Page 299 of 340
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
r
-
2
0
0
,
s
/
n
2
8
r
-
7
2
3
5
0
0
1
a
n
d
u
p
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
4
-
4
0
0
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
2
6
0
a
n
d
p
a
-
3
2
-
3
0
0
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
r
-
3
0
0
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
3
-
2
5
0
a
n
d
p
a
-
e
2
3
-
2
5
0
,
s
/
n
2
7
-
2
0
0
0
t
h
r
o
u
g
h
s
/
n
2
7
-
7
5
5
4
1
7
2
a
n
d
t
h
e
a
b
o
v
e
m
o
d
e
l
s
w
h
e
n
e
q
u
i
p
p
e
d
w
i
t
h
a
p
p
r
o
v
e
d
t
u
r
b
o
c
h
a
r
g
e
d
e
n
g
i
n
e
s
(
2
5
0
h
.
p
.
)
a
n
d
/
o
r
w
i
n
g
t
i
p
t
a
n
k
s
p
e
r
s
t
c
s
a
1
4
8
0
w
e
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
r
-
3
0
1
a
n
d
p
a
-
3
2
r
-
3
0
1
t
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
0
a
n
d
p
a
-
3
9
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
1
4
0
,
p
a
-
2
8
-
1
5
0
,
p
a
-
2
8
-
1
6
0
,
p
a
-
2
8
-
1
8
0
a
n
d
p
a
-
2
8
-
2
3
5
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
2
0
1
t
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
3
-
2
5
0
a
n
d
p
a
-
e
2
3
-
2
5
0
,
s
/
n
2
7
-
2
0
0
0
t
h
r
o
u
g
h
s
/
n
2
7
-
7
5
5
4
1
7
2
a
n
d
t
h
e
a
b
o
v
e
m
o
d
e
l
s
w
h
e
n
e
q
u
i
p
p
e
d
w
i
t
h
a
p
p
r
o
v
e
d
t
u
r
b
o
-
c
h
a
r
g
e
d
e
n
g
i
n
e
s
(
2
5
0
h
.
p
.
)
a
n
d
/
o
r
w
i
n
g
t
i
p
t
a
n
k
s
p
e
r
s
t
c
s
a
1
4
8
0
w
e
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
4
-
2
0
0
t
a
n
d
p
a
-
3
4
-
2
2
0
t
)
View Item »
Part Number
Description
Alternate
system 40/50 single and two axis flight guidance system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
3
0
1
a
n
d
p
a
-
3
2
-
3
0
1
t
)
View Item »
Part Number
Description
Alternate
system 40x/50x single and two axis automatic flight guidance systems
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
4
(
p
a
-
2
4
-
1
8
0
)
,
p
a
-
2
4
-
2
5
0
,
p
a
-
2
4
-
2
6
0
,
a
n
d
p
a
-
2
4
-
4
0
0
)
View Item »
Part Number
Description
Alternate
system 40x/50x single and two axis automatic flight guidance systems
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
2
6
0
,
p
a
-
3
2
-
3
0
0
,
a
n
d
p
a
-
3
2
r
-
3
0
0
)
View Item »
Part Number
Description
Alternate
system 55/55x two axis automatic flight control system kit
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
3
0
1
,
p
a
-
3
2
-
3
0
1
t
,
p
a
3
2
r
-
3
0
1
,
p
a
-
3
2
r
-
3
0
1
t
,
p
a
-
3
2
-
3
0
1
f
t
,
p
a
-
3
2
-
3
0
1
x
t
c
)
View Item »
Part Number
Description
Alternate
system 55/55x two axis automatic flight control system kit
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
3
0
1
,
p
a
-
3
2
-
3
0
1
t
,
p
a
3
2
r
-
3
0
1
,
p
a
-
3
2
r
-
3
0
1
t
,
p
a
-
3
2
-
3
0
1
f
t
,
p
a
-
3
2
-
3
0
1
x
t
c
)
View Item »
Part Number
Description
Alternate
system 550 flight director/autopilot with trim, yaw damper, and altitude selector alerter
