(d)  
Put an 8-inch piece of vinyl adhesive tape horizontally over the barricade tape below the static port holes, overlapping the two vertical strips of adhesive tape (see Fig. 205, step 4).

 (e)  
The barricade tape should be allowed to stream down so it is visible from the ground.

 S 842-032
 (8)  
Attach a red paper tag that has "STATIC PORTS COVERED" printed on it in black letters, to the top of the left control wheel in the flight deck with wire.

 S 842-026

 (9)  
Use plastic membranes to cover the components in Table 204. All components are identified in Fig. 201, 202 and 203.

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 12-40-00
 ALL  ú ú 01 Page 207 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ~................................................................. | TABLE 204 | ................................................................... | | | FIGURE | | DESCRIPTION | LOCATION | NUMBER | ...................................................................
 |Aileron Centering Mechanism Assembly  |  |  |
 |  Aileron Upper Reaction Support Assembly  |  |  |
 |  Bearing  | 1  | 201  |
 |  Bearing  | 2  | 201  |
 |  Bearing  | 3  | 201  |
 |  Lever Assembly  |  |  |
 |  Bearing  | 4  | 201  |
 |  Aileron Lower Reaction Support Assembly  |  |  |
 |  Bearing  | 5  | 201  |

 ................................................................... |Aileron Trim Mechanism | | | | Aileron Trim Actuator/Electrical Connector | 6 | 201 | ................................................................... |Aileron Position Sensor | | | | Transmitter/Electrical Connector | 7 | 202 | | Rod Assembly/Bearings | 8,9 | 202 | ................................................................... |Aileron Control Autopilot Actuator | | | | Autopilot Actuator/Electrical Connector | 10 | 202 | | Rod Assembly and Bearings | 11,12 | 202 | ................................................................... |Power Control - Aileron Control | | | Power Control Assembly (B System) | 30 | | | Bearing | 13 | 201 | | Bearing | 14 | 201 | | Support Assembly (Upper) | | | | Bearing | 15 | 201 | | Bearing | 16 | 201 | | Lever Assembly | | | | Bearing | 17 | 201 | | Power Control Assembly (A System) | 31 | | | Bearing | 18 | 201 | | Bearing | 19 | 201 | | Support Assembly (Lower) | | | | Bearing | 20 | 201 | | Support Assembly | | | | Bearing | 21 | 201 | | Lever Assembly | | | | Bearing | 22 | 201 |
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-40-00
 ALL  ú
 ú  01  Page 208
 ú  Jul 15/97 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ~................................................................. | TABLE 204 | ................................................................... | | | FIGURE | | DESCRIPTION | LOCATION | NUMBER | ...................................................................
 |Quadrant - Spoiler Control  |  |  |
 |  Shaft Assembly  |  |  |
 |  Bearing  | 23  | 203  |
 |  Support Assembly  |  |  |
 |  Bearing  | 24  | 203  |
 |  Cartridge Assembly  |  |  |
 |  Rod End Bearing  | 25  | 203  |
 |  Casing Assembly  |  |  |
 |  Rod End  | 26  | 203  |

 ................................................................... |Spoiler-Mixer Assembly | 27 | 203 | ................................................................... |Spoiler Ratio Changer Assembly | 28 | 203 | ................................................................... |Ground Spoiler Control Valve Assembly and | 29 | 203 | |Rod Bearings | | | 2.............................................…..........…........1
　
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