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R  THE GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE 
R  BLOOD. THIS CONDITION CAN KILL YOU. 
R  WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER_______ 
R  SPECIAL MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. 
R  OBEY THE MANUFACTURERS INSTRUCTIONS. 
R  PUT ON PROTECTIVE CLOTHING. 
R  DO NOT GET THEM IN YOUR MOUTH. 
R  DO NOT SMOKE. 
R  DO NOT BREATHE THE GAS. 
R  THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN 
R  IRRITANT. 
R  GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 
R  1_  Use a clean lint-free cotton cloth MISCELLANEOUS (Material No.
R  19-003) and the cleaning agent CLEANING AGENTS (Material No. 
R  11-026) to clean the parts that follow: 
R  - The nuts (22) 
R  - The bolts (23) 
R  - The flange of the universal joint (21) 
R  - The flange of the torque shaft (20). 
R  2_  Dry the parts with compressed air.
R  3_  Make sure that the parts retained from the removed component
R  are clean and in the correct condition. 
R  4_  Clean the component interface and/or the adjacent area.
R  5_  Lubricate the torque splines as follows:
R  CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______ 
R  GREASE AND ASSEMBLY PASTE DO NOT MIX. 
R  - Apply a thin layer of the COMMON GREASE (Material No. 04-
R  018) to the splines of the torque shaft (20). 
R  Or:

 

R  - Apply a thin layer of the COMMON GREASE (Material No. 04-
R  022) to the splines of the torque shaft (20). 
R  6_  Apply a layer of the STORAGE PRESERVATION (Material No. 15-
R  007) to the parts that follow: 
R  - The nuts (22) 
R  - The bolts (23) 
R  - The flange of the universal joint (21) 
R  - The flange of the torque shaft (20). 
R  (d) Installation of the torque shaft 6222CM (6272CM) 
R  1_  Put the universal joint (21) in the installation position.
R  Make sure that the flange aligns with the torque shaft (20). 
R  2_  Install the bolts (23) and the nuts (22). Tighten the nuts
R  (22) with your hand. 
R  3_  TORQUE the nuts (22) to between 1.02 and 1.24 m.daN (90.26 and
R  109.73 lbf.in). 
R  (e) Install the PIN RIGGING FLAPS (2). 
R  1_  Make sure that you can remove/install the rigging pin (2)
R  easily. 
R  2_  If you cannot remove/install the rigging pin (2) easily do the
R  adjustment procedure again. 
R  (f) Make sure that: 
R  - You cannot see the spline engagement groove at the movable 
R  joint 
R  - The dimension "A" is a minimum of 6.5 mm (0.2559 in.) at the 
R  movable joint. 
R  (g) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 
R  (Ref. TASK 27-50-00-000-003)

 

R  Subtask 27-54-00-865-083 
R  E. Make sure that this(these) circuit breaker(s) is(are) closed: 
R  -------------------------------------------------------------------------------
R  PANEL DESIGNATION IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  49VU AUTO FLT/FAC1/28VDC 5CC1 B04 
R  49VU AUTO FLT/FAC1/26VAC 14CC1 B03 
R  121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 
R  121VU AUTO FLT/FAC2/28VDC 5CC2 M19 
R  121VU AUTO FLT/FAC2/26VAC 14CC2 M18 
R  Subtask 27-54-00-740-050 
R  F. Do a Check of the Position Pick-Off Units (PPUs) on the Centralized Fault 
R  Display-System (CFDS) 
R  (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-
R  002). 
R  (2) Get access to the SYSTEM REPORT/TEST (F/CTL) page on the Multipurpose 
R  Control Display-Unit (MCDU) (Ref. TASK 31-32-00-860-006). 
R  (3) Do a check of the flap PPU angles (deg) at the slat/flap control 
R  lever position FULL on the MCDU as follows: 
R  -------------------------------------------------------------------------------
R  ACTION RESULT 
R  -------------------------------------------------------------------------------

R  1. On the MCDU:  On the MCDU: 
　
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