R  EFF : 001-049, 101-105, 107-107, 151-199, 49-23-51Page 407 201-210, Config-2 Aug 01/05
 CES

 (11)
 Position the fuel pipes (3), (16) and (18) into the IGV actuator.

 (12)
 Turn plate (2) into position on the fuel pipes (3) and (18) and connect the captive bolts (1).

 (13)
 TORQUE the bolts (1) to 0.57 m.daN (50.44 lbf.in).

 (14)
 Rotate cover (11) into position and tighten the bolts (9).

 (15)
 TORQUE the bolts (2) to 0.57 m.daN (50.44 lbf.in)

 (16)
 Remove the blanking cap from the electrical connection and connect the electrical connection (6).

 Subtask 49-23-51-865-065
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.
 Subtask 49-23-51-710-054
 C. Do the operational test of the APU (Ref. TASK 49-00-00-710-010). Subtask 49-23-51-360-051
 D. Inspect the APU.
 (1) Examine the IGV actuator and the fuel pipes for the fuel leaks. NOTE : No leaks are permitted.
____
 ________

5. Close-up
 Subtask 49-23-51-410-055
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).

 (3)
 Remove the access platform(s).

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 CES  Subtask 49-23-51-865-066

 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
 Subtask 49-23-51-860-059
 C. Aircraft Maintenance Configuration
 (1)
 Pressurize the reservoirs of the hydraulic systems.
 (Ref. TASK 29-14-00-614-002).

 (2)
 De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

 (3)
 Remove the warning notice(s).

R  EFF : 001-049, 101-105, 107-107, 151-199, 49-23-51Page 409 201-210, Config-2 Aug 01/05
 CES

 ACTUATOR - INLET GUIDE VANE - REMOVAL/INSTALLATION
__________________________________________________ TASK 49-23-51-000-003 Removal of the Inlet Guide Vane Actuator (8014KM) (APS 3200) WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______ WHEN YOU DO THE MAINTENANCE TASK(S).
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific container 2.0 l (0.5283 USgal)
 No specific access platform 2.5 m (8 ft. 2 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-00-00-910-001 Fuel Safety Procedures 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action 52-41-00-010-001 Open the APU Doors for Access 49-23-51-991-004 Fig. 401
 3. Job Set-up
__________ Subtask 49-23-51-941-055
 A. Safety Precautions
 (1) Obey the Fuel Safety Precautions (Ref. TASK 28-00-00-910-001).

 Subtask 49-23-51-860-050
 B. Aircraft Maintenance Configuration
 (1)
 On the panel 25VU, make sure that the APU MASTER SW pushbutton switch is off.

 (2)
 Put a warning notice in the cockpit to tell persons not to start the APU.

 (3)
 Make sure that ground fire extinguishing equipment is available.

 (4)
 Make sure that hydraulic systems are depressurized
 (Ref. TASK 29-00-00-864-001).

 Subtask 49-23-51-865-058
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
　
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