C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground 27-80-00-866-005 Retracting the Slats on the Ground 36-22-00-710-001 Operational Test of the Overheat Detection System 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)
57-41-37-400-002 Installation of the Pressure-Relief Panels
521AB(621AB), 521CB(621CB), 521EB(621EB),
522AB(622AB), 522CB(622CB) 57-41-37-400-005 Installation of the NACA Duct Panel 521BB(621BB) 36-22-16-991-001 Fig. 401 36-22-16-991-002 Fig. 402 36-22-16-991-003 Fig. 403 36-22-16-991-004 Fig. 404 36-22-16-991-005 Fig. 405 36-22-16-991-009 Fig. 406 36-22-16-991-011 Fig. 407
3. Job Set-up
__________
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 36-22-16-941-063
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.
Subtask 36-22-16-860-075
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 (4) Make sure that the applicable access panels are removed (Ref. TASK R 57-41-37-000-004), (Ref. TASK 57-41-37-000-005):
-
FOR 28HF, 49HF, 22HF, 55HF panels 521AB, 521BB, 521CB, 521EB, 521GB, 521BT
-
FOR 44HF, 65HF, 38HF, 71HF panels 621AB, 621BB, 621CB, 621EB, 621GB, 621BT.
Subtask 36-22-16-865-071
C. 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 49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
4. Procedure_________
R (Ref. Fig. 403/TASK 36-22-16-991-003)
Subtask 36-22-16-420-063
A. Preparation for Installation
(1) Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2) Do an inspection of the component interface and/or the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
R R (4) Examine the applicable overheat sensing element (5), (6), (7) and (8) for the correct condition. The element tube must not be twisted and the surface must be free of damage other than the limits that follow:
R (a) The maximum permitted depth of abrasions or dents is 0.05 mm (0.0019 in.).
R (b) The minimum permitted tube diameter at a dent is 1.78 mm (0.0700 in.).
(5) Remove the blanking caps from the overheat sensing element connectors and examine the connectors for the correct condition. Put the blanking caps on the connectors again.
Subtask 36-22-16-420-055
R B. Installation of the Overheat Sensing Elements
CAUTION : REMOVE OR INSTALL THE SENSING ELEMENTS CAREFULLY. DO NOT TWIST,_______ BEND OR CAUSE KINKS IN THE SENSING ELEMENTS.
R NOTE : Obey the permitted tolerances for the installation of the sensing____ elements: (Ref. Fig. 406/TASK 36-22-16-991-009, 407/TASK 36-22-16-991-011)
(1) Carefully install the overheat sensing element (5), (6), (7) or (8) and install the applicable grommets (36).
(2) Remove the blanking caps from the connectors (19) and (22).
(3)
Install the connector (22) in the flanged attachment (21).
(4)
Install the nut (20) on the connector (22).
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