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A

757
MAINTENANCE MANUAL

3. PCA INPUT  1. AILERON 
10. BOLT  LEVER  (ROD END FAIRING)  B 
11. WASHER 
12. NUT 
5. HYDRAULIC 
RETURN LINE 

2. PCA INPUT 21. TUBING
ROD SUPPORT BRACKETPCA FILTER
SEE B
9. HYDRAULIC PRESSURE LINE
4. PCA TO AILERON QUADRANT AND OVERRIDE MECHANISM
6.
 BOLT

7.
 WASHER (2) (4 LOCATIONS)

B
8. TRUNNION PCA
SUPPORT
C
22. TUBING SUPPORT BRACKET
23.
 SCREW HYDRAULIC

24.
 WASHER LINE

REACTION LINK
23. BOLT
ROD END
24. WASHER
HYDRAULIC LINE
CLAMP
PCA
ROD END
23.
 BOLT

24.
 WASHER

HYDRAULIC
LINE
RIGHT AILERON INBOARD PCA B-B
Aileron PCA Maintenance Figure 201 (Sheet 2)
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 27-11-20
 ALL  ú ú 01 Page 204 ú Jun 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 TASK 27-11-20-422-018
 3.  Aileron PCA and Reaction Link - Installation____________________________________________
 A. Equipment
 (1)
Rig Pins from set B20003-XX (Ref 20-10-24):

 (a)
A3 - P/N B20003-23

 (b)
A4 - P/N B20003-23

 (2)
Scale - accurate to 0.01 inch (0.25 mm), Commercially Available

 B.
Consumable Materials

 (1)
D00015 Grease, Corrosion Preventive - BMS 3-24

 (2)
A00247 Sealant, BMS 5-95

 C.
Parts ~.............................................................................. | AMM | | AIPC | .................. ........................... | FIG | ITEM | NOMENCLATURE | SUBJECT |FIG| ITEM | ................................................................................ | 201 | 4 | Left Aileron PCA | 27-11-20 |01 | 400 | | | 6 | Bolt | | | 375 | | | 7 | Washer | | | 380 | | | 10 | Bolt | | | 250 | | | 11 | Washer | | | 255 | | | 12 | Nut | | | 260 | | | 13 | Bushing | | | 390 | | | 14 | Nut | | | 370 | | | 15 | Washer | | | 365 | | | 16 | Washer | | | 360 | | | 17 | Bolt | | | 355 | | | 18 | Union | 27-11-20 |51 | 195 | | | 19 | Packing | | | 200 | | | 20 | Filter | | | 205 | 2.......…........…...................................…...........…...….........1

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757
MAINTENANCE MANUAL

 ~.............................................................................. | AMM | | AIPC | .................. ........................... | FIG | ITEM | NOMENCLATURE | SUBJECT |FIG| ITEM | ................................................................................ | 201 | 4 | Right Aileron PCA | 27-11-20 |02 | 340 | | | 6 | Bolt | | | 315 | | | 7 | Washer | | | 320 | | | 10 | Bolt | | | 160 | | | 11 | Washer | | | 165 | | | 12 | Nut | | | 170 | | | 13 | Bushing | | | 330 | | | 14 | Nut | | | 310 | | | 15 | Washer | | | 305 | | | 16 | Washer | | | 300 | | | 17 | Bolt | | | 295 | | | 18 | Union | 27-11-20 |51 | 195 | | | 19 | Packing | | | 200 | | | 20 | Filter | | | 205 | | | 22 | Hydraulic Tubing Support Bracket | 27-11-20 |02 | 66 | | | 23 | Screw | | | 18 | | | 24 | Washer | | | 20 | 2.......…........…...................................…...........…...….........1
MECHANISM AND OVERRIDE QUADRANT AILERON  MECHANISM AND OVERRIDE QUADRANT AILERON ASEE 
SEE  A 
(LEFT SIDE SHOWN, RIGHT SIDE OPPOSITE) AILERON QUADRANT AND OVERRIDE MECHANISM OR A4 (RIGHT) HOLE A3 (LEFT) RIG PIN WING CABLE WING CABLE A2B (RIGHT) A1B (LEFT) A2A(RIGHT) A1A (LEFT) 
A 
Figure 202 Rig Pin Locations 

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