B.
Standard Tools and Equipment
(1)
Steel straightedge, 4 foot
(2)
Scale, graduated in 0.01 inch
C.
Consumable Materials
(1)
D00633 Grease - BMS 3-33 (preferred)
(2)
D00013 Grease - MIL-G-23827 (optional)
D.
References
(1)
AMM 07-11-01/201, Jacking Airplane
(2)
AMM 09-11-00/201, Towing
(3)
AMM 29-11-00/201, Main Hydraulic Supply System
(4)
AMM 32-00-30/201, Landing Gear Door Locks
(5)
AIPC 32-11-08 Fig. 1
(6)
AIPC 32-11-09 Fig. 1
E.
Access
(1)
Location Zone
735 Wing Landing Gear, LH
745 Wing Landing Gear, RH
F.
Preconditions
S 865-021
(1)
These conditions are necessary for this task:
(a)
The airplane is on jacks (AMM 07-11-01/201).
(b)
The hydraulic power is off (AMM 29-11-00/201).
G.
Adjust the Jury Strut
(1)
Install the ground locks for the landing gear (AMM 09-11-00/201).
S 865-002
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32-11-08
ALL ú ú 01 Page 501 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
SEE A
SENSORS
STOP PLATE
BOLT (3)
A LOWER JURY STRUT
LOWER JURY STRUT UPPER JURY STRUT
A
SHIM
BARREL NUT (3)
APEX BOLT
FWD
JURY STRUT APEX
A
UPPER JURY
STRUT
A = 0.25 |0.02 INCH
JURY STRUT APEX BOLT CENTERLINE
OFF-CENTER DIMENSION
A-A
Wing Gear Jury Strut Adjustment
Figure 501
CENTERLINE UPPER JURY STRUT PIN/ LOWER JURY STRUT PIN
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32-11-08
ALL ú ú 01 Page 502 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 495-003
WARNING: YOU MUST REFER TO 32-00-30/201 FOR THE LOCK INSTALLATION
_______ PROCEDURE. FAST MOVEMENT OF THE DOORS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT IF THE LOCKS ARE NOT CORRECTLY INSTALLED.
(2)
Install the door locks for the wing and body landing gear (AMM 32-00-30/201).
S 225-004
(3)
Examine the off-center dimension A with a straightedge and a scale.
NOTE: If dimension A is not in tolerance, you must adjust the
____ strut. The tolerance is shown in Figure 501, View A-A.
S 845-005
(4)
Release the pressure from hydraulic system No. 4 (AMM 29-11-00/201).
S 495-006
(5)
Install the bungee clamp.
NOTE: Tighten the bungee clamp to make sure the spring tension will
____
decrease when you remove the apex bolt.
S 865-007
(6)
Lift the airplane with jacks to decrease the load on the landing gear and the pressure on the apex bolt (AMM 07-11-01/201).
S 035-008
(7)
Hold the upper jury strut and remove the apex bolt.
S 015-009
(8)
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