Page 106 of 110
Part Number
Description
Alternate
unknown
Airborne 211CW
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
l
i
o
-
3
6
0
,
g
o
-
4
3
5
,
t
i
o
-
5
4
1
)
View Item »
Part Number
Description
Alternate
unleaded and leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
b
1
a
5
,
b
1
b
5
,
b
1
d
5
,
b
2
a
5
,
b
2
b
5
,
b
2
c
5
,
b
4
a
5
,
b
4
b
5
)
View Item »
Part Number
Description
Alternate
unleaded and leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
3
2
0
-
b
1
a
,
b
1
b
,
b
2
a
,
b
2
b
,
b
2
c
,
b
3
a
,
b
3
b
,
b
3
c
,
d
1
a
,
d
1
b
,
d
1
c
,
d
1
d
,
d
1
f
,
d
2
a
,
d
2
b
,
d
2
c
,
d
2
f
,
d
2
g
,
d
2
h
,
d
2
j
,
d
3
g
)
View Item »
Part Number
Description
Alternate
unleaded and leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
3
6
0
-
b
1
a
,
b
1
b
,
b
2
a
,
b
2
b
,
d
1
a
,
d
2
a
,
d
2
b
)
View Item »
Part Number
Description
Alternate
unleaded and leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
k
2
a
,
-
k
2
b
,
-
k
2
c
,
-
l
2
a
,
-
l
2
c
,
-
m
1
)
View Item »
Part Number
Description
Alternate
unleaded and leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
3
2
0
,
a
1
a
,
a
2
b
,
a
2
a
,
a
2
b
,
a
2
c
,
a
2
d
,
a
3
a
,
a
3
b
,
a
3
c
,
c
1
a
,
c
1
b
,
c
2
a
,
c
2
b
,
c
2
c
,
c
3
a
,
c
3
b
,
c
3
c
,
e
1
a
,
e
1
b
,
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
,
e
1
j
)
View Item »
Part Number
Description
Alternate
unleaded or leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
c
,
o
-
2
3
5
-
c
1
,
-
c
1
b
,
-
e
1
,
-
e
1
b
,
-
c
1
c
,
-
c
1
a
,
-
h
2
c
,
-
c
2
a
,
-
c
2
b
,
-
c
2
c
,
-
e
2
a
,
-
e
2
b
)
View Item »
Part Number
Description
Alternate
unleaded or leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
5
4
0
-
b
1
a
5
,
b
1
b
5
,
b
1
d
5
,
b
2
a
5
,
b
2
b
5
,
b
2
c
5
,
b
4
a
5
,
b
4
b
5
)
View Item »
Part Number
Description
Alternate
unleaded or leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
c
,
o
-
2
3
5
-
c
1
,
-
c
1
b
,
-
e
1
,
-
e
1
b
,
-
c
1
c
,
-
c
1
a
,
-
h
2
c
,
-
c
2
a
,
-
c
2
b
,
-
c
2
c
,
-
e
2
a
,
-
e
2
b
)
View Item »
Part Number
Description
Alternate
unleaded or leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
3
2
0
,
a
1
a
,
-
a
1
b
,
a
2
a
,
a
2
b
,
a
2
c
,
a
2
d
,
a
3
a
,
a
3
b
,
a
3
c
,
c
1
a
,
c
1
b
,
c
2
a
,
c
2
b
,
c
2
c
,
c
3
a
,
c
3
b
,
c
3
c
,
e
1
a
,
e
1
b
,
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
,
e
1
j
)
View Item »
Part Number
Description
Alternate
unleaded or leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
9
0
,
-
a
,
-
a
p
,
-
b
,
(
o
-
2
9
0
-
1
)
,
-
c
(
o
-
2
9
0
-
3
)
,
-
c
p
,
-
d
,
(
o
-
2
9
0
-
1
1
)
,
-
d
2
,
-
d
2
a
,
-
d
2
b
,
-
d
2
c
)
View Item »
Part Number
Description
Alternate
unleaded or leaded automotive gasoline
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
9
0
,
-
a
,
-
a
p
,
-
b
,
(
o
-
2
9
0
-
1
)
,
-
c
(
o
-
2
9
0
-
3
)
,
-
c
p
,
-
d
,
(
o
-
2
9
0
-
1
1
)
,
-
d
2
,
-
d
2
a
,
-
d
2
b
,
-
d
2
c
)
View Item »
Part Number
Description
Alternate
v packing
Facet Marvel-Schebler 44-286
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
e
n
g
i
n
e
s
)
View Item »
Part Number
Description
Alternate
v packing
Facet Aerospace Prod. Co. Marvel/Schebler (Facet) 44-286
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
)
View Item »
Part Number
Description
Alternate
vacuum pump
Pesco 3P194, 3P-194-D, 3P-194-F, 3P-194-FA, 3P-194-G, 3P-194-LB, 3P-194-LC, 3P-194-M Airborne 200CC, 200CW, 200CC9,201, 202, 205, 206, 211CC, 211CC9, 212CW, 215CW, 215CC9, 216CW, 241CC, 242CW
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
2
3
5
-
a
,
-
b
,
-
b
p
-
c
,
-
c
1
,
-
c
1
a
,
-
c
1
c
,
-
c
2
b
,
-
c
2
c
,
-
e
1
,
-
e
1
b
,
-
e
2
a
,
-
e
2
b
,
-
f
1
,
-
f
1
b
,
-
f
2
a
,
-
f
2
b
,
-
g
1
,
-
g
1
b
,
-
g
2
a
,
-
g
2
b
,
-
h
2
c
,
-
j
2
a
,
-
j
2
b
,
-
k
2
a
,
-
k
2
b
,
-
k
2
c
,
-
l
2
a
,
-
l
2
c
,
-
n
2
c
,
-
m
1
,
o
2
9
0
,
o
2
9
0
-
a
,
-
a
p
,
-
b
,
-
c
,
-
d
,
-
d
2
a
,
-
d
2
c
,
-
d
2
b
,
o
3
2
0
-
-
a
1
a
,
-
a
1
b
,
-
a
2
a
,
-
a
2
b
,
-
a
2
c
,
-
a
2
d
,
-
a
3
a
,
-
a
3
b
,
-
a
3
c
,
-
b
1
a
,
-
b
2
a
,
-
b
2
b
,
-
b
2
c
,
-
b
3
a
,
-
b
3
b
,
-
b
3
c
,
-
c
1
a
,
-
c
1
b
,
-
c
2
a
,
-
c
2
b
,
-
c
2
c
,
-
c
3
a
,
-
c
3
b
,
-
c
3
c
,
-
d
1
a
,
-
d
1
b
,
-
d
1
c
,
-
d
1
d
,
-
d
1
f
,
-
d
2
a
,
-
d
2
b
,
-
d
2
c
,
-
d
2
f
,
-
d
2
g
,
-
d
2
h
,
-
d
2
j
,
-
d
3
g
,
-
e
1
a
,
-
e
1
b
,
-
e
1
c
,
-
e
1
f
,
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e
1
j
,
-
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
,
-
h
1
a
d
,
-
h
2
a
d
,
-
h
2
b
d
,
-
h
3
a
d
,
-
h
3
b
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
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,
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d
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a
