R ELAC1 pushbutton switch is pushed (FAULT and OFF legends off).
R (9) On the overhead panel, on the FLT CTL panel 24VU, make sure that the
R ELAC2 pushbutton switch is pushed (FAULT and OFF legends off).
R (10) On the panel 110VU, make sure that the RUD TRIM indicator shows zero.
R (11) Pressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-863-
R 002)
「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 ∞∞32-51-00∞∞∞∞∞∞∞∞∞∞Page 254
Aug 01/05 CES
**ON A/C ALL
C. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU L/G/LGCIU/SYS1/NORM 1GA C09 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33 121VU ENGINE/ENG2/OIL/PRESS 2EN2 N42 121VU ENGINE/ENG1/OIL/PRESS 2EN1 N40 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
D. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FWS/FWC1/SPLY 3WW F01 121VU ENGINE/ENG2/OIL/PRESS 2EN2 N42 121VU ENGINE/ENG1/OIL/PRESS 2EN1 N40 121VU EIS/FWC2/SPLY 2WW Q07
R
R **ON A/C 001-004, 051-054,
R
E. Procedure
(1) Depressurize the green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
NOTE : Use the results table to help you record the different values
____ thru the procedure that follows. R (Ref. Fig. 201/TASK 32-51-00-991-006-A)
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Results table R Figure 201/TASK 32-51-00-991-006-A
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Aug 01/05 CES (2) Do a check of the steering angle on the MCDU.
(a) On the MCDU, get the STEERING DATA for the BSCU SYS 1 and BSCU
SYS 2: R (Ref. Fig. 202/TASK 32-51-00-991-005)
- On the MCDU, get the SYSTEM REPORT/TEST/L/G page (Ref. AMM TASK 31-32-00-860-009).
- On the SYSTEM REPORT/TEST/L/G page, push the line key adjacent to the BSCU1 indication.
- Make sure that the N/WS handwheels and the rudder pedals are in the neutral position.
- On the BSCU SYS 1 page, push the line key adjacent to the STEERING DATA indication.
- Push the line key adjacent to the REFRESH indication.
- Print the STEERING DATA page of the BSCU SYS 1.
- Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/ TEST/L/G page.
- On the SYSTEM REPORT/TEST/L/G page, push the line key adjacent to BSCU2 indication.
- On the BSCU SYS 2 page, push the line key adjacent to STEERING DATA indication.
- Push the line key adjacent to the REFRESH indication.
- Print the STEERING DATA page of the BSCU SYS 2.
- Put the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST/L/G page.
(b) Do a check of CAPT,FO, rudder pedal, steering command angle and BSCU RVDT input : CAPT ANGLE, FO ANGLE,Pedal angle,STEER ORDER and NWS ANGLE 3GC parameters :
1 Make sure that the CAPT ANGLE value is less than or equal to 0
_ deg. plus or minus 0.4 deg. for the SYS 1 and SYS 2.
2 Make sure that the FO ANGLE value is less than or equal to 0
_ deg. plus or minus 0.4 deg. for the SYS 1 and SYS 2.
3 Make sure that the pedal angle value is less than or equal to
_ 0 deg. Plus or minus 0.1 deg. For the SYS 1 and SYS 2.
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