RPCP Mechanical Linkage and Override Mechanism Wear Limits
Figure 601 (Sheet 5)
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747-400
MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS PART WORN REPLACE PART WORN REPAIR INSTR REPAIR
DIAMETER PER-MITTED WEAR DIM. ANCE CLEAR-MAX DIA
MIN MAX
9 BEARING ID 0.3747 0.3750 0.3755 0.0030 2
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
10 BEARING ID 0.3747 0.3750 0.3755 0.0030 2
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
11 INNER SHAFT ID 0.8749 0.8755 0.8760 0.0019 X 3
BEARING OD 0.8746 0.8750 0.8741 2
12 OUTPUT CRANK ID 0.3750 0.3760 0.3810 0.0085 X
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
13 BEARING ID 0.3747 0.3750 0.3755 0.0030 2
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
14 BEARING ID 0.3743 0.3750 0.3756 0.0031 4
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
15 LINK ASSY ID 0.3750 0.3760 0.3810 0.0085 X
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
16 BEARING ID 1.3120 1.3125 1.3130 0.0035 2
OUTER SHAFT OD 1.3105 1.3115 1.3095 X 3
RPCP Mechanical Linkage and Override Mechanism Wear Limits
Figure 601 (Sheet 6)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-13-04
ALL ú ú 01 Page 609 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
INDEX NO. PART NAME DIM. DESIGN LIMITS WEAR LIMITS REPLACE WORN PART REPAIR WORN PART REPAIR INSTR
DIAMETER DIM. WEAR MITTED PER- DIA MAX CLEAR-ANCE
MIN MAX
17 BEARING ID 0.3747 0.3750 0.3755 0.0030 2
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
18 CLEVIS ASSY ID 0.3745 0.3755 0.3765 0.0040 X 3
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
19 BEARING ID 0.3747 0.3750 0.3755 0.0030 2
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
20 TUBE ASSY ID 0.3745 0.3755 0.3765 0.0040 X 3
BOLT ASSY OD 0.3735 0.3745 0.3725 X 3
21 BRACKET ID 0.3745 0.3755 0.3765 0.0040 X 3
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