,
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e
1
a
,
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e
1
b
,
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e
2
a
,
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e
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b
,
-
f
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a
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l
i
o
3
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0
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b
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c
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a
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,
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a
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,
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a
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b
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c
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o
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e
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e
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3
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a
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a
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a
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a
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a
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a
4
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a
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a
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c
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c
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c
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f
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l
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6
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a
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b
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i
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3
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a
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b
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c
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c
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1
b
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f
1
a
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l
h
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3
6
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c
1
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c
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l
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3
6
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c
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a
e
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3
6
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a
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a
2
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a
1
b
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a
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a
1
c
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a
2
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a
1
b
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a
1
d
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a
1
e
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-
b
1
b
,
-
b
1
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,
-
b
1
f
,
-
b
2
f
,
-
b
4
a
,
-
b
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-
c
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o
7
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a
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d
1
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View Item »
Part Number
Description
Alternate
vacuum pump model 1u128b
Installed Vcuum pump on engines listed in FAA approved Sigma Tek Installation Procedures
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
v
a
r
i
o
u
s
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
l
i
s
t
e
d
i
n
s
i
g
m
a
t
e
k
i
n
s
t
a
l
l
a
t
i
o
n
p
r
o
c
e
d
u
r
e
s
r
e
v
1
6
d
a
t
e
d
1
0
/
2
0
/
9
2
f
a
a
a
p
p
r
o
e
d
1
1
/
1
7
/
9
2
)
View Item »
Part Number
Description
Alternate
vacuum pump, model 1u22 ( )
Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
v
a
r
i
o
u
s
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
l
i
s
t
e
d
i
n
s
i
g
m
a
t
e
k
i
n
s
t
a
l
l
a
t
i
o
n
p
r
o
c
e
d
u
r
e
r
e
v
.
