153QM(154QM)
AMM 28-26-43-400-001 Installation of the Jet Pump Fuel Control Valve
153QM(154QM)
3. Fault Confirmation
__________________
A. Do the Operational Test of the Main Transfer System (Ref. AMM TASK 28-26-00-710-001).
NOTE : The main (wing) pumps will always supply sufficient primary flow
____
to induce jet pump transfer except:
- under gravity feed
- where one pump is being used to feed both engines at high power
- if the primary fuel flow is blocked
- if the primary fuel flow is leaking away before the jet pump.
4. Fault Isolation
_______________
A. If it is only possible to transfer fuel by gravity and not by the jet pump:
(1) Check/replace the JET PUMP-L, CENTER TANK (157QM), (Ref. AMM TASK 28-26-41-000-001) and (Ref. AMM TASK 28-26-41-400-001).
(2) Do the test given in Para 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-26-00∞∞∞∞∞∞∞∞∞∞Page 222
Aug 01/05R CES
(3) If the fault continues:
- check/replace the FUEL CONTROL VALVE-JET PUMP, L WING TK (153QM), (Ref. AMM TASK 28-26-43-000-001) and (Ref. AMM TASK 28-26-43-400-001).
(4) Do the test given in Para 3.A.
(5) If the fault continues:
- check the primary fuel supply pipe between the left wing fuel pumps and the JET PUMP-LEFT WING TANK (157QM) for leaks or a blockage.
(6) Repair/replace any unserviceable pipes.
(7) Do the test given in Para 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-26-00∞∞∞∞∞∞∞∞∞∞Page 223
Aug 01/05R
CES TASK 28-26-00-810-811
Fuel, Main Transfer System - Right Side Primary Supply Failure or Jet Pump Jet Blocked
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
1. Possible Causes
_______________
- JET PUMP-R, CENTER TANK (158QM)
- FUEL CONTROL VALVE-JET PUMP, R WING TK (154QM)
- primary fuel supply pipe between the right wing fuel pumps and the JET PUMP-RIGHT WING TANK (158QM)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 28-26-00-710-001 Operational Test of the Main Transfer System
AMM 28-26-41-000-001 Removal of the Center Tank Jet Pump 157QM(158QM)
AMM 28-26-41-400-001 Installation of the Center Tank Jet Pump 157QM(158QM)
AMM 28-26-43-000-001 Removal of the Jet Pump Fuel Control Valve
153QM(154QM)
AMM 28-26-43-400-001 Installation of the Jet Pump Fuel Control Valve
153QM(154QM)
3. Fault Confirmation
__________________
A. Do the Operational Test of the Main Transfer System (Ref. AMM TASK 28-26-00-710-001).
NOTE : The main (wing) pumps will always supply sufficient primary flow
____
to induce jet pump transfer except:
- under gravity feed
- where one pump is being used to feed both engines at high power
- if the primary fuel flow is blocked
- if the primary fuel flow is leaking away before the jet pump.
4. Fault Isolation
_______________
A. If it is only possible to transfer fuel by gravity and not by the jet pump:
(1) Check/replace the JET PUMP-R, CENTER TANK (158QM), (Ref. AMM TASK 28-26-41-000-001) and (Ref. AMM TASK 28-26-41-400-001).
(2) Do the test given in Para 3.A.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-26-00∞∞∞∞∞∞∞∞∞∞Page 224
Aug 01/05R CES
(3) If the fault continues:
- check/replace the FUEL CONTROL VALVE-JET PUMP, R WING TK (154QM), (Ref. AMM TASK 28-26-43-000-001) and (Ref. AMM TASK 28-26-43-400-001).
(4) Do the test given in Para 3.A. 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油2(99)
