(2)
Access Panels
6540 Refueling Station Access Door
B. Procedure
S 865-002-002
(1) Make sure these circuit breakers are closed:
(a) P6 Main Power Distribution Panel
1) QTY
2) EP GND FUELING
S 975-003-002
(2)
Write the values shown on the fuel quantity indicators.
S 715-004-002
(3)
Push and hold the QTY TEST switch adjacent to the fuel quantity indicators.
S 715-005-002
(4)
Make sure the fuel quantity indicators go to a value of zero and show ERR 4 on the display.
NOTE: ERR 4 will not show on MOD 4 or subsequent indicators
____ unless you hold the QTY TEST switch for more than 30 seconds. The indicator will show ERR 2 on the display if the indicator has error code 3 in its memory.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SIMMONDS DIGITAL FUEL ú
28-41-02 QUANTITY INDICATORS ú CONFIG 2
ú 01 Page 502 (SIMMONDS SYSTEM TESTER) ú Jul 15/93
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A
737-300/400/500MAINTENANCE MANUAL
S 715-006-002
(5) Release the test switch and make sure the indicators do these steps in this sequence:
(a)
The fuel quantity indicators show all segments of the display for two seconds.
(b)
The fuel quantity indicators show no segments for two seconds.
(c)
The fuel quantity indicators show each error code in the indicator memory for two seconds each.
(d)
The fuel quantity indicators show the tank capacity value.
(e)
The fuel quantity indicators show the value that you wrote before this step with a tolerance of |10 pounds (|10 kilograms).
S 015-012-002
(6)
Open the access door, 6540, for the refuel control panel (P15).
S 975-007-002
(7)
Write the values shown on the refuel quantity indicators.
S 715-008-002
(8)
Set and hold the test switch to TEST GAGES.
S 715-009-002
(9)
Make sure the refuel quantity indicators do these steps in this sequence:
NOTE: The indicators will do these steps again until you
____
release the test switch.
(a)
The refuel quantity indicators show all segments of the display for two seconds.
(b)
The refuel quantity indicators show no segments for two seconds.
(c)
The refuel quantity indicators show the tank capacity value for two seconds.
S 715-010-002
(10)
Release the test switch, and make sure the indicators show the same values that you wrote before this step with a tolerance of |10 pounds (|10 kilograms).
(11)
Close the access door, 6540, for the refuel control panel (P15).
S 415-011-002
TASK 28-41-02-825-013-002
3. System Trim - Fuel Quantity Indicating System
_____________________________________________
A. Special Tools and Equipment
(1) System test unit (one of these units):
(a) Model PSD40-1, J. C. Air, 400 Industrial Parkway, Industrial Airport, KS 66031
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH SIMMONDS DIGITAL FUEL ú
28-41-02 QUANTITY INDICATORS ú CONFIG 2
ú 01 Page 503 (SIMMONDS SYSTEM TESTER) ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(b) Models PSD60-1, -2, -2R: J. C. Air
(2) Test harnesses (use one of these):
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