(2)
The aft shockmount
(3)
The support block for the cone bolt
(4)
The aft mount links
(5)
The bushings and the bolts.
C.
You can only do the inspection of the dimensions when the APU is removed or when the load from the aft mount is removed.
D.
The visual inspection finds loose fasteners, corrosion, and damage.
E.
The aft mount assembly is on the top aft side of the APU. You can get access to the aft mount assembly through the APU access doors.
TASK 49-13-08-206-001
2. APU Aft Mount Assembly Visual Inspection (Fig. 601)________________________________________
A. References
(1)
AIPC 49-13-01, Fig. 1, AIPC 49-13-04, Fig. 1, AIPC 49-13-51 Fig. 1
B.
Access
(1)
Location Zone 317 APU Compartment-Upper Aft Side of Engine, LH 318 APU Compartment-Upper Aft Side of Engine, RH
(2)
Access Panel
317AL APU Access Door
318AR APU Access Door
C.
Procedure
S 866-011
(1)
Make sure the APU control switch on the P5 panel is OFF and attach a DO-NOT-OPERATE tag.
S 016-004
(2)
Open the APU access doors:
(a)
Open the latches on the APU access doors.
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A
747-400 MAINTENANCE MANUAL
BOLT
SEE A
WASHER
NUT
SEE B
A
A
AIRPLANE STRUCTURE
VERTICAL SUPPORT TUBE
A
FWD
BUSHING BUSHINGBOLT BOLT
WASHER (QTY 2)
VERTICAL
WASHER (QTY 2) VERTICAL
NUT
SUPPORT TUBE
NUT SUPPORT TUBE
B B
AFT SHOCKMOUNTAFT SHOCKMOUNT
BEAM BEAM
DD B B
DD CC C C
B1 B
2
1 LORD MANUFACTURING COMPANY - OPTIONAL TO 2
2 BARRY CONTROLS - OPTIONAL TO 1
APU Aft Mount Assembly Inspection
Figure 601 (Sheet 1)
F58210
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
1
1
2 1
A-A B-B
2 1
4
2
3 APU Aft Mount Assembly Inspection Figure 601 (Sheet 2) D-DC-C
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A
747-400
MAINTENANCE MANUAL
REPLACE WHEN WORN.
MAXIMUM AXIAL GAP IS 0.008 INCH (0.20 mm). MAXIMUM RADIAL GAP IS 0.005 INCH (0.13 mm).
APU Aft Mount Assembly Inspection
Figure 601 (Sheet 3)
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