(5)
 TORQUE the nut (20) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).

 (6)
 Install the connector (19) on the connector (22).

 (7)
 TORQUE the connector (19) to between 0.56 and 0.68 m.daN (49.55 and

 60.17 lbf.in). R WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,
_______ R REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE R LOCKWIRE CAN CUT OR BLIND YOU.
 (8)
 Safety the connectors (19) and (22) and the nut (20) with MISCELLANEOUS (Material No. 19-010).

 (9)
 Install a protective sleeve (26) on the overheat sensing element (5), (6), (7) or (8) at each clamp (25). Close the clamps (25) and lock the quick-release fasteners (27).

 (10) Install a protective sleeve (26) on the overheat sensing element (5) or (6) at the fairlead (34). Install the removable part of the fairlead (34) with the bolt (33) and the nut (35).
 Subtask 36-22-16-865-072
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3HA1, 2HA1, 3HA2, 2HA2.
 Subtask 36-22-16-710-055
 D. Test
 (1) Do an operational test of the overheat detection system (Ref. TASK 36-22-00-710-001).

 5. Close-up
________

 (Ref. Fig. 401/TASK 36-22-16-991-001)
 Subtask 36-22-16-410-055
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items. 
R R  (2) Install the applicable access panels (Ref. TASK 57-41-37-400-002), (Ref. TASK 57-41-37-400-005):
R  - FOR 28HF, 49HF, 22HF, 55HF install 521AB, 521BB, 521CB, 521EB, 521GB, 521BT
R  - FOR 44HF, 65HF, 38HF, 71HF install 621AB, 621BB, 621CB, 621EB, 621GB, 621BT.
 Subtask 36-22-16-865-073
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 36-22-16-860-074
 C. Aircraft Configuration
 (1) Retract the slats fully (Ref. TASK 27-80-00-866-005).
 Subtask 36-22-16-942-055
 D. Removal of Equipment
 (1) Remove the safety barriers.
 (2) Remove the warning notice(s).
 (3) Remove the access platform(s).
 (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 SENSING ELEMENT - OVERHEAT, WINGS (LOOP A AND B) (21HF,22HF,23HF,24HF,25HF,
___________________________________________________________________________ 26HF,27HF,28HF,29HF,37HF,38HF,39HF,40HF,41HF,42HF,43HF...) - INSPECTION/CHECK
_____________________________________________________________________________
 TASK 36-22-16-200-001
 Detailed Inspection of the LH and RH Wing Leading Edge Overheat Sensing
 Elements

 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
R  Detailed inspection of the bleed air duct leak/sensing element detection system, for example, after a duct leak warning.
 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 notice
 No specific access platform 2.8 m (9 ft. 2 in.)

 B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground
R 27-80-00-866-005 Retracting the Slats on the Ground 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 53-35-11-000-001 Removal of the Wing-to-Fuselage Fairings 53-35-11-400-001 Installation of the Wing-to-Fuselage Fairings 57-41-37-000-003 Removal of the Access Panel 522AT(622AT) 57-41-37-000-004 Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) 57-41-37-000-005 Removal of the NACA Duct Panel 521BB(621BB) 57-41-37-000-006 Removal of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB) 57-41-37-400-002 Installation of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) 57-41-37-400-003 Installation of the Access Panel 522AT(622AT) 57-41-37-400-005 Installation of the NACA Duct Panel 521BB(621BB) 57-41-37-400-006 Installation of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB) 36-22-16-991-008 Fig. 601 36-22-16-991-007 Fig. 602
　
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