R 36-11-00-720-004 Leak Check of Engine Bleed Air Supply System 36-11-00-720-005 Functional Test of the Engine Bleed Air Supply System 36-11-17-400-001 Installation of the Heat-Exchanger Outlet-Temperature Sensor 6HA1(6HA2) 54-51-17-000-001 Removal of the Pylon-to-Wing Forward Attach Fitting at RIB4
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REFERENCE DESIGNATION ------------------------------------------------------------------------------- -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
54-51-17-400-001 Installation of Pylon-to-Wing Forward Attach Fitting at RIB4
57-41-37-000-004 57-41-37-000-005 57-41-37-400-002 Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)Removal of the NACA Duct Panel 521BB(621BB)Installation of the Pressure-Relief Panels
57-41-37-400-005 SIL 36-036 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)Installation of the NACA Duct Panel 521BB(621BB)
36-11-48-991-010 Fig. 401
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
R 36-11-48-991-011-A Fig. 402 **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,
R 36-11-48-991-012 Fig. 403 **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
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
36-11-48-991-018 Fig. 407 R **ON A/C 106-149, 211-299, 301-399, 401-499,
36-11-48-991-018-A Fig. 407A
**ON A/C ALL
3. Job Set-up
__________
Subtask 36-11-48-941-055
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in the cockpit on the panel 30VU, to tell persons not to operate the pneumatic systems.
(3)
Make sure that the warning notice is on the panel 114VU, to tell persons not to operate the flap/slat controls.
Subtask 36-11-48-860-053
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)
Make sure that the slats are fully extended (Ref. TASK 27-80-00-866-004).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever on panel 114VU.
(3)
Make sure that the access platform, adjustable is in position below the applicable access panels.
(4)
Make sure that the applicable access panels are removed (Ref. TASK 57-41-37-000-004), (Ref. TASK 57-41-37-000-005):
(a)
For the left wing: 521AB, 521BB, 521CB, 521DB, 521EB, and 521BT
(b)
For the right wing: 621AB, 621BB, 621CB, 621DB, 621EB, and 621BT.
Subtask 36-11-48-865-064
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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
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