W DOC AIRBUS | Discussion

Loss of the Rudder Trim Function on the FAC 2

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MEASUREMENTS
ASM 22-68-03
10CC ACTUATOR RUD TRIM PNR: 6137-5
PINS A/V AND B/X = 340 kΩ +/- 10kΩ
Another system is the same.
From FAC AE/11C to GND 316Ω (relay 7CC)

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4CC Relay
From FAC AB/11A to GND 485Ohms

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