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时间:2011-03-27 08:55来源:蓝天飞行翻译 作者:admin
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 5. Close-up
________
 Subtask 55-33-00-860-052
 A. Put the aircraft back to the serviceable condition.
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 If necessary, close/install the trailing edge access-panels (Ref. TASK 55-33-13-410-002).

 (3)
 Remove the access platform(s).

 (4)
 Remove the warning notice(s).

 


 Subtask 55-33-00-865-051

 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2, 14CC1, 14CC2, 15CC, 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3, 21CE1, 21CE2, 21CE3, 22CE


 TRAILING EDGE - VERTICAL STABILIZER - MAINTENANCE PRACTICES
___________________________________________________________
 TASK 55-33-13-010-002
 Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific warning notice
 No specific adjustable access platform 6 m (19 ft. 8 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
29-00-00-864-001  Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action R 55-33-13-991-002 Fig. 201


 3. Job Set-up__________
 Subtask 55-33-13-865-056
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 55-33-13-864-052
 B. Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-00-00-864-001).
 Subtask 55-33-13-941-052
 C. Get Access
 (1)
 Put the warning notice in the cockpit to tell persons not to operate the flight controls.

 (2)
 Put the rudder pedals in a neutral position.

 (3)
 Put the adjustable access platform in position.


 1EFF : ALL 1 55-33-13Page 202 1 1 Aug 01/02R 1 1 1CES 1

 4. Procedure
_________

 (Ref. Fig. 201/TASK 55-33-13-991-002)
 Subtask 55-33-13-020-051

 A. Open/Remove the access panels.
 (1) For access panels 325BL, 325BR, 325CL, 325CR and 325DL: NOTE : The opening procedure for one access panel is given; the
____ procedures for all access panels are almost the same.
 (a) Release the studs (1) and carefully open the access panel. R
 (b)
 Remove the quick release pin (5) from the lever assembly (2).

 (c)
 Align the holes (3) and (4) and install the quick release pin (5) through the two holes.


 (2) For access panels 325EL, 325ER and 325DR: NOTE : The removal procedure for one access panel is given; the
____ procedures for all access panels are almost the same.
 (a)
 Release the studs (6).

 (b)
 Hold the panel and release the studs (1).


 (c) Remove the access panel. R


R  Trailing Edge Access-Panels Figure 201/TASK 55-33-13-991-002
 1EFF : 1 1 1CES  ALL  1 111 55-33-13 Page 204 Aug 01/02


 TASK 55-33-13-410-002


 Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
 
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