(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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