R Subtask 05-51-29-420-056
R B. Installation of the Components
R (1) For the passenger/crew doors.
R (a) Install the escape slide (escape slide/raft) container of the
R related door (Ref. TASK 25-62-44-400-001).
R (b) Install the door lining panels of the related door.
R 1_ For the FWD passenger/crew door (Ref. TASK 25-23-46-400-001).
R 2_ For the aft passenger/crew door (Ref. TASK 25-23-46-400-002).
R (c) Install the door frame linings of the related door
R 1_ For the left FWD passenger/crew door (Ref. TASK 25-23-45-400-
R 006).
R 2_ For the right FWD passenger/crew door (Ref. TASK 25-23-45-400-
R 007).
R 3_ For the left aft passenger/crew door (Ref. TASK 25-23-45-400-
R 008).
R 4_ For the right aft passenger/crew door (Ref. TASK 25-23-45-400-
R 005).
R (2) For the emergency exits
R (a) Install the door lining panels of the related emergency exit.
R 1_ For the left FWD emergency exit door (Ref. TASK 25-23-47-400-
R 012).
R 2_ For the right FWD, right aft or left aft emergency exit
R (Ref. TASK 25-23-47-400-013).
R (b) Install the frame lining panels of the related emergency exit.
R 1_ For the left FWD emergency exit (Ref. TASK 25-23-47-400-004).
R 2_ For the right FWD emergency exit (Ref. TASK 25-23-47-400-009).
R 3_ For the left/right aft emergency exit (Ref. TASK 25-23-47-400-
R 010).
R Subtask 05-51-29-410-051
R C. Close Access
R (1) For the passenger/crew doors.
R (a) Obey the special precautions after the work on the door
R (Ref. TASK 52-10-00-860-002).
R (b) Close the related passenger/crew door (Ref. TASK 52-10-00-410-
R 001).
R (2) For the emergency exit.
R (a) Obey the special precautions after the work on the door
R (Ref. TASK 52-22-00-860-004).
R (b) Close the related emergency exit (Ref. TASK 52-22-00-410-002).
R (3) Remove the access platform(s).
R (4) Make sure that the work area is clean and clear of tool(s) and other
R items.
INSPECTION AFTER SIGNIFICANT MLG VIBRATION AT TOUCH-DOWN - INSPECTION/CHECK
___________________________________________________________________________
TASK 05-51-31-200-001
Inspection after Significant MLG Vibration at Touch-Down
1. Reason for the Job
__________________
This inspection is recommended to make sure that the bottom cardan joint and the torque link installation are in a serviceable condition if significant MLG vibration occurs at touchdown.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific feeler gauge No specific safety barriers No specific warning notice No specific access platform 1.5 m (4 ft. 11 in.) 460005834 1 TUBE SPANNER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-004 D DA-2-657-4 SEALANT, AERODYNAMIC SMOOTHING-OBSOLETE USE 09016 (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001
07-11-00-586-002
24-41-00-862-002
29-00-00-864-001
32-00-00-481-001
32-11-16-000-001
32-11-16-400-001
R 32-11-27-200-001 32-11-27-210-001
32-12-00-010-001
32-12-00-410-001
32-31-00-720-002
R 32-33-00-720-001 05-51-31-991-001 05-51-31-991-002 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 時(shí)間限制/維護(hù)檢查 4(123)
