**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
36-11-48-991-011-A Fig. 402
R **ON A/C 106-149, 211-299, 301-399, 401-499,
36-11-48-991-011 Fig. 402A
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
36-11-48-991-012 Fig. 403
R **ON A/C 106-149, 211-299, 301-399, 401-499,
36-11-48-991-012-A Fig. 403A
**ON A/C ALL
36-11-48-991-013 Fig. 404
36-11-48-991-014 Fig. 405
36-11-48-991-015 Fig. 406
3. Job Set-up
__________
Subtask 36-11-48-941-053
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put the warning notice in the cockpit on panel 30VU, to tell persons not to operate the pneumatic system.
(3)
Put the warning notices on the flap/slat control lever on panel 114VU, to tell persons not to operate the flap/slat controls.
Subtask 36-11-48-860-051
B. Aircraft Maintenance Configuration
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Fully extend the slats (Ref. TASK 27-80-00-866-004).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on panel 114VU.
Subtask 36-11-48-865-061
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 49VU AIR BLEED/ENG 1/MONG 2HA1 D11 121VU ENGINE/ENG2/FADEC B 4KS2 Q40 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
1EFF : ALL 1 36-11-48Page 403 1 1 Nov 01/04R 1 1 1CES 1
Subtask 36-11-48-010-057
D. Get Access
R R (1) Put the access platform, adjustable in position below the applicable access panels.
R R R (2) Remove the access panels (Ref. TASK 57-41-37-000-004), (Ref. TASK 57-41-37-000-005):
R R (a) For the left wing: 521AB, 521BB, 521CB, 521DB, 521EB, 521BT.
R (b) For the right wing: 621AB, 621BB, 621CB, 621DB, 621EB, 621BT.
4. Procedure_________
Subtask 36-11-48-020-080
A. Removal of the Bleed Air Ducts between the Fuselage and the Slat Track 1
(Ref. Fig. 401/TASK 36-11-48-991-010)
(1) Remove and discard the braided wire from the insulation muffs (2) and (7). Remove the insulation muffs (2) and (7).
(2) Remove the clamps (4) and (6).
(3) Remove the bleed-air duct (5) from the aircraft.
(4) Remove the nut (12), the facing washer (11), the insulation washer (13) and the bolt (14). Remove the insulation washer (9) and the facing washer (8) from the bolt (14).
(5) Disconnect the link assembly (10) from the bleed-air duct (1).
(6) Remove the clamp (3).
(7) Remove the bleed-air duct (1) from the aircraft.
(8) Install a blanking cap on the bleed-air duct in the fuselage.
Bleed Air Ducts from the Fuselage to the Slat Track 1 Figure 401/TASK 36-11-48-991-010
1EFF : ALL 1 36-11-48Page 405 1 1 Nov 01/04R 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
Subtask 36-11-48-020-081-A
B. Removal of the Bleed Air Duct between the Slat Track 1 and the Intermediate Rib
(Ref. Fig. 402/TASK 36-11-48-991-011-A, 403/TASK 36-11-48-991-012)
NOTE : You must remove the duct assembly (77) before you remove the bleed
____ air ducts between the Slat Track 1 and the Intermediate Rib.
(1)
Remove and discard the braided wire from the insulation muffs (29),
(46) and (64). Remove the insulation muffs (29), (46) and (64).
(2)
Remove the nut (31), the washer (32) and the bolt (33). Disconnect the bonding straps (30) and (25) from the duct assembly (24).
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