(2)
Install the cable mount (Ref. AIPC 49110405010) assembly (10) on the transverse support (3) with the bolts (6), the washers (5) and the nuts (4).
(3)
Connect the starter cables (20) to the transverse support (3) with the nuts (21)and the washers (22).
Suspension and electrical Connections
Figure 801/TASK 49-11-00-991-004
CES
Fuel Feed, Exhaust Muffler, Bleed Air Duct and Oil Cooler Outlet Figure 802/TASK 49-11-00-991-005
R EFF : 106-106, 108-149, 211-299, 301-399, 49-11-00Page 805 Config-3 Aug 01/05
CES
(4)
Connect the generator cables (7) to the cable mount assembly (10) with the nuts (9) and the washers (8).
(5)
Install the blanking caps (19) on the connector sockets 7120VC, 7118VC and 7138VC, which are on the forward bulkhead FR80.
(6)
Install the rear suspension assembly (18) with the washers (12) and the nut (13) to the aft mount assembly (11).
(7)
Install and support the rear suspension assembly (18) with the bolt (14), the washer (16) and the nut (17) to the top bracket (15).
(8)
Before installing the blanking plug to the fuel feed pipe (29), apply LUBRICANTS (Material No. 06-001A) to the internal threads.
(9)
Install the blanking plug (28) to the APU fuel feed pipe (29).
(10)
Attach the APU fuel feed pipe (29) to the bracket on the bulkhead with lockwire-corrosion resistant steel 0.8 mm (0.032 in.) dia..
(11)
Install the blanking plugs on the APU access door 316AR drain interfaces.
(12)
Install the exhaust muffler plug (32) to the APU exhaust outlet (33).
(13)
Install the blanking plug (27) to the exhaust muffler drain (30).
(14)
Install the bleed-air duct plug (35) to the bleed air duct (24) with the tie-rods (23), the bolts (34), the washers (36) and the nuts (37).
(15)
Install the oil-cooler outlet-duct plug (31) on door 315AL with the screws (26) and the washers (25).
Subtask 49-11-00-865-058
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1WG, 2WG, 1WF, 2WF.
5. Close-up
________ Subtask 49-11-00-410-056
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Set the LIGHT control switch 11LJ to the off position.
(3)
Close the APU access doors 315AL, 316AR.
(4)
Close the APU exhaust access fairing 317.
(5)
Remove the access platform(s). Subtask 49-11-00-860-063
B.
Aircraft Maintenance Configuration
(1)
Make an entry in the aircraft technical log book.
(2)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
TASK 49-11-00-000-003
Removal of the APU Substitution Kit (APS 3200)
1. Reason for the Job
__________________
Removal of the APU Substitution Kit
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific protective cover
No specific thread protector
No specific access platform 3.5 m (11 ft. 6 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 49-11-11-400-003 Installation of the Power Plant (APU) (APS 3200) 52-41-00-010-001 Open the APU Doors for Access 52-41-00-410-001 Close the APU Doors after Access 49-11-00-991-004 Fig. 801 49-11-00-991-005 Fig. 802
3. Job Set-up
__________ Subtask 49-11-00-860-061
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
On the panel 25VU make sure that the APU MASTER SW pushbutton switch is off.
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