B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R 27-80-00-866-004 57-41-37-000-003 57-41-37-000-004 36-22-16-991-001 36-22-16-991-002 36-22-16-991-003 36-22-16-991-004 36-22-16-991-005 Extending the Slats on the Ground Removal of the Access Panel 522AT(622AT) Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)Fig. 401Fig. 402 Fig. 403 Fig. 404 Fig. 405
3. Job Set-up__________
R R (Ref. Fig. 401/TASK 36-22-16-991-001, 402/TASK 36-22-16-991-002, 403/TASK 36-22-16-991-003, 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005)
Subtask 36-22-16-941-054
A. Safety Precautions
(1) Put the safety barriers in position.
(2) Put a warning notice in position in the cockpit to tell persons not to operate the slat controls.
Subtask 36-22-16-860-061
B. Aircraft Maintenance Configuration
(1) Extend the slats fully (Ref. TASK 27-80-00-866-004).
(2) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever on panel 114VU.
Subtask 36-22-16-865-054
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------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
Subtask 36-22-16-010-054
D. Get Access
R R (1) Put the access platform in position below the applicable access panel.
R R (2) Remove the applicable access panels (Ref. TASK 57-41-37-000-003), (Ref. TASK 57-41-37-000-004):
- FOR 27HF, 50HF remove 521BT, 522AT, 521HB, 522AB
- FOR 43HF, 66HF remove 621BT, 622AT, 621HB, 622AB
- FOR 54HF, 23HF remove 521BT, 522AT, 521HB, 522AB, 521EB, 521GB
- FOR 70HF, 39HF remove 621BT, 622AT, 621HB, 622AB, 621EB, 621GB.
4. Procedure
_________
R
Subtask 36-22-16-020-057
A. Removal of the Overheat Sensing Elements
R R CAUTION : REMOVE OR INSTALL THE SENSING ELEMENTS CAREFULLY. DO NOT TWIST,_______ BEND OR CAUSE KINKS IN THE SENSING ELEMENTS.
(1) Release the quick-release fasteners (27) and open the clamps (25). Retain the protective sleeves (26).
(2) Remove and discard the cable-ties (30) and the retainers (28).
(3) Remove the support-plugs (29) from the RIB7 and the RIB8.
(4) Remove the support-plugs (29) from the overheat sensing elements (11) and (12).
(5) Remove the nut (35) and the bolt (33) from the fairlead (34). Retain the removable part of the fairlead (34) and the protective sleeves (26).
R R R WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,_______ REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
(6) Remove and discard the lockwire from the connectors (19) and (22) and the nut (20).
(7) Disconnect the connector (19) from the connector (22).
(8) Remove the nut (20) from the connector (22). Remove the connector (22) from the flanged attachment (21).
(9) Put blanking caps on all the disconnected connectors.
(10) Remove the applicable overheat sensing element (9), (10), (11) or (12).
TASK 36-22-16-400-005
Installation of the Overheat Sensing Elements 27HF(43HF),50HF(66HF),23HF(39HF), 54HF(70HF)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
1. Reason for the Job__________________
R R Self Explanatory
2. Job Set-up Information______________________
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