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[70-80 CFM56] 求教高手320CFM56飞机滑耗高的TSM章节号,谢谢

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东航南京航空航天大学

发表于 2011-8-1 12:57:44 | 显示全部楼层 |阅读模式 来自: 中国江苏南京
RT,谢谢!!!!!!
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实名认证TAECO中国民航大学

发表于 2011-8-4 23:15:54 | 显示全部楼层 来自: 中国北京
以前有找到过的!怎么突然给忘记了啊!你那里不能直接摄取吗?就是搜索一下吗?明天我给你看看!
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发表于 2011-8-11 21:42:37 | 显示全部楼层 来自: 中国宁夏银川
在TSM从pattern search进入,然后在79章搜索,标题为:high oil  consumption,再点击进入,程程序如下:
TASK 79-00-00-810-818
Incorrect Oil Quantity Level on Engine 1
1. Possible Causes  

-  ENGINE-1 (1000EM1)  

-  EIU-1 (1KS1)  

-  lubrication unit  

-  XTMR-OIL QTY (4002EN)  

-  wiring  

-  wiring between the circuit breaker (1EN1) and the oil quantity transmitter (4002EN)  

-  wiring from the oil quantity transmitter (4002EN) to the EIU1 (1KS1)  

2. Job Set-up Information  


A. Referenced Information

REFERENCE DESIGNATION
  AMM 71-00-00-000-042  Removal of the Power Plant  
  AMM 71-00-00-400-042  Installation of the Power Plant  
  AMM 71-00-00-710-006  Minimum Idle Check  
  AMM 72-31-00-290-002  Inspection of the High Pressure Compressor Rotor Assembly  
  AMM 73-25-34-000-040  Removal of the Engine Interface Unit (EIU) (1KS1,1KS2)  
  AMM 73-25-34-400-040  Installation of the Engine Interface Unit (EIU) (1KS1,1KS2)  
  AMM 79-00-00-210-006  Visual Inspection of the Aft Sump Oil System  
  AMM 79-21-10-000-004  Removal of the Lubrication Unit  
  AMM 79-21-10-400-004  Installation of the Lubrication Unit  
  AMM 79-31-15-000-041  Removal of the oil Quantity Transmitter (4002EN)  
  AMM 79-31-15-400-041  Installation of the Oil Quantity Transmiter (4002EN)  
  ASM 79-36/01   

3. Fault Confirmation  

A. Test  

(1) Make sure that the oil tank level confirms the oil indication on the lower ECAM display unit.  

4. Fault Isolation  

A. If the oil tank level confirms the oil indication:  

NOTE: Refer to CFM SB 79-021 covering HTS Oil coking issues. Trend instructions to monitor oil pressure trend and implement Inspection and Cleaning procedures if necessary.  

(1) Do a minimum idle check to make sure there are no leaks  AMM TASK 71-00-00-710-006 .  

(2) Do a check of the magnetic chip detector for abnormal debris.  

(3) Do a check of the oil tank, lubrication unit, external oil supply and scavenge lines, for cracks/leaks.  

(a) Do a check of the Aft Sump Oil System for leakage  AMM TASK 79-00-00-210-006 .  

(4) Do a check for heavy oil discharge in the center vent tube.  

(a) If confirmed:  

-  replace the ENGINE-1 (1000EM1)  
     AMM TASK 71-00-00-000-042 and  AMM TASK 71-00-00-400-042 .  

(5) Do a check to see if the flame arrestor is clogged.  

(a) If confirmed:  

-  clean or replace it.  

(6) Remove TGB/AGB drain plug and do a check for abnormal oil quantity. If greater than one quart:  

-  do a check for blockage of the oil scavenge line or replace the lubrication unit  
     AMM TASK 79-21-10-000-004 and  AMM TASK 79-21-10-400-004 .  

(7) Do a borescope inspection of the high pressure compressor stage 1 and 2 to see if they are covered with oil  AMM TASK 72-31-00-290-002 .  

(8) Do an inspection of the fan blades and booster stage 1 at 6 o'clock to see if they are covered with oil.  

(9) Do an inspection of the frame struts and aft side of stage 4 low pressure blades to see if they are covered with oil.  

(a) If there is oil:  

-  replace the ENGINE-1 (1000EM1)  
     AMM TASK 71-00-00-000-042 and  AMM TASK 71-00-00-400-042 .  

B. If the oil tank level does not confirm the oil quantity:  

-  replace the XTMR-OIL QTY (4002EN)  
     AMM TASK 79-31-15-000-041 and  AMM TASK 79-31-15-400-041 .  

(1) If the fault continues:  

-  do a check and repair the wiring  from the oil quantity transmitter (4002EN) to the SDAC-1 (1WV1), SDAC-2 (1WV2 and EIU1 (1KS1).  

C. If there are amber XX at the oil quantity indication location on the lower ECAM DU:  

-  do a check for 28VDC at the oil quantity transmitter (4002EN).  

(1) If there is no 28VDC:  

-  do a check of the wiring between the circuit breaker (1EN1) and the oil quantity transmitter (4002EN)  
     ASM 79-36/01 .  

(2) If there is 28VDC:  

-  do a check and repair the wiring from the oil quantity transmitter (4002EN) to the EIU1 (1KS1)  pins AA/3, 4 to pins AA/8F, 8H  
     ASM 79-36/01 .  

(a) If the fault continues:  

-  replace the EIU-1 (1KS1)  
     AMM TASK 73-25-34-000-040 and  AMM TASK 73-25-34-400-040 .  

D. Do a minimum idle check  AMM TASK 71-00-00-710-006 .
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西藏航空

发表于 2011-12-8 21:58:23 | 显示全部楼层 来自: 中国北京
原来如此!!
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