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时间:2011-03-27 17:17来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (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.

 (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).

 


 Subtask 78-36-42-010-050
 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 in position.
 Subtask 78-36-42-040-050


 C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).
 Subtask 78-36-42-866-050

 

 D. Retract the slats (Ref. TASK 27-80-00-866-005) and install a warning notice.
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 E E Feb 01/98 E E ECES E Subtask 78-36-42-010-051

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 E. Open the thrust reverser doors to 45 degrees position (Ref. TASK 78-36-00-010-040): FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
 4. Procedure
_________
 (Ref. Fig. 601/TASK 78-36-42-991-305, 602/TASK 78-36-42-991-313, 603/TASK
 78-36-42-991-314)
 Subtask 78-36-42-210-050
 A. Do a visual inspection of the adaptor ring, inner and outer flanges, struts, lower stop fitting, upper outer and forward seal fittings, splice assembly, and hold open rod as follows:
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1. Inspect the adaptor ring and the related hardware for:
 A. Damage  No damage permitted If you find some damage, replace the defective part (Ref. TASK 78-36-42-000-001) and (Ref. TASK 78-36-42-400-001)
 2. Inspect the outer flange for:
 A. Crack  No crack permitted If there is a crack, replace the outer flange (Ref. TASK 78-36-42-000-001) and (Ref. TASK 78-36-42-400-001)
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 Adapter Ring Assembly
 Figure 601/TASK 78-36-42-991-305

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 Adapter Ring Assembly
 Figure 602/TASK 78-36-42-991-313

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R  Adapter Ring Assembly Figure 603/TASK 78-36-42-991-314- 16 (SHEET 1)
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R  Adapter Ring Assembly Figure 603/TASK 78-36-42-991-314- 26 (SHEET 2)
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R  Adapter Ring Assembly Figure 603/TASK 78-36-42-991-314- 36 (SHEET 3)
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R  Adapter Ring Assembly Figure 603/TASK 78-36-42-991-314- 46 (SHEET 4)
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R  Adapter Ring Assembly Figure 603/TASK 78-36-42-991-314- 56 (SHEET 5)
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R  Adapter Ring Assembly Figure 603/TASK 78-36-42-991-314- 66 (SHEET 6)
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 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
B. Fretting

R R R R R
3. Inspect the inner flange for:
 A. Crack
B. Fretting
4. Inspect the struts for:
 A. Crack The fretting must not be felt with a radius scribe (radius equal to 0.0314 in. (0.80 mm))
2 in. (50.8 mm) maximum length, 1 in. (25.4mm) minimum between two cracks, 12 in. (304.8 mm) maximum total length of cracks
The fretting must not be felt with a radius scribe (radius equal to 0.0314 in. (0.8 mm))
 
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