b
2
b
,
b
3
a
,
b
3
b
,
b
3
c
,
i
o
-
3
2
0
-
e
2
a
,
i
g
o
-
5
4
0
,
i
g
s
o
-
5
4
0
)
View Item »
Part Number
Description
Alternate
intake pipe
Textron Lycoming P/N 74084
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
t
o
-
3
6
0
-
c
1
a
6
d
i
o
-
3
2
0
-
d
1
a
,
-
d
1
b
o
-
3
2
0
-
a
2
b
,
-
d
1
a
,
-
d
1
f
,
-
d
2
a
,
-
d
2
b
,
-
d
2
c
,
-
d
2
g
,
-
d
2
j
,
-
d
3
g
,
-
e
1
a
,
-
e
1
f
,
-
e
2
a
,
-
e
2
b
,
-
e
2
c
,
-
e
2
d
,
-
e
2
f
,
-
e
2
h
,
-
e
3
d
,
-
e
3
h
)
View Item »
Part Number
Description
Alternate
intake pipe
Textron Lycoming P/N 70485
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
a
e
i
o
-
3
6
0
-
b
1
g
6
,
-
h
1
a
i
o
-
3
6
0
-
b
1
a
,
-
b
1
b
,
-
b
1
d
,
-
b
1
f
,
-
b
2
f
,
-
b
2
f
6
,
-
b
4
a
,
-
l
2
a
i
o
-
5
4
0
-
a
b
1
a
5
,
-
c
1
b
5
,
-
c
4
b
5
,
-
c
4
c
5
,
-
d
4
a
5
,
-
j
4
a
5
,
-
n
1
a
5
,
-
r
1
a
5
-
t
4
a
5
d
,
-
t
4
b
5
,
-
t
4
b
5
d
,
-
t
4
c
5
d
,
-
v
4
a
5
d
,
-
w
1
a
5
,
-
w
1
a
5
d
,
-
w
3
a
5
d
,
-
c
4
d
5
d
o
-
3
6
0
-
a
1
a
,
-
a
1
a
d
,
-
a
1
d
,
-
a
1
f
6
,
-
a
1
f
6
d
,
-
a
1
l
d
,
-
a
1
p
,
-
a
2
a
,
-
a
2
d
,
-
a
2
e
,
-
a
2
f
,
-
a
3
a
,
-
a
3
a
d
,
-
a
4
a
,
-
a
4
m
,
-
a
4
n
,
-
a
4
p
,
-
a
5
a
d
,
-
b
2
a
,
-
b
2
c
,
-
c
1
a
,
-
c
1
c
,
-
c
1
e
,
-
c
i
g
,
-
c
2
a
,
-
c
2
c
,
-
c
2
e
,
-
c
4
p
,
-
d
2
a
,
-
d
2
b
,
-
j
2
a
o
-
5
4
0
-
a
1
a
,
-
a
1
a
5
,
-
a
1
b
5
,
-
a
1
c
5
,
-
a
i
d
,
-
a
1
d
5
,
-
a
2
b
,
-
a
3
d
5
,
-
b
1
a
5
,
-
b
1
b
5
,
-
b
2
b
5
,
-
b
2
c
5
,
-
b
4
b
5
,
-
e
4
a
5
,
-
e
4
b
5
,
-
e
4
c
5
,
-
g
1
a
5
,
-
g
2
a
5
,
-
h
1
b
5
d
,
-
h
2
b
5
d
,
-
j
1
a
5
d
,
-
j
3
a
5
,
-
j
3
a
5
d
t
i
o
-
5
4
0
-
a
a
1
a
d
,
-
a
b
1
a
d
,
-
a
f
1
a
,
-
a
g
1
a
,
-
c
i
a
,
-
e
1
a
,
-
g
1
a
,
-
h
1
a
)
View Item »
Part Number
Description
Alternate
intercooler assembly
Modification
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
e
4
a
5
)
View Item »
Part Number
Description
Alternate
intercooler assembly
Modification Parts
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
t
1
0
-
5
4
1
-
e
1
a
4
&
-
e
1
c
4
)
View Item »
Part Number
Description
Alternate
intercooler flex duct
Modification
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
e
4
a
5
)
View Item »
Part Number
Description
Alternate
intercooler mt. bracket
Modification
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
e
4
a
5
)
View Item »
Part Number
Description
Alternate
intercooler naca duct
Modification
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
e
4
a
5
)
View Item »
Part Number
Description
Alternate
jaw, starter
Textron Lycoming 67605
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
g
o
-
4
8
0
-
d
1
a
,
g
1
b
6
,
