-
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 575316-02
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific warning notices
 No specific access platform 2.5 m (8 ft. 2 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-061A  D DAN 220 ALUMINIUM FOIL ADHESIVE TAPE (Ref. 20-31-00)
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 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-62-000-003 Removal of the Leading Edge Panels 2 and 5 on the
 Outboard Flap 27-54-62-400-003 Installation of the Leading Edge Panels 2 and 5 on
 the Outboard Flap 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
 4
 NTM 57-53-16 PART 9
 ASRM 575300 (for corrective action)

 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
 57-53-00-991-024 Fig. 622
R **ON A/C 106-149, 215-299, 401-499,
 57-53-00-991-024-A Fig. 622A
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 3. Job Set-up
__________
 Subtask 57-53-00-941-074
 A. Safety Precautions
 (1)
 Put warning notices in the cockpit to tell persons not to operate the flaps or slats.

 (2)
 Put the safety barriers in position.

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 B. Aircraft Maintenance Configuration
 (1)
 Extend the flaps fully (Ref. TASK 27-50-00-866-008).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.

 Subtask 57-53-00-865-101
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
 Subtask 57-53-00-010-073
 D. Get Access
 (1)
 Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633). (Ref. Fig. 622/TASK 57-53-00-991-024)

 (2)
 Remove the access panel 533AT (633AT) and the flap track 4 fairing 533CB (633CB) (Ref. TASK 57-55-11-000-001).

 (3)
 Remove the outboard flap leading edge panel 5 (Ref. TASK 27-54-62-000-003).

 (4)
 Remove and discard the cover from the RH inspection hole on the front spar.

 (5)
 Make sure that the inspection hole is clear of unwanted material.

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 Outboard Flap
 Figure 622/TASK 57-53-00-991-024

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R  **ON A/C 106-149, 215-299, 401-499,
 Subtask 57-53-00-010-073-A
 D. Get Access
 (1) Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633). (Ref. Fig. 622A/TASK 57-53-00-991-024-A)
 (2) Remove the access panel 533AT (633AT) and the flap track 4 fairing 533CB (633CB) (Ref. TASK 57-55-11-000-001).
 (3) Remove and discard the cover(s) from the applicable inspection hole(s) on the front spar.
 (4) Make sure that the applicable inspection hole is clear of unwanted material. 
　
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