Subtask 28-42-15-865-060
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHANNEL/1 AND 2 8QT L26 121VU FUEL/FQI/CHAN/2 2QT M27
4. Procedure
_________
(Ref. Fig. 408/TASK 28-42-15-991-008) Subtask 28-42-15-420-060
A. Preparation for Installation
(1)
Clean the component interfaces and the adjacent areas with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 28-42-15-420-055
B. Installation of the Center (Transfer) Tank Fuel-Quantity Probe
CAUTION : REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU
_______ CONNECT THE ELECTRICAL WIRES. INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
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(1)
Install the bracket (11) on the probe (10).
(2)
Put the probe (10) in the correct position and loosely install the
bolts (9) and (12).
(3)
Measure the clearance between the structure and the top and bottom of the probe (10). Make sure that the clearance is a minimum of 7.0 mm (0.2755 in.)
NOTE : When a probe is installed, a minimum clearance of 7.0 mm
____ (0.2755 in.) is recommended. (A clearance of less than 7.0 mm (0.2755 in.) but more than 5.0 mm (0.1968 in.) is acceptable, if local installation does not allow the recommended clearance)
(4)
To prevent possible static discharge, make sure that the fuel probe is not less than 5.0 mm (0.1968 in.) from:
-the nearest structure
-rib and tank wall
-pipework
-brackets and p-clips
-fasteners and other metal parts.
(5)
TORQUE the bolts (9) to between 0.45 and 0.56 m.daN (39.82 and 49.55 lbf.in) (Ref. TASK 20-28-00-912-002).
(6)
Tighten the bolts (12) (Ref. TASK 20-28-00-912-002).
(7)
Remove the blanking caps from the electrical connectors.
(8)
Identify and connect the electrical connectors of the cable (8) with the screws (3), (4) and (5).
(9)
TORQUE the screws (3), (4) and (5) as follows:
-
the screw (3) to between 0.102 and 0.124 m.daN (9.02 and 10.97 lbf.in)
-
the screw (4) to between 0.203 and 0.226 m.daN (17.96 and 19.99 lbf.in)
-
the screw (5) to between 0.316 and 0.362 m.daN (27.96 and 32.03 lbf.in).
(10)
Put the cable (8) in position under the clamp block (6) and TORQUE the clamp screw (7) to between 0.023 and 0.045 m.daN (2.03 and 3.98 lbf.in).
(11)
Install the cable ties (1), as necessary, to attach the cable (8) to the probe (10).
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Subtask 28-42-15-865-061
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1QT, 2QT, 8QT.
Subtask 28-42-15-740-053
D. Test
(1) Do a status report (BITE) of the FQI system (Ref. TASK 28-42-00-740-001).
5. Close-up
________ Subtask 28-42-15-410-054
A. Close Access WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR DOORS ARE
_______
CLEAR.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the applicable access panel(s) 147AZ and/or 148AZ (Ref. TASK 57-17-11-400-001).
(3)
Remove the access platform(s).
(4) Close the applicable MLG door(s) (Ref. TASK 32-12-00-410-001). Subtask 28-42-15-650-057
B. Fuel Configuration
(1) Refuel, defuel or transfer fuel as necessary (Ref. TASK 12-11-28-650-003), (Ref. TASK 28-25-00-650-001) or (Ref. TASK 28-25-00-869-001).
Subtask 28-42-15-942-053
C. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
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(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items. 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油5(71)
