B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
Material No. 05-005 GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)USA MIL-C-16173 GRADE II
Material No. 09-013 CORROSION PREVENTIVE (Ref. 20-31-00)USA MIL-PRF-81733 TYPE I CLASS A
CORROSION INHIBITING BRUSH CONSISTENCY
Material No. 09-019 (Ref. 20-31-00)USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT
Material No. 11-002 (Ref. 20-31-00)USA MIL-PRF-680
Material No. 16-003 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00)F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 27-00-00-080-002 27-00-00-480-002 27-50-00-866-009 27-54-00-710-001 29-00-00-864-001 32-12-00-410-001 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)Retraction of the Flaps on the GroundOperational Test of the Flap SystemPut the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionClose the Main Gear Doors after Access
27-54-41-991-001 FOR FIN 6253CM Fig. 401
32-12-00-010-001 Open the Main Gear Doors for Access
1EFF : ALL 1 27-54-41Page 408 1 1 May 01/04R 1 1 1CES 1
3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-41-860-053
A. Aircraft Maintenance Configuration
(1)
Make sure that the the flaps are in the the 0 degree position (Ref. TASK 27-50-00-866-009).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) (Ref. TASK 27-00-00-480-002) is installed on the slat/flap control lever.
(3)
Make sure that the Green and Yellow hydraulic systems are depressurized and put them in the maintenance configuration (Ref. TASK 29-00-00-864-001)
(4)
Make sure that the PIN RIGGING-FLAPS (TRACK 1) (98D27504005000) is installed in the flap track position 1 to lock the flap transmission: FOR 6203CM
-
lock the left flap transmission.
FOR 6253CM
-
lock the right flap transmission.
(5)
Make sure that the warning notice is in position to tell persons not to pressurize the hydraulic systems.
(6)
Make sure that the main doors of the main gear are open (Ref. TASK 32-12-00-010-001).
(7)
Make sure that the access platform is in position at the opening of the main gear main door.
R **ON A/C 301-399,
R Subtask 27-54-41-860-053-A
R A. Aircraft Maintenance Configuration
R (1) Make sure that the the flaps are in the the 0 degree position
R (Ref. TASK 27-50-00-866-009).
R (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER
R (98D27803000000) (Ref. TASK 27-00-00-480-002) is installed on the
R slat/flap control lever.
R (3) Make sure that the Green and Yellow hydraulic systems are
R depressurized and put them in the maintenance configuration
R (Ref. TASK 29-00-00-864-001)
R (4) Make sure that the PIN RIGGING FLAPS (98D27504006000) is installed in
R the flap track position 1 to lock the flap transmission:
R FOR 6203CM
R - lock the left flap transmission.
R FOR 6253CM
R - lock the right flap transmission.
R (5) Make sure that the warning notice is in position to tell persons not
R to pressurize the hydraulic systems.
R (6) Make sure that the main doors of the main gear are open (Ref. TASK
R 32-12-00-010-001).
R (7) Make sure that the access platform is in position at the opening of
R the main gear main door.
R **ON A/C ALL
Subtask 27-54-41-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
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