Mooney M20R - Skin Specifications; Wing Skin Panels View

MOONEY
AIRCRAFT
CORPORATION
M20R
SERVICE
AND
MAINTENANCE
MANUAL
20-00-00
GENERAL
tification.
Advisory
Circular
43.13-1(
outlines
inspec-
tion
and
repair
practices
acceptable
to
the
F.A.A.
Ad-
This
chapter
of
the
manual
discusses
treatment
of
ministrator.
metal surfaces
for
corrosion
control
and
the
identifica-
tion
of
skin
panels
for
replacement
purposes.
Those
20-80-01
SKIN
SPECIFICATIONS
who
inspect
or
repair
aircraft
should
consult
FAR
43,
Maintenance,
Preventive
Maintenance,
Rebuilding
and
Alteration
and
Sub Parts
A,
D
and
E of
FAR
65,
Cer-
6
r5
r4
r3
STA
I I
STA
I
STA
I
STA
I
STA
210~971 1
147,75
1
103,50
1
59,25
24~50
STA
193~50
18
15
19
13
12
17
11
10
I
14
--J
L9
WING
SKIN
PANELS
INDEX-
SKIN
.MATERIAL
INDEX
SKIN
MATERIAL
NO.
THICKNESS
NO.
.THICKNESS
1.
0.063
2024
T-3
CLAD
12.
0.025(c)
2024
T-3
CLAD
2.
0.050
2024
T-3
CLAD
13.
0.020(a)
2024
T-3
CLAD
3.
0.040
2024
T-3
CLAD
14.
0.032
2024
T-3
CLAD
2024
T-3
CLAD
6.
0.025
2024
T-3
CLAD
17.
0.016
2024
T-3
CLAD
4.
0.040
2024
T-3
CLAD
15.
0.040
5.
0 025
2024
T-3
CLAD
16.
0.040
2024
T-3
CLAD
7.
8.832
2324
T-3
CLAD
18.
0.050
2024
T-3
CLAD
8.
0.848
21124
T-3
CLAD
19.
Polyester
Glass-Fiber
keinforced
9.
0.025
2024
T-3
CLAD
10.
0.625
2024
T-3
CLAD
11.
0.025
2024
T-3
CLAD
(a)
Same
thickness
on
top
and bottom.
(b)
Top
of
wing
only.
(c)
Top
aft
flap
skin
that
section).
(d)
Top
inboard
flap
skin.
WING SKIN
PANELS
FIGURE
20-1
28-00-00
Island Enterprises