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时间:2011-03-29 14:38来源:蓝天飞行翻译 作者:航空
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 (a) If you find magnetic particles:
 - follow the related instructions per (Ref. AMM TASK 79-00-00-281-002) and NDT Manual (section CHIP ANALYSIS).

 (2) If nothing is found:


 - do a check for cracks/leaks at oil tank, lubrication, external oil supply and scavenge lines.
 (a) If there is sign of heavy oil discharge in the center vent tube:

 - replace the engine (Ref. AMM TASK 71-00-00-000-042) and (Ref. AMM TASK 71-00-00-400-042).

 (b) If nothing is found:


 - do a check of the flame arrestor for clogging.
 1 If confirmed:
_
 - clean or replace it (Ref. AMM TASK 72-56-00-000-001) and (Ref. AMM TASK 72-56-00-400-001).
 (3) If nothing is found:

 - remove the TBG/AGB drain plug and do a check for abnormal oil quantity.
 (a) If there is more than one quart:
 - do a check for oil scavenge line blockage or replace the lubrication unit (Ref. AMM TASK 79-21-10-000-004) and (Ref. AMM TASK 79-21-10-400-004).

 (4) If nothing is found:

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

 - do an inspection of the fan blades and booster stage 1 at 6 o'clock to see if they are wet with oil,

 - do an inspection of the frame struts and aft side of stage 4 low pressure blades to see if they are wet with oil.

 


 (a) If there is oil:
 - replace the engine (Ref. AMM TASK 71-00-00-000-042) and (Ref. AMM TASK 71-00-00-400-042).
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R  B. If nothing is found: 
R  - Replace the XMTR-OIL PRESS (4003EN) (Ref. AMM TASK 79-33-15-000-041) 
R  and (Ref. AMM TASK 79-33-15-400-041). 
R  (1) If the fault continues: 
R  - do a check of the electrical wiring between the ENG2 OIL PRESS XMTR 
R  (4003EN), the SDAC1 and the SDAC2 (Ref. ASM 79-36/01). 
R  (2) If the fault continues: 
R  - replace the SDAC-1 (1WV1) (Ref. AMM TASK 31-55-34-000-001) and 
R  (Ref. AMM TASK 31-55-34-400-001) 
R  (3) If the fault continues: 
R  - replace the SDAC-2 (1WV2) (Ref. AMM TASK 31-55-34-000-001) and 
R  (Ref. AMM TASK 31-55-34-400-001) 
R
 C. Do a minimum idle check (Ref. AMM TASK 71-00-00-710-006).

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 TASK 79-00-00-810-810
 Oil Quantity Indication on Engine 1 Higher than on Engine 2
 1. Possible Causes
_______________
 - EIU-1 (1KS1)

 - servo fuel heater

 - main oil/fuel heat exchanger

 - XMTR-OIL QTY (4002EN)

 - aircraft wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 71-00-00-710-006 Minimum Idle Check
 AMM 73-11-20-000-002 Removal of the Servo Fuel Heater
 AMM 73-11-20-400-002 Installation of the Servo Fuel Heater
 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 79-21-20-000-002 Removal of the Main Oil/Fuel Heat Exchanger AMM 79-21-20-400-002 Installation of the Main Oil/Fuel Heat Exchanger 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) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU ENGINE/ENG1/OIL/QTY 1EN1 N39
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