(4)
 Make the surface rough by hand:

 -for all the areas to which it is not possible to get access with the sanding machine
 -if there is a risk of damage when you use the machine (overlaping sheet metal junctions, window and windshield frames, antenna supports, fuselage area behind the radome).

 (5)
 Use an abrasive rotative brush to clean the areas with round head rivets.

 Subtask 11-00-00-110-063
 C. Final Cleaning and Wiping
 (1)
 Rince the surfaces you have rubbed with CLEANING AGENTS (Material No. 11-004) then wipe with a clean lint-free cloth before the cleaning agent evaporates.

 (2)
 Lightly wipe again all the upper sections of the aircraft (fuselage above the windows, upper surface wings) with anti-dust pads before application of the wash primer.

 EFF : ALL

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 4. Procedure
_________

 Subtask 11-00-00-370-050
 A. Application of Identification and Marking Paints
 (1) Apply a coat of paint and then a cross paint. NOTE : The time between the last cleaning operation and the
____ application of paint must not be more than 4 hours.
R **ON A/C 001-002, 051-052, 151-199, 301-399, 401-499,
 Subtask 11-00-00-916-053-A
 B. Not Applicable
 **ON A/C 003-049, 053-099, 101-149, 201-299,

 Subtask 11-00-00-916-053
 B. Protection of exterior markings
 (1) Apply a PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No. 07-018) on all exterior functional and maintenance markings.
 **ON A/C ALL
 5. Close-up
________
 Subtask 11-00-00-942-051

 A. Clean the component interface and/or the adjacent area.
 EFF : ALL

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 TASK 11-00-00-960-001

 Replacement of the Reference Triangle
 1. Reason for the Job
__________________
 This procedure gives the information to bond the reference triangle on the tail cone after adjustment of the rudder or elevator to the neutral position.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific non-metallic spatula
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific adhesive tape No specific emery paper grade 320 Material No. 08-001 USA DOD-A-82720
 GENERAL PURPOSE ADHESIVE HONEYCOMB FILLER (Ref. 20-31-00) Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 EFF : ALL

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 C. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-24-00-820-001 Adjustment of the Rudder Neutral Position 27-34-00-820-003 Adjustment of the Elevator and Hydraulic Actuation to
 0.5 Degrees Nose-Up with the Gauge-Elevator Neutral
 Setting (98D27309006000) 27-34-00-820-003 Adjustment of the Elevator and Hydraulic Actuation to
 0.5 Degrees Nose-Up with the Gauge-Elevator Neutral Setting (98D27309002000)
R  AMM 11-21-27 P.Block 001 FLIGHT CONTROLS SRM 512111,P.Block001 SRM 512311,P.Block001
 3. Job Set-up
__________
 Subtask 11-00-00-120-053
 A. Removal of the reference triangle and preparation of the surface.
 (1)
 Remove the old reference triangle with a non-metallic spatula.

 (2)
 Remove the remaining adhesive compound as follows:

 (a)
 Clean the contact surfaces with MISCELLANEOUS (Material No. 19-003) soaked with CLEANING AGENTS (Material No. 11-003).

 (b)
 Remove the remaining adhesive coumpound with a non-metallic spatula.

 (c)
 Use adhesive tape to show the limits of the bonded area.

 (d)
 Make sure that the contact surfaces are in the correct condition and apply protection if necessary (Ref. SRM 512111,P.Block001) and (Ref. SRM 512311,P.Block001).

 (e)
 Apply finish paint on the contact surfaces.

 (f)
　
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