B. Consumable Materials
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REFERENCE DESIGNATION
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Material No. 04-018
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
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REFERENCE DESIGNATION
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27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 57-51-37-000-002 Removal of the Access Panels 573AB(673AB),
573BB(673BB), 573CB(673CB)
57-51-37-000-004 Removal of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
R **ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-45-991-001 Fig. 401 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
27-54-45-991-001-A Fig. 401A
**ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-45-991-003 Fig. 404
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
27-54-45-991-003-A Fig. 404A
FOR FIN 6216CM
57-51-37-400-002 Installation of the Access Panels 573AB(673AB),
573BB(673BB), 573CB(673CB)
FOR FIN 6226CM
57-51-37-400-004 Installation of the Access Panels
575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB
(675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB) FOR FIN 6266CM 57-51-37-400-002 Installation of the Access Panels 573AB(673AB),
573BB(673BB), 573CB(673CB)
FOR FIN 6276CM
57-51-37-400-004 Installation of the Access Panels
575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
**ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 401/TASK 27-54-45-991-001)
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-54-45-991-001-A)
**ON A/C ALL
Subtask 27-54-45-941-084
A. Safety Precautions
(1) Make sure that the safety barriers are in position.
(2) Make sure that the warning notice is in position to tell persons not to operate the slat/flap controls.
Subtask 27-54-45-860-070
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.
R (1) Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
R R (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever on panel 114VU.
(3) Make sure that the access platform is in the applicable position.
(4) Make sure that the applicable spoiler is in the 'M' (Maintenance) position (Ref. TASK 27-60-00-866-002).
(5) Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
R R R R (6) Make sure that the applicable access panel is removed: - for 6216CM, panel 573CB (Ref. TASK 57-51-37-000-002) - for 6226CM, panel 575DB (Ref. TASK 57-51-37-000-004) - for 6266CM, panel 673CB (Ref. TASK 57-51-37-000-002) - for 6276CM, panel 675DB (Ref. TASK 57-51-37-000-004).
(7) Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on the flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the removed component.
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