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
4
6
-
5
0
0
t
p
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
3
0
1
a
n
d
p
a
-
3
2
-
3
0
1
t
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
4
-
2
0
0
t
a
n
d
p
a
-
3
4
-
2
2
0
t
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
r
-
2
0
0
,
s
/
n
2
8
r
-
7
2
3
5
0
0
1
a
n
d
u
p
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
1
4
0
,
p
a
-
2
8
-
1
5
0
,
p
a
-
2
8
-
1
6
0
,
a
n
d
p
a
-
2
8
-
1
8
0
,
s
/
n
2
8
-
1
t
h
r
o
u
g
h
s
/
n
2
8
-
7
2
0
5
3
1
8
a
n
d
p
a
-
2
8
-
2
3
5
,
s
/
n
2
8
-
1
0
0
0
3
t
h
r
o
u
g
h
s
/
n
2
8
-
7
2
1
0
0
2
3
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
r
-
3
0
1
a
n
d
p
a
-
3
2
r
-
3
0
1
t
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
r
-
3
0
0
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
2
-
2
6
0
a
n
d
p
a
-
3
2
-
3
0
0
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
r
t
-
2
0
1
a
n
d
p
a
-
2
8
r
t
-
2
0
1
t
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
3
-
2
5
0
a
n
d
p
a
-
e
2
3
-
2
5
0
,
s
/
n
2
7
-
2
0
0
0
t
h
r
o
u
g
h
s
/
n
2
7
-
7
5
5
4
1
7
2
a
n
d
t
h
e
a
b
o
v
e
m
o
d
e
l
s
w
h
e
n
e
q
u
i
p
p
e
d
w
i
t
h
a
p
p
r
o
v
e
d
t
u
r
b
o
c
h
a
r
g
e
d
e
n
g
i
n
e
s
{
2
5
0
h
.
p
.
)
a
n
d
/
o
r
w
i
n
g
t
i
p
t
a
n
k
s
p
e
r
s
t
c
s
a
1
4
8
0
w
e
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
4
-
4
0
0
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
4
-
2
0
0
t
a
n
d
p
a
-
3
4
-
2
2
0
t
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
1
5
1
,
p
a
-
2
8
-
1
6
1
,
p
a
-
2
8
-
1
8
1
,
a
n
d
p
a
-
2
8
-
2
3
6
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
3
0
a
n
d
p
a
-
3
9
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
3
-
2
5
0
a
n
d
p
a
-
e
2
3
-
2
5
0
,
s
/
n
2
7
-
2
0
0
0
t
h
r
o
u
g
h
s
/
n
2
7
-
7
5
5
4
1
7
2
a
n
d
t
h
e
a
b
o
v
e
m
o
d
e
l
s
w
h
e
n
e
q
u
i
p
p
e
d
w
i
t
h
a
p
p
r
o
v
e
d
t
u
r
b
o
c
h
a
r
g
e
d
e
n
g
i
n
e
s
(
2
5
0
h
.
p
.
)
a
n
d
/
o
r
w
i
n
g
t
i
p
t
a
n
k
s
p
e
r
s
t
c
s
a
1
4
8
0
w
e
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
1
5
1
,
p
a
-
2
8
-
1
6
1
,
p
a
-
2
8
-
1
8
1
,
a
n
d
p
a
-
2
8
-
2
3
6
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
1
4
0
,
p
a
-
2
8
-
1
5
0
,
p
a
-
2
8
-
1
6
0
a
n
d
p
a
-
2
8
-
1
8
0
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
Modification Part
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
r
-
2
0
1
a
n
d
p
a
-
2
8
r
-
2
0
1
t
)
View Item »
Part Number
Description
Alternate
system 60 pitch stabilization system
-
Applicable aircraft models: p
i
p
e
r
(
p
a
-
2
8
-
1
4
0
,
p
a
-
2
8
-
1
5
0
,
p
a
-
2
8
-
1
6
0
,
p
a
-
2
8
-
1
8
0
,
s
/
n
2
8
-
1
t
h
r
o
u
g
h
s
/
n
2
8
-
7
2
0
5
3
1
8
a
n
d
p
a
-
2
8
-
2
3
5
,
s
/
n
2
8
-
1
0
0
0
3
t
h
r
o
u
g
h
s
/
n
2
8
-
7
2
1
0
0
2
3
)
View Item »
