EXAMPLE
0.022 INCH (0.56mm)
UPPER LINK FORWARD FUSE PIN
Outboard Strut Wear Limits
Figure 603 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SB 747 ú
54-51-01
54-2155 ú
ú 01 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 615Jun 10/96
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A 747-400 MAINTENANCE MANUAL
10. BUSHING/PIN 10. BUSHING/PIN
LEFT SIDE FUSE PIN RIGHT SIDE FUSE PIN
SPRING BEAM FUSE PIN
Outboard Strut Wear Limits
Figure 603 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SB 747 ú
54-51-01
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A 747-400 MAINTENANCE MANUAL
A
SEE H
A
SIDE BRACE
G
BOLT 14. BEARING/ STRUT FITTING (REF)
SIDE BRACE (REF) (2 LOCATIONS) BOLT 15. BUSHING/BOLT 16. BUSHING/ (2 LOCATIONS) BOLT 13 BUSHING/ SIDE BRACE (REF) 1 FITTING/ BEARING (2 LOCATIONS) BRACE/BUSHING
FITTING (REF) WING (2 LOCATIONS) BOLT 11 BUSHING/ BOLT 12. BUSHING/ 3
2 FITTING/ BUSHING H 1 BRACE/ BUSHING (2 LOCATIONS) 3 FITTING/BUSHING 3 FITTING/ BUSHING FITTING (REF) STRUT
A-A
Outboard Struts Wear Limits Figure 603 (Sheet 5)
E77123
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SB 747 ú
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A
747-400
MAINTENANCE MANUAL
Outboard Strut Wear Limits
Figure 603 (Sheet 6)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SB 747 ú
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E80991
A
747-400
MAINTENANCE MANUAL
REFER TO OHM 54-00-01.
REFER TO SRM 57-20-90.
REFER TO SRM 54-50-90.
REPLACE THE DIAGONAL BRACE (AMM 54-51-02/401).
TO REPLACE THE DIAGOINAL BRACE BUSHING, SEE
. REPLACE THE PIN/BOLT (AMM 54-51-02/401). REPLACE THE BUSHING/BEARING, SEE
. REPLACE THE BUSHING/BEARING, SEE
. REPLACE THE UPPER LINK (AMM 54-51-02/401). TO REPLACE THE UPPER LINK BUSHING/BEARING,
SEE
.
REPLACE THE SPRING BEAM (AMM 54-51-03/401).
TO REPLACE THE SPRING BEAM BUSHING,
SEE
.
REPLACE THE SIDE BRACE (AMM 54-51-02/401). TO REPLACE THE SIDE BRACE BUSHING/BEARING, SEE
Outboard Strut Wear Limits
Figure 603 (Sheet 7)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SB 747 ú
54-51-01
54-2155 ú
ú 01 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 619Feb 10/96
E81001
A
747-400 MAINTENANCE MANUAL
NACELLE STRUT ATTACH PIN/BOLT - REMOVAL/INSTALLATION
____________________________________________________
1. General_______
A. This procedure provides instructions for removal/installation of all strut attach pin/bolts with the engine removed or installed. If a midspar pin is to be removed, both upper link pins/bolts and both diagonal brace pins/bolts must be installed. Only one midspar/spring beam pin is to be removed at a time. Both upper link pins/bolts or both diagonal brace pins/bolts may be removed simultaneously but only one link should be free at any one time, unless nacelle strut is to be removed.
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