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时间:2011-03-27 16:55来源:蓝天飞行翻译 作者:航空
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 4. Procedure
_________
 (Ref. Fig. 611/TASK 72-21-00-991-335)
 Subtask 72-21-00-210-061
 A. Do an inspection/check of the items which follow:
 (1) Fan blade airfoils, midspan shrouds and dovetails (Ref. TASK 72-21-00-210-006).

 (2) Fan blade spacers and fan dovetails slots (Ref. TASK 72-21-00-210-007).


 5. Close-up
________
 Subtask 72-21-00-640-052
 A. Apply MoS2 dry film lubricant (Material No. CP5062) or molykote G rapid (Material No. CP2104):
 - the fan disk dovetail slots,

 - the blade spacers,

 - the blade dovetails,

 - the blade midspan shrouds, before the re-installion of the blades. Lubricant should be applied liberally to all dovetail and slot pressure faces. Brush application is preferred. Allow the lubricant to dry to a dull opaque finish before installation of blades in disk slots.


 Subtask 72-21-00-420-085
 B. Install fan blades (Ref. TASK 72-21-00-400-007).
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 Fan Blade, Blade Spacer and Disk Areas to Be Inspected after Cleaning for

 Removal of Lubricant from Pressure Faces
 Figure 611/TASK 72-21-00-991-335
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 Subtask 72-21-00-942-080
 C. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Remove the warning notice(s).


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 FAN AND BOOSTER ASSEMBLY - REPAIRS
__________________________________ TASK 72-21-00-300-001 Replacement of the Crimped Self-Locking Nuts on the Spinner Rear Cone
 1. Reason for the Job

__________________
 Self Explanatory


 2. Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific access platform 1 m (3 ft. 3 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
72-21-00-000-005 Removal of the Spinner Front Cone 72-21-00-000-006 Removal of the Spinner Rear Cone 72-21-00-400-005 Installation of the Spinner Front Cone 72-21-00-400-006 Installation of the Spinner Rear Cone SPM 704251350018
 3. Job Set-up
__________ Subtask 72-21-00-941-071
 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) Put an access platform in position.
 4. Procedure
_________ Subtask 72-21-00-020-067
 A. Removal of the defective cimpred Nut(s).
 (1) Remove the spinner front cone (Ref. TASK 72-21-00-000-005)

 (2) If necessary, remove the spinner rear cone (Ref. TASK 72-21-00-000-006)

 (3) Remove the defective crimped self-locking nut(s) from the spinner rear cone. (Ref. SPM 704251350018)


 Subtask 72-21-00-420-070
 B. Crimping of the New Self-Locking Nuts. CAUTION : BE CAREFUL NOT TO CAUSE DAMAGE TO THE SURFACE PROTECTION AROUND
_______
 THE NUTS DURING NUT INSTALLATION.

 (1) Crimp the new self-locking nut(s). (Ref. SPM 704251350018) NOTE : No radial or end play is permitted in the installation of the

____
 crimped self-locking nuts type B.


 (2) Install the spinner front cone. (Ref. TASK 72-21-00-400-005)
 
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