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时间:2011-03-27 12:40来源:蓝天飞行翻译 作者:航空
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R Material No. 04-024  AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (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. Expendable Parts

 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
75 cotter pin 76 cotter pin R 76 cotter pin 77 cotter pin 78 cotter pin 79 cotter pin 80 cotter pin 81 cotter pin 82 cotter pin 83 cotter pin 84 cotter pin 85 cotter pin 86 cotter pin 87 cotter pin R 87 cotter pin 88 cotter pin R 88 cotter pin R 89 cotter pin 89 cotter pin
R  90 cotter pin 90 cotter pin 96 cotter pin 97 cotter pin 98 cotter pin 99 cotter pin 100 cotter pin 101 cotter pin 102 cotter pin 103 cotter pin 104 cotter pin 105 cotter pin 106 cotter pin 107 cotter pin 108 cotter pins
R  108 cotter pins
R  109 cotter pin 109 cotter pin
R  110 cotter pin 110 cotter pin 126 cotter pin 127 cotter pin 57-41-05 42C-003A57-41-05 04B-110 57-41-05 04C-11057-41-05 43C-003A57-41-05 43C-003A57-41-05 45C-003A57-41-05 09A-11057-41-05 46C-003A57-41-05 46C-003A57-41-05 48C-003A57-41-05 48C-003A57-41-05 49C-003A57-41-05 49C-003A57-41-05 50C-003A 57-41-05 50D-00357-41-05 50C-003A 57-41-05 50D-003 57-41-05 51C-00357-41-05 51C-003A 57-41-05 51C-00357-41-05 51C-003A57-41-05 42C-005A57-41-05 42C-007A57-41-05 43C-005A57-41-05 43C-007A57-41-05 45C-005A57-41-05 45C-007A57-41-05 46C-005A57-41-05 46C-007A57-41-05 48C-005A57-41-05 48C-007A57-41-05 49C-005A57-41-05 49C-007A57-41-05 50C-005A 57-41-05 50D-005 57-41-05 51C-00557-41-05 51C-005A 57-41-05 51C-00557-41-05 51C-005A57-41-05 40C-003A57-41-05 40C-007A -------------------------------------------------------------------------------


FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
128 cotter pin 57-41-05 41C-003A 129 cotter pin 57-41-05 02B-110
R  129 cotter pin 57-41-05 02C-110 130 cotter pin 57-41-05 44C-003A 131 cotter pin 57-41-05 44C-007A 132 cotter pin 57-41-05 47C-003A 133 cotter pin 57-41-05 47C-003A 139 cotter pin 57-41-05 40C-005A 140 cotter pin 57-41-05 40C-007A 141 cotter pin 57-41-05 41C-005A 142 cotter pin 57-41-05 41C-007A 143 cotter pin 57-41-05 44C-005A 144 cotter pin 57-41-05 44C-007A 145 cotter pin 57-41-05 47C-005A 146 cotter pin 57-41-05 47C-007A
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-84-61-000-001 Removal of the Slat Tracks 1 thru 4
 27-84-61-400-004 Installation of the Slat Tracks 1 thru 4
 27-84-62-000-001 Removal of the Slat Tracks 5 thru 12
 27-84-62-400-001 Installation of the Slat Tracks 5 thru 12
 27-84-63-000-001 Removal of the No. 1 Slat
 27-84-63-400-002 Installation of the No. 1 Slat
 27-84-64-000-001 Removal of the No. 2 Slat
 27-84-64-400-002 Installation of the No. 2 Slat
 27-84-65-000-001 Removal of the No. 3 Slat
 27-84-65-400-002 Installation of the No. 3 Slat
 27-84-66-000-001 Removal of the No. 4 Slat
 27-84-66-400-002 Installation of the No. 4 Slat
 27-84-67-000-001 Removal of the No. 5 Slat
 27-84-67-400-002 Installation of the No. 5 Slat
 57-41-33-991-001 Fig. 401
 57-41-33-991-002 Fig. 402

 

 3. Job Set-up
__________
 Subtask 57-41-33-941-051
 A. Safety Precautions
 (1)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed on the flap/slat control lever.

 (2)
 Make sure that the warning notices are in position in the cockpit to tell persons not to operate the flaps or slats.

 (3)
 Make sure that the safety barriers are in position.


 Subtask 57-41-33-860-050
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the adjustable access platform is in position below the applicable wing inboard and outboard leading edge, zones 521

 (621) or 522 (622).

 (2)
 Make sure that the applicable slats have been removed:

 -
for the rollers at slat tracks 1, 2, 3 and/or 4, remove the slat No. 1 (Ref. TASK 27-84-63-000-001)

 -
for the rollers at slat tracks 5 and/or 6, remove the slat No. 2 (Ref. TASK 27-84-64-000-001)

 -
for the rollers at slat tracks 7 and/or 8, remove the slat No. 3 (Ref. TASK 27-84-65-000-001)
 
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