Mooney M20V - Page 128

MOONEY INTERNATIONAL CORPORATION
M20V SERVICE AND MAINTENANCE MANUAL
Page
Date
5
MAR 2017
Rev Date
20-00-00 - GENERAL
This chapter of the manual discusses treatment of met-
al surfaces for corrosion control and the identification of
skin panels for replacement purposes. Those who in-
spect or repair aircraft should consult FAR 43, Mainte-
nance, Preventive Maintenance, Rebuilding and Alter-
ation and Sub Parts A, D and E of FAR 65, Certification.
Advisory Circular 43.13- 1( ) outlines inspection and re-
pair practices acceptable to the F.A.A. Administrator.
20-00-01 - SKIN SPECIFICATIONS
24.50
STA
59.25
STA
103.50
STA
147.75
STA
193.50
STA
210.97
STA
19
17
13
12
11
10
14
9
16
8
15
7
1
18
23
4
5
6
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............ ........... .......... .....
4. 0.040 2024 T- 3 CLAD 15. 0.040(b) 2024 T- 3 CLAD............ ........... ......... ....
5. 0.025 2024 T- 3 CLAD 16. 0.040(d) 2024 T- 3 CLAD............ ........... ......... ....
6. 0.025 2024 T- 3 CLAD 17. 0.016(a) 2024 T- 3 CLAD............ ........... ......... ....
7. 0.032 2024 T- 3 CLAD 18. 0.050(b) 2024 T- 3 CLAD............ ........... ......... ....
8. 0.040 2024 T- 3 CLAD 19. Polyester Glass- Fiber Reinforced............ ........... .
9. 0.025 2024 T- 3 CLAD (a) Same thickness on top and bottom............. ...........
10. 0.025 2024 T- 3 CLAD (b) Top of wing only............ ...........
11. 0.025 2024 T- 3 CLAD (c) Top aft flap skin (hat section)............ ...........
(d) Top inboard flap skin.
WING SKIN PANELS
FIGURE 20- 1
20-00-00