61-101-00802.EF1 Revision J Page | 13
(30) Repeat steps D.2 through D.29 until an accurate gage adjustment is obtained.
(31) Set the MAIN / TOT – AUX / NAC switch to MAIN / TOT.
(32) Rotate the TEST FUNCTION switch to CAP SIM CAL (NORM SYS).
(33) Set the 200 (pF) / 1000 (pF) switch to 1000 (pF).
(34) Set the CAP SIM (pF) 100’s thumbwheel to 2. Set the 10’s thumbwheel to 1.
(35) Press and hold the PRESS TO READ CAP (pF) pushbutton while adjusting the CAP
SIM (pF) control knob to obtain a T/S reading of 210 pF.
(36) Rotate the TEST FUNCTION switch to IND AMP.
(37) Verify the indicator reads 300 ± 35 lbs.
(38) Rotate the TEST FUNCTION switch to CAP SIM CAL (NORM SYS).
(39) Set the CAP SIM (pF) 100’s thumbwheel to “2”. Set the 10’s thumbwheel to “3.”
(40) Press and hold the PRESS TO READ CAP (pF) pushbutton while adjusting the CAP
SIM (pF) control knob to obtain a test display of 231 pF.
(41) Rotate the TEST FUNCTION switch to IND AMP.
(42) Verify the indicator reads 600 ± 35 lbs.
(43) Rotate the TEST FUNCTION switch to CAP SIM CAL (NORM SYS).
(44) Set the CAP SIM (pF) 100’s thumbwheels to “2”. Set the 10’s thumbwheel to “5”.
(45) Press and hold the PRESS TO READ CAP (pF) pushbutton while adjusting CAP SIM
(pF) control knob to obtain a T/S display of 252 pF.
(46) Rotate the TEST FUNCTION switch to IND AMP.
(47) Verify the indicator reads 900 ± 35 lbs.
(48) Set the T/S ON / OFF switch to OFF.
E. Disconnecting/Reconfiguring
(1) Open the circuit breakers, turn the battery switch OFF.
CAUTION: WHEN RAISING OR LOWERING THE PILOT FUEL PANEL, ENSURE
AIRCRAFT BATTERY IS DISCONNECTED.
(2) Disconnect T/S from the aircraft wiring.
(3) Disconnect T/S from the Indicator.
(4) Reconnect aircraft wiring plug to Indicator.
(5) Return the aircraft to its original configuration.
To Next Page
Loading...
