R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
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REFERENCE DESIGNATION
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Material No. 09-018 Material No. 09-019 Material No. 11-004 Material No. 15-007 Material No. 19-003 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT (Ref. 20-31-00)USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
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REFERENCE DESIGNATION
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R R R R R R R 27-50-00-400-003 27-50-00-866-009 27-54-00-710-001 27-54-45-000-008 27-54-45-000-009 27-54-45-000-010 27-54-45-000-012 27-54-45-000-013 27-54-45-400-008 27-54-45-400-009 27-54-45-400-010 27-54-45-400-012 27-54-45-400-013 57-51-37-000-004 Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Retraction of the Flaps on the GroundOperational Test of the Flap System Removal of the Torque Shafts 6216CM(6266CM)/6226CM(6276CM)Removal of Torque Shaft 6218CM(6268CM)Removal of the Torque Shaft 6222CM(6272CM)Removal of the Torque Shaft 6228CM(6278CM)Removal of the Torque Shaft 6232CM(6282CM) Installation of the Torque Shafts 6216CM(6266CM)/6226CM(6276CM)Installation of the Torque Shaft 6218CM(6268CM)Installation of the Torque Shaft 6222CM(6272CM)Installation of the Torque Shaft 6228CM(6278CM)Installation of the Torque Shaft 6232CM(6282CM) Removal of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)
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R R R 57-51-37-400-004 27-54-44-991-001 Installation of the Access Panels 575AB/575BB/575CB/575DB/575EB/575FB/575GB/ 575HB (675AB/675BB/675CB/675DB/675EB/675FB/675GB/675HB)Fig. 401
3. Job Set-up__________
(Ref. Fig. 401/TASK 27-54-44-991-001)
Subtask 27-54-44-941-055
A. Safety Precautions
(1) Make sure that the safety barriers are in position.
(2) Make sure that the warning notice is in the cockpit to tell persons not to operate the landing-gear doors.
(3) Make sure that the warning notice is on panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-54-44-860-053
B. Aircraft Maintenance Configuration
R R (1) Make sure that the access platform is below the applicable torque shaft.
R (2) Make sure that the flaps are retracted fully (Ref. TASK 27-50-00-866-009).
(3) Make sure that the applicable torque shaft (11) is removed (Ref. TASK 27-54-45-000-008), (Ref. TASK 27-54-45-000-009), (Ref. TASK 27-54-45-000-010), (Ref. TASK 27-54-45-000-012), (Ref. TASK 27-54-45-000-013): - FOR 6215CM the torque shaft 6216CM - FOR 6225CM the torque shaft 6226CM - FOR 6265CM the torque shaft 6266CM - FOR 6275CM the torque shaft 6276CM - FOR 6219CM
the torque shaft 6218CM
-
FOR 6269CM
the torque shaft 6268CM
-
FOR 6223CM
the torque shaft 6222CM
-
FOR 6273CM
the torque shaft 6272CM
-
FOR 6229CM
the torque shaft 6228CM
-
FOR 6279CM
the torque shaft 6278CM
-
FOR 6231CM
the torque shaft 6232CM
-
FOR 6281CM
the torque shaft 6282CM.
R (4) Make sure that the applicable access panels 575EB (675EB) have been R removed (Ref. TASK 57-51-37-000-004).
(5)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is installed on the flap/slat control lever on panel 114VU.
(6)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is installed on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
Subtask 27-54-44-865-051
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
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