(7)
 Make sure that the surge/bleed duct (8049KM) (15) is correctly aligned and tighten the bolts (19) and the V-clamp (13) and (16).

 (8)
 TORQUE the bolts (19) to 0.56 m. daN (49.55 lbf.in).

 (9)
 TORQUE the V-clamp (16) to 0.68 m.daN (60.17 lbf.in).

 (10)
 TORQUE the V-clamp (13) to 0.56 m.daN (49.55 lbf.in).

 (11)
 Install the bracket (18) which holds the fuel drain pipes and cables to the surge/bleed duct (8049KM) (15).

 (12)
 Remove the blanking plugs and install the load-compressor discharge temperature-sensor (12) (Ref. Task 49-23-16-400-00100).

 (13)
 Put a new gasket (11) in position on the mating face of the sensor module assembly (10) and the surge/bleed duct (8049KM) (15).

 (14)
 Put the sensor module assembly (10) in position on the surge/bleed duct (8049KM) (15) and install the bolts (9) and the bolts (8).

 NOTE : You must install the sensor module assembly carefully to
____ prevent damage to the total pressure sensor pipe.
 (15)
 TORQUE the bolts (9) and the bolts (8) to 0.56 m.daN (49.55 lbf.in).

 (16)
 Remove the blanking plug from the sensor ring.

 (17)
 Install the new O-ring (7) on the air pipe (6).

 (18)
 Attach the air pipe (6) to the sensor ring with the retainer (5), the washer (4) and the bolt (3).

 (19)
 Tighten the bolt (3) and safety with lockwire-corrosion resistant steel 0.8 mm.

 (20)
 Remove the blanking caps from the electrical connections.

 (21)
 Connect the electrical connector (2) to the total pressure sensor.

 (22)
 Connect the electrical connector (1) to the differential pressure sensor.

 Subtask 49-51-42-865-052
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD  Subtask 49-51-42-710-050

 C. Do the operational test of the APU (Ref. TASK 49-00-00-710-004).
 (1) Operate the APU for min. five minutes and examine the joints of the air by-pass duct for leaks (Ref. TASK 49-00-00-790-004).
 NOTE : Leaks are not permitted.
____
 ________

5. Close-up
 Subtask 49-51-42-410-052
 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 SW to the OFF position.

 (3)
 Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).

 (4)
 Remove the access platform(s). Subtask 49-51-42-865-064

 B.
 Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD

 Subtask 49-51-42-860-055
 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).

 TASK 49-51-42-400-002 Installation of the Sensor Assembly (GTCP 36-300) 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 access platform 3.5 m (11 ft. 6 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-41-00-010-001 Open the APU Doors for Access
 3. Job Set-up
__________ Subtask 49-51-42-010-062
 A. Get Access
 (1)
 Put the access platform in position below the APU access doors 315AL and 316AR.

 (2)
 Open the APU access doors 315AL and 316AR (Ref. TASK 52-41-00-010-001).

 (3)
 Make sure that the light SW 11LJ is set to the ON position.

 4.
 Procedure

_________

 5.
 Close-up

________ Subtask 49-51-42-865-065
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD
　
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