6
d
t
d
6
/
1
0
/
7
4
f
a
a
a
p
p
r
o
v
e
d
7
/
3
/
7
4
)
View Item »
Part Number
Description
Alternate
vacuum system
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
s
e
e
f
a
a
a
p
p
r
o
v
e
d
a
m
l
f
o
r
m
o
d
e
l
)
View Item »
Part Number
Description
Alternate
vacuum system
Modification Part
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
s
e
e
f
a
a
a
p
p
r
o
v
e
d
a
m
l
f
o
r
m
o
d
e
l
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive Facet/Marvel-Schebler 34-91 Consolidated Fuel Systems CF34-91)
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
r
e
p
l
a
c
e
m
e
n
t
p
a
r
t
f
o
r
p
r
e
c
i
s
i
o
n
a
i
r
m
o
t
i
v
e
f
a
c
e
t
/
m
a
r
v
e
l
-
s
c
h
e
b
l
e
r
3
4
-
9
1
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
)
View Item »
Part Number
Description
Alternate
valve
Textron Lycoming 66531
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
3
5
-
c
,
o
-
2
9
0
-
d
,
o
-
2
9
0
-
d
2
)
View Item »
Part Number
Description
Alternate
valve
Textron Lycoming 66429
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
1
b
,
c
2
b
,
o
-
2
9
0
-
d
)
View Item »
Part Number
Description
Alternate
valve
Textron Lycoming LW11901
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
1
b
,
c
2
a
,
c
2
b
,
c
2
c
,
e
2
a
,
f
1
b
,
f
2
a
,
f
2
b
,
g
1
a
,
g
2
a
,
h
2
c
,
j
2
a
,
k
2
a
,
k
2
b
,
k
2
c
,
l
2
a
,
l
2
c
,
m
1
,
m
2
,
n
2
c
,
p
1
,
p
2
a
,
p
2
c
,
p
3
c
,
t
h
e
f
o
l
l
o
w
i
n
g
e
l
i
g
i
b
l
e
a
f
t
e
r
c
o
m
p
l
i
a
n
c
e
w
i
t
h
l
y
c
o
m
i
n
g
s
e
r
v
i
c
e
i
n
s
t
r
u
c
t
i
o
n
n
o
.
