R 1EFF : ALL 1 36-22-16Page 464 1 1 May 01/05 1 1 1CES 1 C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004 27-80-00-866-005 36-22-00-710-001
R 57-41-37-000-003 R 57-41-37-000-004 R R R 57-41-37-400-002 R R R 57-41-37-400-003
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 GroundRetracting the Slats on the GroundOperational 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) Installation of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Installation of the Access Panel 522AT(622AT)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 36-22-16-941-062
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 36-22-16-860-073
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 57-41-37-000-003), (Ref. TASK 57-41-37-000-004):
-
FOR 27HF, 50HF
panels 521BT, 522AT, 521HB, 522AB
-
FOR 43HF, 66HF
panels 621BT, 622AT, 621HB, 622AB
-
FOR 54HF, 23HF panels 521BT, 522AT, 521HB, 522AB, 521EB, 521GB
-
FOR 70HF, 39HF panels 621BT, 622AT, 621HB, 622AB, 621EB, 621GB.
Subtask 36-22-16-865-068
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
Subtask 36-22-16-420-061
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 (9), (10), (11) and (12) 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 0.5 mm (0.0196 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.
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