• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 14:35来源:蓝天飞行翻译 作者:admin
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

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-84-49-000-001  Removal of the Type B Actuators 6027CM(6077CM)/6029CM(6079CM)/6035CM (6085CM)/6039CM(6089CM)/6045CM(6095CM)
 27-84-49-000-002  Removal of the Type B Actuators
 6033CM(6083CM)/6037CM(6087CM)/6041CM (6091CM) 27-84-64-000-001 Removal of the No. 2 Slat 27-84-65-000-001 Removal of the No. 3 Slat 27-84-66-000-001 Removal of the No. 4 Slat 27-84-67-000-001 Removal of the No. 5 Slat 27-84-69-000-001 Removal of the Closing Plates for the Slat Tracks 1
 thru 12 27-84-62-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 27-84-62-941-053
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice(s) in the cockpit to tell persons not to operate the slat controls.


 Subtask 27-84-62-010-050
 B. Get Access
 (1)
 Put the adjustable access platform below the applicable zone 510 or

 610.

 (2)
 Remove the applicable closing plate(s) (Ref. TASK 27-84-69-000-001).

 (3)
 Remove the applicable slat:

 -
for the tracks 5 and 6 (Ref. TASK 27-84-64-000-001)

 -
for the tracks 7 and 8 (Ref. TASK 27-84-65-000-001)

 -
for the tracks 9 and 10 (Ref. TASK 27-84-66-000-001)

 -
for the tracks 11 and 12 (Ref. TASK 27-84-67-000-001).

 

 


 (4) Remove the applicable actuators: - for the tracks 5, 6, 8, 10 and 12 (Ref. TASK 27-84-49-000-001) - for the tracks 7, 9, and 11 (Ref. TASK 27-84-49-000-002).
 (5) Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the slat/flap control lever.
 Subtask 27-84-62-865-053
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 4. Procedure_________
 (Ref. Fig. 401/TASK 27-84-62-991-001)
 Subtask 27-84-62-020-053 
R  A. Removal of the Slat Tracks 5 thru 12 
R R R  (1) Install the applicable TOOL-BACKSTOP SLAT (1) through the guide (4) on the side of the track (2). Install the backstop tool on the inboard side on the LH wing and on the outboard side on the RH wing: - for the tracks 5 thru 8 install the TOOL-BACKSTOP SLAT (TRACKS 5, 6, 7, AND 8) (98D27804015000) - for the tracks 9 thru 12 install the TOOL-BACKSTOP SLAT (TRACKS 9, 10, 11, AND 12) (98D27804016000).
 (2) Push the applicable slat backstop tool (1) against the rearstop (3) to disengage it from the track stop. Pull the track (2) from its installed position and remove it.
 (3) Remove the applicable TOOL-BACKSTOP SLAT (1) from the track (2).

 

 Slat Tracks 5 thru 12 - Location and Detail
 Figure 401/TASK 27-84-62-991-001
 1EFF :  ALL  1  27-84-62 Page 404 
1  1  Feb 01/98
 1  1
 1CES  1

 

 TASK 27-84-62-400-001
 Installation of the Slat Tracks 5 thru 12
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
R R Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice(s)
 No specific adjustable access platform 3.5 m (11 ft. 6 in.)
 98D27804015000 1 TOOL-BACKSTOP SLAT (TRACKS 5, 6, 7, AND 8)
 98D27804016000 1 TOOL-BACKSTOP SLAT (TRACKS 9, 10, 11, AND 12)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-024  AIB AIMS 09-06-001
 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM
 (Ref. 20-31-00)

 Material No. 09-018  USA AMS 3267/3
 
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8(79)