1
2
4
6
:
o
-
2
9
0
-
d
,
d
2
,
d
2
b
,
d
2
c
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive Bendix 2541265 Consolidated Fuel Systems CF2541265
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
a
e
i
o
-
3
2
0
s
e
r
i
e
s
a
e
i
o
-
5
4
0
-
d
4
a
5
a
e
i
o
-
3
6
0
s
e
r
i
e
s
a
i
o
-
3
2
0
s
e
r
i
e
s
a
i
o
-
3
6
0
s
e
r
i
e
s
h
i
o
-
3
6
0
s
e
r
i
e
s
i
o
-
3
2
0
s
e
r
i
e
s
i
o
-
3
6
0
s
e
r
i
e
s
i
o
-
5
4
0
-
c
1
b
5
,
c
1
c
5
,
c
1
d
6
,
c
4
b
5
,
c
4
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5
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4
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f
1
a
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c
,
c
1
a
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)
View Item »
Part Number
Description
Alternate
valve
Textron Lycoming 73938
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
o
-
2
9
0
,
o
-
3
2
0
,
i
o
-
3
2
0
,
l
i
o
-
3
2
0
,
a
e
i
o
-
3
2
0
,
a
i
o
-
3
2
0
,
o
-
3
4
0
,
o
-
3
6
0
,
l
o
-
3
6
0
,
t
o
-
3
6
0
,
l
t
o
-
3
6
0
,
i
o
-
3
6
0
,
t
i
o
-
3
6
0
,
h
o
-
3
6
0
,
h
i
o
-
3
6
0
,
a
e
i
o
-
3
6
0
,
o
-
5
4
0
,
i
o
-
5
4
0
,
t
i
o
-
5
4
0
,
l
t
i
o
-
5
4
0
,
a
e
i
o
-
5
4
0
)
View Item »
Part Number
Description
Alternate
valve
Facet Marvel-Schebler 34-91
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
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive Facet/Marvel-Schebler 14-190 Consolidated Fuel Systems CF14-190)
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
r
e
p
l
a
c
e
m
e
n
t
p
a
r
t
f
o
r
p
r
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c
i
s
i
o
n
a
i
r
m
o
t
i
v
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f
a
c
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t
/
m
a
r
v
e
l
-
s
c
h
e
b
l
e
r
1
4
-
1
9
0
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive/ Bendix 2541564 (Consolidated Fuel Systems CF2541564)
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
r
e
p
l
a
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t
p
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p
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c
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o
n
a
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r
m
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t
i
v
e
/
b
e
n
d
i
x
p
/
n
2
5
4
1
5
6
4
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
.
)
View Item »
Part Number
Description
Alternate
valve
Textron Lycoming LW13622
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
i
o
-
3
6
0
,
t
o
-
3
6
0
,
t
i
o
-
3
6
0
,
g
o
-
4
3
5
,
v
o
-
4
3
5
,
g
o
-
4
8
0
,
g
s
o
-
4
8
0
,
i
o
-
5
4
0
,
t
i
o
-
5
4
0
,
i
g
s
o
-
5
4
0
,
i
o
-
7
2
0
s
e
r
i
e
s
)
View Item »
Part Number
Description
Alternate
valve
Facet Marvel-Schebler 34-91
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive/ Bendix 2541265 (Consolidated Fuel Systems CF2541265)
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
r
e
p
l
a
c
e
m
e
n
t
p
a
r
t
f
o
r
p
r
e
c
i
s
i
o
n
a
i
r
m
o
t
i
v
e
/
b
e
n
d
i
x
p
/
n
2
5
4
1
2
6
5
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
.
)
View Item »
Part Number
Description
Alternate
valve
Textron Lycoming LW16740
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
g
s
o
-
4
8
0
,
i
o
-
3
6
0
,
t
o
-
3
6
0
,
t
i
o
-
3
6
0
,
g
o
-
4
3
5
,
v
o
-
4
3
5
,
g
o
-
4
8
0
,
i
o
-
5
4
0
,
t
i
o
-
5
4
0
,
i
g
s
o
-
5
4
0
,
i
o
-
7
2
0
s
e
r
i
e
s
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive/ Bendix 2541562 (Consolidated Fuel Systems CF2541562)
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
r
e
p
l
a
c
e
m
e
n
t
p
a
r
t
f
o
r
p
r
e
c
i
s
i
o
n
a
i
r
m
o
t
i
v
e
/
b
e
n
d
i
x
p
/
n
2
5
4
1
5
6
2
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
.
)
View Item »
Part Number
Description
Alternate
valve
Facet Marvel-Schebler 14-190
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
e
n
g
i
n
e
s
)
View Item »
Part Number
Description
Alternate
valve
Precision Airmotive/ Bendix 2541563 (Consolidated Fuel Systems CF2541563)
Applicable aircraft models: t
e
x
t
r
o
n
l
y
c
o
m
i
n
g
(
r
e
p
l
a
c
e
m
e
n
t
p
a
r
t
f
o
r
p
r
e
c
i
s
i
o
n
a
i
r
m
o
t
i
v
e
/
b
e
n
d
i
x
p
/
n
2
5
4
1
5
6
3
w
h
e
n
i
n
s
t
a
l
l
e
d
o
n
l
y
c
o
m
i
n
g
e
n
g
i
n
e
s
.
)
View Item »
