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时间:2011-03-27 17:01来源:蓝天飞行翻译 作者:航空
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 1 Inspect D-bolt threads for evidence of damages as thread
_ damaged, nicks or dents on threads, etc... In case of damages, replace the D-bolt (300) as follows:
 - Remove and discard the retaining ring (310).

 - Remove and discard the D-bolt.

 - Install a new D-bolt on the main fuel pump housing.

 - Install a new retaining ring on the D-bolt.


 (i) Make an inspection of the fuel filter cover and the filter element for contamination. According to the filter element contaminants, you must do an inspection of the filter element (Ref. TASK 73-11-10-210-003).
R R PRE SB CFM 73-0107 R
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R  1_  Remove and discard the fuel filter element (20) with the
R  O-rings (10) and (30). 
R  NOTE : Make sure that o-rings (10) and (30) are in the fuel____ 
R  filter element. 

R  END OF PRE SB CFM 73-0107 

R  POST SB CFM 73-0107 

R  2_  Remove and discard the fuel filter element (20).
R  NOTE : Make sure that o-rings are in the fuel filter element.____ 

R  END OF SB CFM 73-0107 

R  3_ If the main fuel pump must be removed, re-install the filter
 element for investigation purpose.
 END OF SB CFM 73-062

 E E Nov 01/02 E E ECES E TASK 73-11-10-400-004

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 Installation of the Fuel Filter Element
 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 Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2101 * graphite grease (Ref. 70-30-00) Material No. CP5070 * vaseline (Ref. 70-30-00) Material No. CP5074 * dearomatized petroleum (Ref. 70-30-00)
 Material No. CP8001  * corrosion resistant steel lockwire 0.8 mm DIA (Ref. 70-30-00)
 Material No. CP8002  * corrosion resistant steel lockwire 0.8 mm DIA (Ref. 70-30-00)
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 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R  10  O-ring 
R  10  O-ring 
R  10  O-ring 
R  10  O-ring 
R  30  O-ring 
R  30  O-ring 
R  30  O-ring 
R  30  O-ring 
80  O-ring 
R
 80  O-ring 
R
 90  O-ring 
R
 90  O-ring 
D. Referenced Information

73-11-10 01B-350 73-11-10 01B-350A 73-11-10 01C-350 73-11-10 01C-350A 73-11-10 01B-350 73-11-10 01B-350A 73-11-10 01C-350 73-11-10 01C-350A73-11-10 01B-290
73-11-10 01C-290
73-11-10 01B-310
73-11-10 01C-310
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  71-00-00-710-006 71-13-00-010-040 71-13-00-410-040 73-11-10-300-002
73-11-10-991-305
73-11-10-991-309

3. Job Set-up
__________
 Subtask 73-11-10-860-052Minimum Idle CheckOpening of the Fan Cowl DoorsClosing of the Fan Cowl DoorsRemoval of Defective Inserts on the Main Fuel Filter HousingFig. 301Fig. 302
 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.
 
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