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时间:2011-03-28 09:19来源:蓝天飞行翻译 作者:航空
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 NOTE : The impedance must be more than 70 Ohms and not open circuit.
____
 (a) If the impedance is not correct (< 70 Ohms or open circuit):
 - do a check of the wiring of the RTL ACT VALID signal from the FAC1 to the RTLU and associated GND signal at the RTLU (Ref. ASM 22-68/02).
 1 If the wiring is correct:
_
 - install the above removed FAC-1 (Ref. AMM TASK 22-66-34-400-002)

 - replace the electronic module of the rudder travel-limitation unit (4CC) (Ref. AMM TASK 27-23-51-000-002) and (Ref. AMM TASK 27-23-51-400-002).


 a If the fault continues:
_
 - replace the LIMITATION UNIT-RUDDER TRAVEL (4CC) (Ref. AMM TASK 27-23-51-000-001) and (Ref. AMM TASK 27-23-51-400-001).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞22-61-00∞∞∞∞∞∞∞∞∞∞Page 206
 Nov 01/04R CES


 (b) If the impedance is correct (no short circuit and no open circuit):
 - do a check of the impedance of the RTL ACT PWR ON signal between the pin AE/11A and the pin AC/3 of the FAC-1 rack connector, (Ref. ASM 22-68/02) and (Ref. ASM 22-67/01).
 NOTE : The impedance must be more than 70 Ohms and not open
____
 circuit.

 1 If the impedance is not correct (< 70 Ohms or open circuit):
_
 - remove the relay 13CC1 (open the circuit breaker 5CC1 before and close it after)

 - do a check of the wiring of the RTL ACT PWR ON signal from the FAC1 to the relay 13CC1 (Ref. ASM 22-68/02).


 a If the wiring is correct:
_
 - replace the RELAY-RTL SYS1 (13CC1)

 - install the above removed FAC-1 (Ref. AMM TASK 22-66-34-400-002).


 2 If the impedance is correct (RTL ACT VALID and RTL ACT PWR ON
_
 signals):

 - do a check of the wiring of the 28VDC and GND at the RTLU (PWR SPLY) (Ref. ASM 22-68/02).
 a If incorrect, repair the wiring.
_
 b If correct, replace the RELAY-RTL SYS1 (13CC1).
_ If the fault continues:
 - replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-400-002).
 (2) If the fault continues:
 - do a check and repair the remaining wiring from the FAC 1 (1CC1) to the rudder travel-limitation unit (4CC) (Ref. ASM 22-68/02).
 B. If the test does not give the maintenance message AFS: FAC 1/RTL ACTR 4CC:
R (1) Replace the SENSOR-TAT, 1 (11FP1) (Ref. AMM TASK 34-11-18-000-001) R and (Ref. AMM TASK 34-11-18-400-001).
R (2) If the fault continues:
 - do the operational test of the rudder travel limiting function (Ref. AMM TASK 22-61-00-710-001).


 C. If the rudder does not move or stops before the rudder travel limit:
 - replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
 (1) If the fault continues:

 - replace the electronic module of the rudder travel limitation unit (Ref. AMM TASK 27-23-51-000-002) and (Ref. AMM TASK 27-23-51-400-002).

 (2) If the fault continues:

 - replace the rudder travel limitation unit (4CC) (Ref. AMM TASK 27-23-51-000-001) and (Ref. AMM TASK 27-23-51-400-001).

 (3) If the fault continues:


 - do a check and repair the wiring of the RTL V1 and RTL V2 discretes from the FAC 1 (1CC1) to the rudder travel-limitation unit (4CC), (Ref. ASM 22-68/02).
 D. Do the test given in Para. 3.B.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞22-61-00∞∞∞∞∞∞∞∞∞∞Page 208
 Nov 01/04R

 CES  Loss of the Rudder Travel Limiting Function on the FAC 2


 1. Possible Causes
_______________
 - LIMITATION UNIT-RUDDER TRAVEL (4CC)

 - RELAY-RTL SYS2 (13CC2)

 - FAC-2 (1CC2)

 - wiring for 28VDC signal (pin A2) and GND signal (pin X2) at the relay (13CC2)

 - wiring of the RTL ACT VALID signal from the FAC2 to the RTLU and associated GND signal at the RTLU

 - electronic module

 - wiring of the RTL ACT PWR ON signal from the FAC2 to the relay 13CC2

 - wiring of the 28VDC signal from the relay 13CC2 to the RTLU and associated GND at the RTLU

 - wiring from the FAC 2 (1CC2) to the rudder travel-limitation unit (4CC)

 - wiring of the RTL V1 and RTL V2 discretes from the FAC 2 (1CC2) to the rudder travel-limitation unit (4CC)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
 
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