g
s
o
-
4
8
0
-
a
1
a
6
,
a
2
a
6
,
b
1
a
6
,
b
1
b
6
,
b
1
c
6
,
b
1
j
6
,
b
2
d
6
,
i
g
s
o
-
4
8
0
-
a
1
a
6
,
a
1
b
6
,
a
1
e
6
,
a
1
f
6
,
i
g
o
-
5
4
0
,
i
g
s
o
-
5
4
0
)
View Item »
Part Number
Description
Alternate
key, valve
60009
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
t
i
o
-
5
4
0
,
t
i
o
-
5
4
1
,
t
i
g
o
-
5
4
1
,
i
o
-
7
2
0
,
o
-
4
3
5
,
g
o
-
4
3
5
,
v
o
-
4
3
5
,
t
v
o
-
4
3
5
,
o
-
2
3
5
,
o
-
2
9
0
,
o
-
3
2
0
,
i
o
-
3
2
0
,
l
i
o
-
3
2
0
,
a
i
o
-
3
2
0
,
a
e
i
o
-
3
2
0
,
o
-
3
4
0
,
o
-
3
6
0
,
i
o
-
3
6
0
,
l
o
-
3
6
0
,
a
e
i
o
-
3
6
0
,
t
o
-
3
6
0
,
l
t
o
-
3
6
0
,
v
o
-
3
6
0
,
i
v
o
-
3
6
0
,
h
o
-
3
6
0
,
h
i
o
-
3
6
0
,
g
s
o
-
4
8
0
,
g
o
-
4
8
0
,
i
g
s
o
-
4
8
0
,
o
-
5
4
0
,
i
o
-
5
4
0
,
a
e
i
o
-
5
4
0
,
v
o
-
5
4
0
,
i
v
o
-
5
4
0
,
t
i
v
o
-
5
4
0
,
i
g
o
-
5
4
0
,
i
g
s
o
-
5
4
0
)
View Item »
Part Number
Description
Alternate
kit brush assembly
MHB-2012S, as used in Kelly Aerospace/ Hartzell Engine Technologies MHB-4001 thru -4003, -4007, -4008, -4010 thru -4013, -4016 thru -4020 starter motors
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
i
o
-
7
2
0
-
a
,
-
b
,
-
c
,
-
d
)
View Item »
Part Number
Description
Alternate
kit, 4/8 cyl distributor gear, d-2000/d-3000 series
OEM
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
u
s
e
d
o
n
a
i
r
c
r
a
f
t
h
a
v
i
n
g
l
y
c
o
m
i
n
g
r
e
c
i
p
r
o
c
a
t
i
n
g
e
n
g
i
n
e
s
w
i
t
h
b
e
n
d
i
x
/
t
c
m
d
-
2
0
0
0
o
r
d
-
3
0
0
0
s
e
r
i
e
s
m
a
g
n
e
t
o
i
g
n
i
t
i
o
n
s
y
s
t
e
m
s
.
)
View Item »
Part Number
Description
Alternate
kit, cam, breaker, 4 lobe
OEM
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
u
s
e
d
o
n
a
i
r
c
r
a
f
t
h
a
v
i
n
g
l
y
c
o
m
i
n
g
r
e
c
i
p
r
o
c
a
t
i
n
g
e
n
g
i
n
e
s
w
i
t
h
t
c
m
/
b
e
n
d
i
x
s
-
1
2
0
0
s
e
r
i
e
s
,
8
c
y
l
m
a
g
n
e
t
o
i
g
n
i
t
i
o
n
s
y
s
t
e
m
s
.
)
View Item »
Part Number
Description
Alternate
kit, ignitioin system, s6ln-1227/1209, 35 degrees impulse, 3/4-20 gold-seal harness
Modification Part - Place Magneto and Ignition Harness in One Kit Part Number
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
b
2
c
5
,
e
4
c
5
,
g
1
a
5
,
g
2
a
5
,
i
o
-
5
4
0
-
d
4
b
5
,
g
1
c
5
,
k
1
a
5
,
k
1
b
5
,
a
e
i
o
-
5
4
0
-
d
4
b
5
)
View Item »
Part Number
Description
Alternate
kit, ignition harness, replacement lead assembly's
OEM
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
u
s
e
d
o
n
a
i
r
c
r
a
f
t
h
a
v
i
n
g
t
c
m
,
l
y
c
o
m
i
n
g
o
r
f
r
a
n
k
l
i
n
r
e
c
i
p
r
o
c
a
t
i
n
g
e
n
g
i
n
e
s
w
i
t
h
m
a
g
n
e
t
o
i
g
n
i
t
i
o
n
s
y
s
t
e
m
a
t
t
a
c
h
m
e
n
t
h
a
r
n
e
s
s
e
s
.
)
View Item »
