Mooney M20V - Page 473

MOONEY INTERNATIONAL CORPORATION
M20V SERVICE AND MAINTENANCE MANUAL
Date
MAR 2017
Rev Date
Page
9
B. Secure wing tip and drill holes to match existing
wing skins. Use clecoes as holes are drilled into new
tip. When all holes are drilled, remove wing tip assem-
bly and deburr.
C. Use CR3214- 4- 2 blind rivets to attach wing tip
to top and bottom skins.
D. Repaint to match aircraft.
E. Re- install navigation/strobe light assembly per
instructions provided in Chapter 33-41-03.
57-30-00 - PLATES - SKIN
The wing access and inspection covers shown in (Fig-
ure 57- 5) provide maintenance access to components,
plumbing and control bellcranks enclosed within wing.
They are flush mounted covers and when installed con-
tinue aerodynamic contour of wing.
-NOTE-
Access covers on bottom of wing that require
removal for inspection intervals are secured with
screws. Any access covers that are riveted in
place are required for manufacturing only and
NOT for routine inspections.
4
1
2
3
5
8
10
9
6
13
15
14
12
11
18
20
17
16
7
7
7
7
7
7
19
19
19
3
7
7
7
7
7
7
4
5
6
2
1
11. OAT PROBE - RIGHT WING ONLY
12. CONTROL TUBE GUIDE BLOCKS
13. PITOT POST - L EFT WING ONLY
14. STROBE LIGHT POWER SUPPLY
15. AILERON BELLCRANK AND CONTROL RODS
16. AUTO PILOT SERVOS
17. GYRO COMPASS FLUX VALVE - LEFT WING ONLY
18. MAIN LANDING GEAR ASSIST BUNGEE
BEARINGS, BELLCRANKS
20. DESCENT RATE CONTROL (SPEEDBRAKES)
1. WING SKIN - .050 THICKNESS (FUEL TANK)
2. WING SKIN - .040 THICKNESS (FUEL TANK)
3. WING SKIN - .040 THICKNESS
4. WING SKIN - .040 THICKNESS
5. WING SKIN - .025 THICKNESS
6. WING SKIN - .025 THICKNESS
7. FUEL TANK ACCESS
8. FUEL TANK FILLER
10. WING - FUSELAGE ATTACH POINTS
21. FLAP GAP SEALS (240026-003) (OPTIONAL)
22. FLAP GAP SEAL (240026-001) (OPTIONAL)
VIEW A
21
22
21
19. ELEVATOR AND RUDDER CONTROLS - ROD END
9. CONTROL TUBE BUIDE BLOCKS
WING SKINS AND INSPECTION COVER
FIGURE 57-5
57-30-00