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时间:2011-03-28 18:47来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R - On the MCDU, push the next page function key twice to get
R the BSCU CHAN 1/SYSTEM DATA page 3/3.
R - On the SYSTEM DATA page 3/3 of the BSCU CHAN 1, push the
R line key adjacent to the REFRESH indication.
R - Record the value of the pedal angle value (value A1).
R - Close the circuit breakers 15CE2 and 16CE2 (the ELAC2 is
R connected).
R - Open the circuit breakers 15CE1 and 16CE1 (the ELAC1 is
R isolated).
R - On the SYSTEM DATA page of the BSCU CHAN 1, push the line
R key adjacent to the REFRESH indication.
R - Record the value of the pedal angle value (value B1).
R - On the SYSTEM DATA page of the BSCU CHAN 1, push the line
R key adjacent to the RETURN indication to get the SYSTEM
R REPORT/TEST/L/G page.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 401-499, ∞∞32-51-00∞∞∞∞∞∞∞∞∞∞Page 289
 Aug 01/05 CES


R - On the SYSTEM REPORT/TEST/L/G page, push the line key
R adjacent to the BSCU2 indication.
R - On the BSCU CHAN 2 page, push the line key adjacent to the
R SPECIFIC DATA indication.
R - Close the circuit breakers 15CE1 and 16CE1 (the ELAC1 is
R connected).
R - Open the circuit breakers 15CE2 and 16CE2 (the ELAC2 is
R isolated).
R - On the BSCU CHAN 2/SPECIFIC DATA page, push the line key
R adjacent to SYSTEM DATA indication.
R - On the MCDU, push the next page function key twice to get
R the BSCU CHAN 2/SYSTEM DATA page 3/3.
R - On the SYSTEM DATA page 3/3 of the BSCU CHAN 2, push the
R line key adjacent to the REFRESH indication.
R - Record the value of the pedal angle (value A2).
R - Close the circuit breakers 15CE2 and 16CE2 (the ELAC2 is
R connected).
R - Open the circuit breakers 15CE1 and 16CE1 (the ELAC1 is
R isolated).
R - On the SYSTEM DATA page of the BSCU CHAN 2, push the line
R key adjacent to the REFRESH indication.
R - Record the value of the pedal angle (value B2).
R - On the MCDU, push the line key adjacent to the RETURN
R indication to get the SYSTEM REPORT/TEST/L/G page.
R
R - If the values A1 and/or A2 only are more than 0 deg. plus or
R minus 0.1 deg. :

R . Replace the ELAC-1 (2CE1) (Ref. AMM TASK 27-93-34-000-001)
R and (Ref. AMM TASK 27-93-34-400-001).
R - If the values B1 and/or B2 only are more than 0 deg. plus or
R minus 0.1 deg. :


R . Replace the ELAC-2 (2CE2) (Ref. AMM TASK 27-93-34-000-001)
R and (Ref. AMM TASK 27-93-34-400-001)
R - If the values (A1 and B1) and/or (A2 and B2) are more than 0
R deg. plus or minus 0.1 deg.:


R . Do a check of the adjustment of the pedal position
R transducer unit (25CE1, 25CE2) (Ref. AMM TASK 27-21-00-820-R 003).
R - Close the circuit breakers 15CE1, 16CE1, 15CE2 and 16CE2.
R - Do steps (b) and (c) 3_ again and make sure that the pedal
R angle value is correct for CHAN 1 and CHAN 2, if not do the
R step 6.

 

R 4_ If the ANGCSG value is not correct for the BSCU CHAN 1 and/orR CHAN 2, do the step 6.
R 5_ If the difference between the RVDTCOM CHAN 1 (value A) andR RVDTCOM CHAN 2 (value B) is not correct, do the step 6.
R 6_ Replace the BSCU (10GG) (Ref. AMM TASK 32-42-34-000-001) andR (Ref. AMM TASK 32-42-34-400-001).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 401-499, ∞∞32-51-00∞∞∞∞∞∞∞∞∞∞Page 290
 Aug 01/05 CESR 7_ Do the steps (a) thru (c) again and make sure that all theR parameters are correct for the CHAN 1 and the CHAN 2, then do R the step 8.


R 8_ Return the aircraft to service and make a record in theR aircraft log book to monitor the NWS during the next taxi R operation and to assess the aircraft lateral deviation, if R any, using the rudder trim input. R - On the overhead panel, on the FLT CTL panel 23VU, make sure R that the ELAC1 pushbutton switch is pushed (FAULT and OFF R legends off). R - On the overhead panel, on the FLT CTL panel 24VU, make sure R that the ELAC2 pushbutton switch is pushed (FAULT and OFF R legends off). R - Refer to the Close-Up part (5.A) and do the relevant steps.
R (3) If the steering angle on the MCDU is correct, do a check of the R servovalve.
R (a) If the Fault Confirmation test was to be done only with the R taxiway procedure, put the aircraft in the necessary R configuration to let the nosewheels move freely to the left or R the right:
R 1_ If the check is to be done with the nosewheels on ground, doR these steps:
R NOTE : You will need two 1.2 m (3.93 ft.) square steel plates.
 
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