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C. Referenced Information
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71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 78-30-00-081-041 Make the Thrust Reverser Serviceable after
Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors 72-23-00-991-305 Fig. 405
3. Job Set-up
__________
Subtask 72-23-00-860-060
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) 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 access platform is in position.
Subtask 72-23-00-010-100
B. Get Access
(1) Make sure that the fan cowl doors are open: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
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(2) Make sure that the thrust reverser doors are open: (Ref. TASK 78-36-00-010-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
Subtask 72-23-00-040-069
C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
4. Procedure_________
(Ref. Fig. 405/TASK 72-23-00-991-305)
Subtask 72-23-00-420-063
A. Installation of the fan duct panels.
R R R R R R R (1) Clean the fan frame cavity and the fan duct panels with acetone (Material No. CP1039) or isopropyl alcohol (Material No. CP1041) or stoddard solvent (Material No. CP2011) or ardrox 552 (Material No. CP2559) or turco ind 79 (Material No. CP2560) or mag-chem teksol (Material No. CP2566) or degreasol 99 R (Material No. CP2584) or mag-chem skysol (Material No. CP2656) at the RTV contact area between the fan frame /fan duct panel.
(2) Install the captive screw (150) the washers (180) and the retaining bushings (170) on the fan duct panel (160).
(3) Apply a thin layer of graphite grease (Material No. CP2101) to the threads of the screws (150), and install the new panel (160).
(4) Install the panel on the bleed valve cavity and attach it with captive screws.
(5) TORQUE screws to between 85 and 95 lbf.in (0.96 and 1.07 m.daN).
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________ Subtask 72-23-00-410-080
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the thrust reverser door: (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
Subtask 72-23-00-440-060
B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). Subtask 72-23-00-410-089
C. Close Access
(1) Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
(2) Remove the access platform(s).
(3) Remove the warning notice(s).
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ECES E TASK 72-23-00-000-028 Removal of the Splitter Fairing
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1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
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