Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004 27-80-00-866-005 36-22-00-710-001 57-41-37-000-003
R 57-41-37-000-004 R R R 57-41-37-000-006 R R R R 57-41-37-400-002 R R
57-41-37-400-003 R 57-41-37-400-006 R R R R 36-22-16-991-001 R 36-22-16-991-002 R 36-22-16-991-003 R 36-22-16-991-004 R 36-22-16-991-005 R 36-22-16-991-009 R 36-22-16-991-011
3. Job Set-up
__________
Extending the Slats on the Ground
Retracting the Slats on the Ground
Operational Test of the Overheat Detection System
Removal of the Access Panel 522AT(622AT)
Removal of the Pressure-Relief Panels 521AB(621AB),
521CB(621CB), 521EB(621EB), 522AB(622AB),
522CB(622CB)
Removal of the Access Panels 522FB(622FB),
522JB(622JB), 522KB(622KB), 522LB(622LB),
522NB(622NB), 522QB(622QB), 522SB(622SB),
522UB(622UB)
Installation of the Pressure-Relief Panels
521AB(621AB), 521CB(621CB), 521EB(621EB),
522AB(622AB), 522CB(622CB)
Installation of the Access Panel 522AT(622AT)
Installation of the Access Panels 522FB(622FB),
522JB(622JB), 522KB(622KB), 522LB(622LB),
522NB(622NB), 522QB(622QB), 522SB(622SB),
522UB(622UB)
Fig. 401
Fig. 402
Fig. 403
Fig. 404
Fig. 405
Fig. 406
Fig. 407

R (Ref. Fig. 401/TASK 36-22-16-991-001, 402/TASK 36-22-16-991-002, 403/TASK R 36-22-16-991-003, 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005)
 Subtask 36-22-16-941-061
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notice is in position in the cockpit to tell persons not to operate the slat controls.

 (2)
 Install a protective sleeve (26) on the overheat sensing element (14) or (17) at each clamp (25).

 (3)
 Close the clamps (25) sufficiently to hold the overheat sensing element (14) or (17) in position. Let the overheat sensing element

 (14) or (17) be sufficiently free for you to make the connections.

 (4)
 Install the overheat sensing element 26HF(42HF) and 53HF(69HF):

 (a)
 At the pylon outboard closing-rib, remove the blanking caps from the connectors (19) and (22).

 (b)
 Install the connector (22) in the flanged attachment (21).

 (c)
 Install the nut (20) on the connector (22).

 (d)
 TORQUE the nut (20) to between 0.56 and 0.68 m.daN (49.55 and

 60.17 lbf.in).

 (e)
 Install the connector (19) on the connector (22).

 (f)
 TORQUE the connector (19) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).

 (g)
 At the outboard telescope-rib, remove the blanking caps from the connectors (19), (22), (23) and (24).

 (h)
 Install the connectors (22) and (23) in the flanged attachment (21).

 (i)
 Install the nut (20) on the connectors (22) and (23).

 (j)
 TORQUE the nut (20) to between 0.56 and 0.680 m.daN (49.55 and

 60.17 lbf.in).

 (k)
 Install the connectors (19) and (24) on the connectors (22) and (23).

 (l)
 TORQUE the connectors (19) and (24) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).

 Subtask 36-22-16-860-071
 B. Aircraft Maintenance Configuration 
R  (1) Make sure that the slats are fully extended (Ref. TASK 27-80-00-866-004).
 (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever on panel 114VU.
 (3) Make sure that the access platform is in position below the applicable access panels. 
R R R  (4) Make sure that the applicable access panels are removed (Ref. TASK 57-41-37-000-003), (Ref. TASK 57-41-37-000-004), (Ref. TASK 57-41-37-000-006):
 - FOR 26HF, 53HF panels 522AT, 522AB, 522CB, 522EB, 522FB
 - FOR 42HF, 69HF panels 622AT, 622AB, 622CB, 622EB, 622FB.
 Subtask 36-22-16-865-065
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
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