61-101-00802.EF1 Revision J
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(8) If pointer position is not acceptable, adjust EMP 1 / E 1 adjustment for the pointer
position.
(9) Rotate the TEST FUNCTION switch to CAP SIM CAL (NORM SYS).
(10) Set the 200 (pF) / 1000 (pF) switch to 1000 (pF).
(11)
Set the CAP SIM (pF) 100’s and the 10’s thumbwheels to the digits required to
adjust the T/S display to a MAIN / TOTAL FULL nominal value for the aircraft listed
in Table 3.
(12) Push and hold the PRESS TO READ CAP (pF) pushbutton while adjusting the CAP
SIM (pF) control knob to obtain the correct T/S reading for the aircraft as per Table
3.
(13) Release the pushbutton.
(14) Rotate the TEST FUNCTION switch to IND AMP.
(15) Verify the indicator reads 1300 lbs.
(16) If the indicator does not read 1300 lbs, adjust F / FULL to obtain the value.
(17) Rotate the TEST FUNCTION switch to CAP SIM CAL (NORM SYS).
(18) Set the 200 (pF) / 1000 (pF) switch to 200 (pF).
(19) Set the MAIN / TOT
– AUX / NAC. switch to AUX / NAC.
(20)
Set the CAP SIM (pF) 100’s and the 10’s to the digits required to adjust the T/S
display to an AUX / NAC. EMPTY nominal value referenced in Table 2 for the
aircraft under test.
(21) Press and hold PRESS TO READ CAP (pF) pushbutton while adjusting CAP SIM
(pF) control knob to obtain the T/S reading for the aircraft as per Table 2.
(22) Release the pushbutton.
(23) Rotate the TEST FUNCTION switch to IND AMP.
(24) Verify the indicator shows zero lbs for all aircraft except C90, C90A / B / GT / GTi /
GTx or C99.
(25) Verify the indicator shows slightly below zero (approximately one needle width) for
C90, C90A / B / GT / GTi / GTx and C99 models.
(26) If pointer position is not acceptable, use the EMP 2 / E 2 adjustment to obtain a
correct reading.
(27) Repeat steps D.2 through D.26 until an accurate calibration is obtained.
(28) Set the T/S and Aircraft battery switch both to OFF.
E. Disconnecting/Reconfiguring
(1) Open circuit breakers, turn the battery switch OFF.
CAUTION:
WHEN LOWERING OR RAISING PILOT FUEL PANEL, ENSURE
AIRCRAFT BATTERY SWITCH IS OFF AND BATTERY IS
DISCONNECTED.
(2) Disconnect the T/S from the aircraft wiring plug.
(3) Disconnect the T/S from the Indicator.
(4) Connect the aircraft wiring plug to the Indicator.
(5) Return the aircraft to its original configuration.
