(2)
Make sure that the warning notice is in the cockpit to tell persons not to operate the slat controls.
Subtask 36-22-16-860-065
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 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 53-35-13-000-002), (Ref. TASK 53-35-11-000-001), (Ref. TASK 57-41-37-000-004), (Ref. TASK 57-41-37-000-005): - FOR 56HF, 81HF panels 191EB, 191CT, 521AB, 521BB, 521CB
- FOR 72HF, 80HF panels 192EB, 192CT, 621AB, 621BB, 621CB
- FOR 29HF, 83HF panels 191EB, 191CT, 191BT, 521AB, 521BB, 521CB
- FOR 45HF, 82HF panels 192EB, 192CT, 192BT, 621AB, 621BB, 621CB.
Subtask 36-22-16-865-056
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
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PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 49VU AIR BLEED/ENG 1/CTL 49VU AIR BLEED/ENG 1/MONG 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 122VU AIR BLEED/ENG 2/CTL 122VU AIR BLEED/ENG 2/MONG 5CV 3HA1 2HA1 7CV 3HA2 2HA2 B06D12D11R21Z23Z22
4. Procedure_________
R
Subtask 36-22-16-420-057
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 sensing element (1), (2), (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 applicable connectors and examine the connectors for the correct condition. Put the blanking caps on the connectors again.
Subtask 36-22-16-420-050
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 applicable overheat sensing element (1), (2), (7) or (8). Do not remove the blanking caps.
(2) Install a protective sleeve (26) on the overheat sensing element (1), (2), (7) or (8) at each clamp (25).
R Permitted Tolerances of the Sensing Elements Figure 406/TASK 36-22-16-991-009
1EFF : 1 1 1CES ALL 1 111 36-22-16 Page 415 May 01/05
R R Sensing Elements - Typical Installation Figure 407/TASK 36-22-16-991-011
1EFF : 1 1 1CES ALL 1 111 36-22-16 Page 416 May 01/05
(3)
Close the clamps (25) sufficiently to hold the overheat sensing element (1), (2), (7) or (8) in position. The overheat sensing element must be free for you to make the connections.
(4)
Install the overheat sensing element 29HF(45HF) (1) and 56HF(72HF)
(8)
as follows:
(a)
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).
