-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
**ON A/C 001-003, 051-054,
53-56-11-991-001 Fig. 401
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
53-56-11-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-56-11-865-050
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
EFF : ALL
53-56-11Page 402
Subtask 53-56-11-010-050
B. Get Access
(1)
Put the THS to the zero position (Ref. TASK 27-41-00-220-003).
(2)
Put the warning notice in position to tell persons not to operate the flight controls.
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.
(3)
Put the access platform below Z312 and Z314.
(4)
Put the adjustable access platform below the THS.
(5)
Open the access doors 312AR, 314AR.
(6)
Open the trailing edge panels 334AB, 344AB, 334AT, 344AT (Ref. TASK 55-13-11-000-001).
(7)
Remove the THS aprons (Ref. TASK 55-15-11-000-001).
(8)
Remove the fairings of the THS (Ref. TASK 53-55-13-000-001).
(9)
Remove the diagonal support struts (Ref. TASK 53-53-11-000-002).
4. Procedure
_________
**ON A/C 001-003, 051-054,
(Ref. Fig. 401/TASK 53-56-11-991-001) R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 53-56-11-991-001-A)
EFF : ALL
53-56-11Page 403
Trimmable Horizontal Stabilizer-Fittings Figure 401/TASK 53-56-11-991-001- 12 (SHEET 1)
R EFF : 001-003, 051-054, 53-56-11 Page 404 May 01/05
CES
Trimmable Horizontal Stabilizer-Fittings Figure 401/TASK 53-56-11-991-001- 22 (SHEET 2)
R EFF : 001-003, 051-054, 53-56-11 Page 405 May 01/05
CES
Trimmable Horizontal Stabilizer-Fittings Figure 401A/TASK 53-56-11-991-001-A12 (SHEET 1)
R EFF : 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499, 53-56-11 Page 406 Aug 01/05
CES
Trimmable Horizontal Stabilizer-Fittings Figure 401A/TASK 53-56-11-991-001-A22 (SHEET 2)
R EFF : 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499, 53-56-11 Page 407 Aug 01/05
CES
R **ON A/C 001-003, 051-054,
Subtask 53-56-11-020-050
A. Removal:
(1) Remove the bolt (16) as follows:
(a) If the bolt (16) is safetied with a STA-LOK nut (Ref. TASK 20-22-00-000-001):
1 Use the TOOL - EXTRACTION, TAB WASHERS STA-LOK NSA5454 (SL90-
_ 314-4375) and remove the tab washer (35) with the spring ring (36).
2 Use the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-
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