
56-101-01501_01502 Revision D
Page | 25
(21) Press F6 to select CAL.
AUTO
MON
INS
CAP
SIM
CAL
F1
F2
F3
F4
F5
F6
(22) Adjust the Full adjustment screw to achieve a correct indicator reading.
(23) With some systems there may be an interaction between the Empty and Full
adjustments; therefore, it will be necessary to repeat the Empty
and
Full adjustments
until no further improvements can be made.
(24) Once the Empty and Full adjustments are finalized, an indicator linearity test may be
accomplished. Refer to the appropriate Maintenance Manuals for capacitance values
between Empty and Full to verify indicator linearity.
(25) This completes the INDICATOR TEST.
(26) Open appropriate Fuel Quantity System circuit breaker(s).
(27) Press PWR to turn test set OFF.
(28) Disconnect the Adapter Cable from the Test Set.
(29) Disconnect the Adapter Cable from the Aircraft and from the Indicator.
(30) Return the Aircraft to its original configuration.
12. BENCH TEST PROBE INSULATION
A.
Connecting Test Set
(1) Position the proper equipment for the following procedures.
(2) Connect the BNC to mini alligator clip leads between the Test Set ACFT jacks and the
associated Probe terminals. Refer to Figure 20.
(3) Connect the ground lead from the Test Set GND receptacle to the probe mounting
flange (refer to Figure 20).
Figure 20
Bench Insulation Test Configuration
B.
Test Procedure
Refer to the appropriate Maintenance Manuals for specific values.
(1) Press PW R to turn test set ON.
(2) Allow initialization to complete.
COMP
HI-Z
ACFT
IND
DFQ40K
+
INPUT
4W
SM
GND
LO-Z
Com Link
-
COMP
LO-Z
HI-Z
GND
LO-Z
COMP
HI-Z
PROBE