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时间:2011-03-28 13:42来源:蓝天飞行翻译 作者:航空
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____ indication, release the FLT CTL/ELAC 1 pushbutton switch on the overhead panel 23VU (on this pushbutton switch the OFF legend comes on) and wait for 30 s.
 C. Put the aircraft back to its initial configuration.
 (1) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-864-003), (Ref. AMM TASK 29-23-00-864-001), (Ref. AMM TASK 29-24-00-864-001).

 (2) On the overhead panel 23VU:


 - push the FLT CTL/ELAC 1 pushbutton switch (on this pushbutton switch, the OFF legend goes off).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message: L B AIL MODE VLV 33CE3
 (1) Remove the ELAC1 (Ref. AMM TASK 27-93-34-000-001).

 (2) At the ELAC1 receptacle, do a check of the resistance between pin AA/7G and pin AD/10C (Ref. ASM 27-93/02).


 NOTE : The resistance must be between 40 and 100 Ohms.
____

 (a) If the resistance is less than 40 Ohms:
 - at the outboard aileron servocontrol (33CE3), do a check of the resistance of the solenoid valve between pin A/H and pin A/T (Ref. ASM 27-93/02).
 NOTE : The resistance must be between 40 and 100 Ohms.
____

 1 If the resistance values are out of the specified limits:
_ a Replace the solenoid valve of the servo control (33CE3),

_ (Ref. AMM TASK 27-14-51-000-004) and (Ref. AMM TASK 27-14-51-400-004).
 b_  Do again a check of the resistance of the solenoid valve
R  between pin A/H and pin A/T of the outboard aileron 
R  servocontrol (33CE3) (40 to 100 Ohms).
 - If the resistance values are out of the specified limits:
 . Replace the SERVO CTL-L AILERON, OUTBD B (33CE3) (Ref.
 AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-
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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 217
 Aug 01/00 CES

 

 . Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-
001) (Ref. AMM TASK 27-93-34-400-001).
 - If the resistance values are in the specified limits: 
R  . Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-
R  001) (Ref. AMM TASK 27-93-34-400-001).

 2 If the resistance values are in the specified limits:
_ a Repair the wiring of the SOL VLV signal from the servo

_ control (33CE3) to the ELAC1 (2CE1), (Ref. ASM 27-93/02).
R b_ Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001)R and (Ref. AMM TASK 27-93-34-400-001).
 (b) If the resistance is more than 100 Ohms:
 - at the outboard aileron servocontrol (33CE3), do a check of the resistance of the solenoid valve between pin A/H and pin A/T (Ref. ASM 27-93/02).
 NOTE : The resistance must be between 40 and 100 Ohms.
____

 1 If the resistance values are out of the specified limits:
_

R a_ Replace the solenoid valve of the servo control (33CE3)R (Ref. AMM TASK 27-14-51-000-004) and (Ref. AMM TASK 27-14-51-400-004).
 b Do again a check of the resistance of the solenoid valve
_ R between pin A/H and pin A/T of the outboard aileron R servocontrol (33CE3) (40 to 100 Ohms).
 - If the resistance values are out of the specified limits: . Replace the SERVO CTL-L AILERON, OUTBD B (33CE3) (Ref. AMM TASK 27-14-51-000-001) and (Ref. AMM TASK 27-14-51-400-001). . Install the ELAC1 (Ref. AMM TASK 27-93-34-400-001).

 - If the resistance values are in the specified limits: Install the ELAC1 (Ref. AMM TASK 27-93-34-400-001).


 2 If the resistance values are in the specified limits:
_

R a_ Repair the wiring of the SOL VLV signal from the servoR control (33CE3) to the ELAC1 (2CE1) (Ref. ASM 27-93/02).
 b Install the ELAC1 (Ref. AMM TASK 27-93-34-400-001).
_

 (c) If the resistance values are in the specified limits: R R - see para. (3)
 「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 218
 Aug 01/00 CESR (3) At the ELAC1 receptacle, do a check of the insulation between pin R AA/7G (pin AD/10C) and the ground.

 

R  NOTE : The resistance must be more than 100 Megohms.
____

R (a) If the resistance is more than 100 Megohms:
R - replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001) and
R (Ref. AMM TASK 27-93-34-400-001).

R  1_  If the fault continues:
R  - replace the solenoid valve (Ref. AMM TASK 27-14-51-000-004) 
R  and (Ref. AMM TASK 27-14-51-400-004). 
 
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