R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)

 B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific talcum powder Material No. 05-013A C Z-24.223 RELEASE AGENT (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
57-41-37-000-004  Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)
 57-41-37-991-023 Fig. 403 57-41-37-991-020 Fig. 404
 3. Job Set-up
__________
 Subtask 57-41-37-941-067
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is installed on the flap/slat control lever.

 (3)
 Make sure that the warning notice is in position in the cockpit to tell persons not to operate the slats.

 (4)
 Make sure that the adjustable access platform is in position below the applicable access panel to be installed.

 1EFF : ALL 1 57-41-37Page 441 1 1 May 01/05R 1 1 1CES 1

 Subtask 57-41-37-865-079

 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 4. Procedure
_________ (Ref. Fig. 403/TASK 57-41-37-991-023) R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-216,
 Subtask 57-41-37-420-060
 A. Installation of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB)
 NOTE : On many of the access panels, the screws that retain the panel
____ have different lengths. Make sure that the correct screws are installed in their correct positions.
 (1)
 For the panel 522FB(622FB):

 (a)
 Hold the panel (1) in position. Install the four screws (2) and the screws (3).

 (b)
 TORQUE tighten the screws (2) and (3) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (2)
 For the panel 522JB(622JB):

 (a)
 Attach the lanyard with the bolt (6), hold the panel (4) in position and install the screws (5).

 (b)
 TORQUE tighten the screws (5) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (3)
 For the panel 522KB(622KB):

 (a)
 Hold the panel (7) in position. Install the three screws (8) and the screws (9).

 (b)
 TORQUE tighten the screws (8) and (9) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (4)
 For the panel 522LB(622LB):

 (a)
 Hold the panel (10) in position. Install the three screws (11) and the screws (12).

 (b)
 TORQUE tighten the screws (11) and (12) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (5)
 For the panel 522NB(622NB):

 (a)
 Hold the panel (13) in position. Install the five screws (14) and the screws (15).

 (b)
 TORQUE tighten the screws (14) and (15) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (6)
 For the panel 522QB(622QB):

 (a)
 Hold the panel (16) in position. Install the five screws (17) and the screws (18).

 (b)
 TORQUE tighten the screws (18) and (17) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (7)
 For the panel 522SB(622SB):

 (a)
 Hold the panel (19) in position. Install the four screws (20) and the screws (21).

 (b)
 TORQUE tighten the screws (20) and (21) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).

 (8)
 For the panel 522UB(622UB):

 (a) Hold the panel (22) in position. Install the two screws (23) and the screws (24).
　
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