-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1.
Reason for the Job
__________________
Because the free movement is more than the limits.
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice
1EFF : ALL 1 27-14-41Page 601 1 1 May 01/00R 1 1 1CES 1
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
2 bush 27-14-05 31A-170A 4 flanged bush 27-14-05 21 -150 6 flanged bush 27-14-05 21 -150 8 flanged bush 27-14-05 21 -150 11 bush 27-14-05 31A-170A
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-14-41-000-001 Removal of the Aileron
27-14-41-400-001 Installation of the Aileron
**ON A/C 001-003, 051-052,
27-14-41-991-003 Fig. 601 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
27-14-41-991-003-A Fig. 601A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-14-41-941-054
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position to tell persons not to operate the flight controls.
Subtask 27-14-41-010-051
B. Get Access
(1) Remove the applicable aileron (Ref. TASK 27-14-41-000-001).
4. Procedure
_________
**ON A/C 001-003, 051-052,
(Ref. Fig. 601/TASK 27-14-41-991-003) R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 601A/TASK 27-14-41-991-003-A)
**ON A/C ALL
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 27-14-41-220-051
A. Dimensions of the Aileron
Aileron Fits and Clearances
Figure 601/TASK 27-14-41-991-003- 12 (SHEET 1)
R 1EFF : 001-003, 051-052, 1 27-14-41Page 604 1 1 May 01/05 1 1 1CES 1
Aileron Fits and Clearances
Figure 601/TASK 27-14-41-991-003- 22 (SHEET 2)
R 1EFF : 001-003, 051-052, 1 27-14-41Page 605 1 1 May 01/05 1 1 1CES 1
Aileron Fits and Clearances Figure 601A/TASK 27-14-41-991-003-A
R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-14-41Page 606 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | View B | 15.841 | 15.859 | | | 15.807 | | | | OD 5 |(0.6236) |(0.6243) | | |(0.6223) | | | | | | | 0.016 | 0.052 | | | 0.120 | | | | | (0.0006)| (0.0020)| | |(0.0047)| | View B | 15.875 | 15.893 | | | | 15.927 | | | ID 2 |(0.6250) |(0.6257) | | | |(0.6270) | | -------------------------------------------------------------------------------
Subtask 27-14-41-220-052
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