R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 28-12-00-200-001 R AMM 28-12-43-000-003 R AMM 28-12-43-400-003 R AMM 28-12-46-000-001 R AMM 28-12-46-200-001 R R AMM 28-12-46-400-001 R AMM 28-25-00-710-003 R AMM 28-25-51-000-001 R AMM 28-25-51-400-001 Inspection of the Tank Venting System Removal of the Float Vent Valve 212QM(213QM) Installation of the Float Vent Valve 212QM(213QM) Removal of the Overpressure-Protector Outlet Inspection of the Wing-Tank Overpressure Protector Outlet Installation of the Overpressure-Protector Outlet Operational Test of the Refuel System Removal of the Refuel Valve 7QU, (8QU) Installation of the Refuel Valve 7QU, (8QU)
R AMM 28-12-00 P.Block 001 TANK VENTING SYSTEM
R 3. Fault Confirmation
__________________
R A. Test
R NOTE : The function of the overpressure protector (located at the
____ R access-panel/door (type 27B) between Ribs 19 and 20) is to protect R the L(R) wing-tank structure from possible damage. R The operation of this overpressure protector will safely release R the (unwanted) pressure to the atmosphere.
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R The defects that follow (and/or) can cause the overpressure R protector to break/operate: R - the refuel supply pressure is above the safe limit R - the L(R) wing-tank vent pipe/duct is blocked R - the float vent valve 212QM(213QM) cannot open (or sufficiently) R to release the (unwanted) pressure R - the related L(R) wing-tank refuel valve 7QU(8QU) does not close R correctly.
R (1) Do the Inspection of the Wing-Tank Overpressure Protector Outlet R (Ref. AMM TASK 28-12-46-200-001).
R (a) If the overpressure protector outlet: R R - and the related items are as specified, no more troubleshooting R work steps are necessary R R - is found to be serviceable but the related items are not as R specified (example, corroded, wire mesh damaged), make them R good before you do the close-up R R - safety disc has operated (is broken or damaged), do Para. 4.A.
R NOTE : The overpressure protector outlet is only included as a
____
R Possible Cause in this TSM procedure.
R 4. Fault Isolation_______________
R A. Procedure
R NOTE : Read all of the steps in this paragraph before you start work.
____
R The order in which the work steps are done is best decided by the
R maintenance staff together with:
R - other malfunction indications
R - the fuel configuration
R - the aircraft location.
R (1) If the (frangible) overpressure protector outlet has operated (is R broken), it is important to do all the steps that follow to find what R caused it to break.
R NOTE : The reasons why a burst disc can break are as follows:
____
R
R - a defective/unserviceable disk (non standard)
R that breaks below the (its) correct operating pressure
R
R - a serviceable disk that operated because the pressure
R difference between the wing-tank and the outside atmospheric
R pressure was more than the correct safe operating pressure
R (Ref. AMM 28-12-00 P.Block 001).
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R (2) Do a check of the applicable fuel tanker or fuel hydrant hose end
R pressure.
R (a) If the fuel pressure is more than 50psi (3.45bar):
R
R - change the fuel pressure if possible or
R
R - get another source of fuel supplied at the correct pressure.
R NOTE : If the fuel tanker or fuel hydrant hose end pressure is____
R more than the maximum safe pressure it can cause:
R - a refuel valve that has been commanded to shut, to stay
R open
R - a overpressure protector (burst disc) to operate
R - damage to the refuel gallery.
R (3) Do a check of the related L(R) wing-tank refuel valve 7QU(8QU) as
R follows:
R (a) Remove the applicable refuel valve 7QU(8QU) (Ref. AMM TASK 28-25-
R 51-000-001).
R (b) Do a visual inspection of the refuel valve 7QU(8QU), valve
R position.
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