A. Aircraft Maintenance Configuration
 (1) On the center pedestal, on the ENG panel 115VU, make sure that a warning notice is in position to tell persons not to start the engine.

 (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a warning notice is in position to tell persons not to energize the FADEC 1(2).

 (3) Make sure that the core nozzle is removed (Ref. TASK 78-11-11-000-041).

 4. Procedure
_________
 (Ref. Fig. 401/TASK 78-11-12-991-300)
 Subtask 78-11-12-420-050

 A. Installation of the Centerbody: NOTE : If you install a centerbody on an engine which has a Turbine Rear
____ Frame (TRF) with tangential struts, make sure that there are two rows of drain holes on the centerbody (SB RA32178-4 incorporated, addition of drain holes).
R
R (1) Put the centerbody (5) on the studs in the engine flange.
R (2) Attach centerbody to the engine studs with new nuts (10) and washers (15).
 NOTE : Make sure that you attach the centerbody to the engine with
____ new nuts. Do not use nuts that were used before.
R (3) Adjust the centerbody (5) position to minimize flowpath mismatch.
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R (4) TORQUE nuts (10) to between 220 and 240 lbf.in (2.48 and 2.71 m.daN). NOTE : If any anomaly occurs when removing nuts (loosing or broken
____ stud), (Ref. TASK 72-56-00-210-002) for serviceability or repair.
 5. Close-up
________
 Subtask 78-11-12-410-050
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Install the core nozzle (Ref. TASK 78-11-11-400-041).

 (3) Remove the warning notice(s).

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 CENTERBODY - INSPECTION/CHECK

_____________________________ TASK 78-11-12-210-042 Visual Inspection of the Centerbody
 1. Reason for the Job
__________________
 This inspection criteria is only for those portions of the centerbody that can be observed on-wing. Therefore, the limits and remarks do not apply to the engine attach ring and forward non-accessible areas of the centerbody. Inspection of these areas should be done at the next component removal from the engine.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
78-11-12-000-041 Removal of the Centerbody 78-11-12-400-041 Installation of the Centerbody CMM 781105 78-11-12-991-301 Fig. 601
 3. Job Set-up
__________ Subtask 78-11-12-941-051
 A. Safety Precautions
 (1) On the center pedestal, on the ENG panel 115VU:

 (a) Put a warning notice to tell persons not to start the engine.

 (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.

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 (3) On the overhead maintenance panel 50VU:

 (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.

 (b) Put a warning notice to tell persons not to energize the FADEC 1(2).

 4. Procedure
_________
 Subtask 78-11-12-210-050
 A. Visual Inspection of the Centerbody
 (1) Use proper lighting to illuminate the centerbody. Be especially sure that there are no cracks beyond the limits at the circumferential weld joints. (Ref. Fig. 601/TASK 78-11-12-991-301)
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1. Examine the area 5
 in. (127 mm) from
　
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