R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
49  cotter pin  27-54-44 01 -010
 D. Referenced Information
 ------------------REFERENCE  -------------------------------DESIGNATION ------------------------------

-------------------------------------------------------------------------------
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 27-54-45-000-007 Removal of the Torque Shafts
 6214CM(6264CM)/6220CM(6270CM) 27-54-45-400-007 Installation of the Torque Shafts 6214CM(6264CM)/6220CM(6270CM) 57-51-37-000-002 Removal of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB) 57-51-37-400-002 Installation of the Access Panels 573AB(673AB), 573BB(673BB), 573CB(673CB)
 1EFF : ALL 1 27-54-45Page 472 1 1 May 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-061, 101-103, 201-203,
R  27-54-45-991-001 Fig. 401 **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,
R  27-54-45-991-003 Fig. 404 **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 27-54-45-991-003-A **ON A/C ALL Fig. 404A
 3. Job Set-up__________ **ON A/C 001-049, 051-061, 101-103, 201-203,
R  (Ref. Fig. 401/TASK 27-54-45-991-001) **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 27-54-45-941-082
 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 flap/slat controls.

 Subtask 27-54-45-860-068
 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).
 (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.

R (4) Make sure that the applicable access panel is removed (Ref. TASK 57-R 51-37-000-002):
 -
for 6212CM, panel 573BB

 -
for 6262CM, panel 673BB.

 (5)
 Make sure that the torque shaft(s) 6214CM(6264CM) is/are removed (Ref. TASK 27-54-45-000-007).

 (6)
 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.

 Subtask 27-54-45-865-075
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-103, 201-203,
 (Ref. Fig. 404/TASK 27-54-45-991-003)
　
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