A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(99)

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

No specific No specific No specific  blanking capscircuit breaker(s) safety clip(s)access platform 1.6 m (5 ft. 3 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  31-32-00-860-006 27-94-34-991-001  Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL PageFig. 401
 3. Job Set-up__________ 
R  Subtask 27-94-34-810-050 
R  A. Trouble Shooting Data 
R R R R R R R R R  (1) You can print the Trouble Shooting Data (TSD) as follows: - get access to the SYSTEM/REPORT/TEST (Ref. TASK 31-32-00-860-006). - on this page, push the line key adjacent to the EFCS1 and/or EFCS2 indication. - on this page, push the line key adjacent to the LAST LEG REPORT indication. - on this page, push the line key adjacent to the failure(s) to get the TROUBLE SHOOTING DATA page. - print the TROUBLE SHOOTING DATA page.

 

 Subtask 27-94-34-010-050 R B. Get Access
 (1)
 Put the access platform in position.

 (2)
 Open the access door:
 FOR 1CE1, 1CE2
 824
 FOR 1CE3
 811

 (3)
 Put the access platform in position at the access door 822.

 (4)
 Open the access door 822.

 (5)
 On the battery power center 105VU:

 -loosen the two screws and remove the protective cover
 Subtask 27-94-34-865-050
R C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 1CE1
 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 FOR 1CE2 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 FOR 1CE3 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-94-34-991-001)
 Subtask 27-94-34-020-050

 A. Removal of the SEC
 (1)
 Loosen the knurled nuts (4).

 (2)
 Lower the nuts (4).

 (3)
 Pull the SEC (1) on its rack (3) to disconnect the electrical connectors (2).

 (4)
 Remove the SEC (1).

 (5)
 Put blanking caps on the disconnected electrical connectors (2).

 

 Spoiler Elevator Computer (SEC)
 Figure 401/TASK 27-94-34-991-001
 1EFF :  ALL  1  27-94-34 Page 403 
1  1  Feb 01/98
 1  1
 1CES  1

 

 TASK 27-94-34-400-001
 Installation of the SEC (1CE1,1CE2,1CE3)
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-94-34-991-001 Fig. 401
 FOR FIN 1CE1, 1CE2 R 52-41-00-410-002 Close the Avionics Compartment Doors after Access R
 FOR FIN 1CE3 27-94-00-710-001 Operational Test of the Spoiler Elevator Computer 3
 (SEC 3) FOR FIN 1CE1 27-94-00-710-002 Operational Test of the Spoiler Elevator Computer 1
 (SEC 1) FOR FIN 1CE2 27-94-00-710-003 Operational Test of the Spoiler Elevator Computer 2
 (SEC 2) 3. Job Set-up

__________
 Subtask 27-94-34-010-052
 A. Get Access
 (1)
 Make sure that the access platform is in position at the access doors 822, 824 and 811.

 (2)
 Make sure that the access doors 822 are open:
 FOR 1CE1, 1CE2
 824
 FOR 1CE3
 811

 (3)
 On the battery power center 105VU:

 -Make sure that the protective cover is open.
 Subtask 27-94-34-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 1CE1
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(99)