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时间:2011-03-27 12:54来源:蓝天飞行翻译 作者:航空
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 E 56-5B E
 E E
 TASK 71-11-00-220-001


 Detailed Visual Inspection of the Inlet Cowl Forward Backskin through the
 Anti-ice Vent Panel

 1. Reason for the Job

__________________
 Refer to the MPD TASK: 711000-C4


 2. Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific 1 ACCESS PLATFORM 1M (3 FT)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors
 71-13-00-410-040 Closing of the Fan Cowl Doors
 CMM 711119
 RA 32071-108
 SRM 541000
 71-11-00-991-306 Fig. 605

 3. Job Set-up
__________
 Subtask 71-11-00-941-063

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

 (2) On the ENG panel 115VU:


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


 Subtask 71-11-00-010-062
 B. Get Access
 (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR.


 (2) Put the ACCESS PLATFORM 1M (3 FT) in position.

 (3) Remove the screws (5) and (10) that attach the anti-ice vent panel to the inlet cowl outer barrel.

 (4) Remove the anti-ice vent panel (10).


 4. Procedure
_________
 Subtask 71-11-00-220-052
 A. Do a detailed visual inspection of the inlet cowl inner barrel forward backskin, that you can see through the anti-ice vent opening, using a flashlight and an inspection mirror: (Ref. Fig. 605/TASK 71-11-00-991-306)
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1. Corrosion/Disbond  Not permitted opposite (Ref. SRM 541000), disbond on opposite face (Ref. CMM 711119), sheet. (Ref. RA 32071-108). Maximum depth 0.63 mm (0.0248 in.). Maximum dimension 55.9 mm (2.2007 in.). Areas of corrosion/disbond must be separated from other
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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
areas of
 corrosion/disbond by 198
 mm (7.7952 in.).
 Multiple damage sites
 exceeding a total of
 55.9 mm (2.2007 in.) in any 254 mm (10.0000 in.) should be repaired.
 5. Close-up
________
 Subtask 71-11-00-410-060
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Install the screws (5) and (10) that attach the anti-ice vent panel to the inlet cowl outer barrel.

 (3) Close the fan cowl doors (Ref. TASK 71-13-00-410-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR.


 (4) Remove the access platform(s).

 (5) Remove the warning notice(s).


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 Air Intake Cowl
 Figure 605/TASK 71-11-00-991-306- 12 (SHEET 1)
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 Air Intake Cowl
 Figure 605/TASK 71-11-00-991-306- 22 (SHEET 2)
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