Page 257 of 340
reinforcement - landing gear cabane vee
Piper 30411
app-acft: p
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p
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عرض المادة »
reinforcement - landing gear cabane vee
Piper 30411-2
app-acft: p
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p
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(
j
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3
,
j
3
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عرض المادة »
reinforcement - landing gear cabane vee
Piper 30411 and 30411-2
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3
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عرض المادة »
reinforcement aileron trailing edge
modification part
app-acft: p
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p
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3
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p
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عرض المادة »
reinforcement aileron trailing edge
modification part
app-acft: p
i
p
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(
j
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3
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p
a
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1
1
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p
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p
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1
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1
8
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1
5
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8
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5
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عرض المادة »
reinforcement aileron trailing edge
modification part
app-acft: p
i
p
e
r
(
j
-
3
,
p
a
-
1
1
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p
a
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p
a
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1
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p
a
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1
8
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p
a
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1
8
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1
0
5
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a
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1
8
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1
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1
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1
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p
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1
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p
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p
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1
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p
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p
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1
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1
5
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8
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"
1
5
0
,
p
a
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1
8
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5
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)
عرض المادة »
reinforcing bracket fitting assembly
Not Applicable - Modification Part
reinforcing bracket fitting assembly
Not Applicable - Modification Part
app-acft: p
i
p
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r
(
p
a
-
1
8
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p
a
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1
8
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,
p
a
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1
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1
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5
"
,
p
a
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1
8
s
"
1
0
5
"
,
p
a
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1
8
a
,
p
a
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1
8
"
1
2
5
"
,
p
a
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1
8
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"
1
2
5
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,
p
a
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1
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1
2
5
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,
p
a
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1
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1
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5
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p
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5
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1
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5
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,
p
a
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1
9
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p
a
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1
9
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)
عرض المادة »
reinforcing plate
2E1193
app-acft: p
i
p
e
r
(
p
a
-
3
2
-
2
6
0
,
-
3
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p
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d
p
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s
t
c
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2
4
9
8
w
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)
عرض المادة »
reinforcing ring
Modification Parts
reinforcing ring
Modification Parts
relay box assembly
Modification Part
app-acft: p
i
p
e
r
(
p
a
-
2
4
-
1
8
0
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p
a
-
2
4
-
2
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p
a
-
2
4
-
2
6
0
,
p
a
-
2
4
-
2
6
0
b
)
عرض المادة »
remote compass mounting bracket
Modification Part
app-acft: p
i
p
e
r
(
j
-
3
t
h
r
o
u
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p
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2
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t
c
s
a
1
4
4
a
l
i
n
s
t
a
l
l
e
d
)
عرض المادة »
remote compass mounting bracket
Modification Part
remote mount oil filter kit
Modification Part
remote mount oil filter kit
Modification Part
removable bar kit
Modification Part
removable bar kit
Modification Part
removable crossbar
Modification Part
app-acft: p
i
p
e
r
(
p
a
-
1
8
1
0
5
1
2
5
1
3
5
1
5
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p
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1
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1
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1
5
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t
c
s
a
6
8
1
a
l
i
n
s
t
a
l
l
e
d
)
عرض المادة »
removable folding seat
Modification Part
removable panel, instrument panel
Modification Part
app-acft: p
i
p
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r
(
p
a
-
1
8
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p
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1
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s
t
c
s
a
1
4
3
a
l
i
n
s
t
a
l
l
e
d
)
عرض المادة »
removable panel, instrument panel
Modification Part
replacement fuselage
Modification Part
app-acft: p
i
p
e
r
(
p
a
-
1
8
,
p
a
-
1
8
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p
a
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1
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p
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1
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1
0
5
(
s
p
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c
i
a
l
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p
a
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1
8
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1
0
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s
p
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c
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p
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1
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2
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(
a
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p
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1
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1
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1
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(
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p
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1
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1
8
a
1
5
0
,
p
a
-
1
8
a
s
1
5
0
)
عرض المادة »
replacement fuselage assembly
Modification Part
replacement skis and rigging hardware
Modification Part
app-acft: p
i
p
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r
(
p
a
-
1
8
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5
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p
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t
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3
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1
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s
t
a
l
l
e
d
)
عرض المادة »
replacment of aft fuselage section
Modification Part
app-acft: p
i
p
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r
(
p
a
-
1
8
,
p
a
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1
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(
s
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p
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s
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(
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p
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1
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1
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p
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(
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p
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1
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1
5
0
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p
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1
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1
5
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)
عرض المادة »
retainer
Modification Part
app-acft: p
i
p
e
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(
j
2
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j
3
c
s
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r
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3
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عرض المادة »
retainer
Modification Part
app-acft: p
i
p
e
r
(
p
a
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2
8
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1
4
0
,
p
a
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2
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a
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2
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2
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1
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(
h
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p
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1
(
s
p
)
,
p
a
-
3
2
r
-
3
0
1
t
,
p
a
-
3
2
r
t
-
3
0
0
,
p
a
-
3
2
r
t
-
3
0
0
t
,
p
a
-
3
4
-
2
0
0
,
p
a
-
3
4
-
2
0
0
t
,
p
a
-
3
4
-
2
2
0
t
)
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retainer
Modification Part
retainer strip
Modification Part
retract cylinder, main gear
Piper Aircraft Corporation 96860-02 (455 994)
app-acft: p
i
p
e
r
(
p
a
-
2
8
r
-
2
0
1
,
p
a
-
2
8
r
-
2
0
1
t
,
p
a
-
2
8
r
t
-
2
0
1
,
p
a
-
2
8
r
t
-
2
0
1
t
,
p
a
-
3
2
r
-
3
0
1
(
s
p
)
,
p
a
-
3
2
r
-
3
0
1
(
h
p
)
,
p
a
-
3
2
r
-
3
0
1
t
,
p
a
-
4
4
-
1
8
0
,
p
a
-
4
4
-
1
8
0
t
,
)
عرض المادة »
retract cylinder, nose gear
Piper Aircraft Corporation 35797-03 (455 997) Piper Specification No. PS50001-7
retract cylinder, nose gear
Piper Aircraft Corporation 35797-05 (455 987) Piper Specification No. PS50001-9
app-acft: p
i
p
e
r
(
p
a
-
2
8
r
-
2
0
1
t
,
p
a
-
3
2
r
-
3
0
1
(
s
p
)
,
p
a
-
3
2
r
-
3
0
1
(
h
p
)
,
p
a
-
3
2
r
-
3
0
1
t
,
p
a
-
4
4
-
1
8
0
,
p
a
-
4
4
-
1
8
0
t
)
عرض المادة »
retractor brackets kit
Modification Part
app-acft: p
i
p
e
r
(
p
a
-
3
4
-
2
0
0
,
-
2
0
0
t
-
2
2
0
t
p
a
-
4
4
-
1
8
0
-
1
8
0
t
)
عرض المادة »
retractor brackets kit (piper pa-28)
Modification Part
app-acft: p
i
p
e
r
(
p
a
-
3
2
-
2
6
0
,
-
3
0
0
,
-
3
0
1
,
-
3
0
1
t
,
-
3
0
1
f
t
,
-
3
0
1
x
t
c
,
p
a
-
3
2
r
-
3
0
0
,
-
3
0
1
(
s
p
)
,
-
3
0
1
(
h
p
)
,
-
3
0
1
t
,
p
a
-
3
2
r
t
-
3
0
0
,
-
3
0
0
t
,
p
a
-
3
2
s
-
3
0
0
)
عرض المادة »
