**ON A/C 001-049, 051-061, 101-105, 201-203,
 27-84-61-991-007 Fig. 601 R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 27-84-61-991-007-A Fig. 601A
 **ON A/C ALL
 27-84-61-991-008 Fig. 602
 3. Job Set-up
__________
 Subtask 27-84-61-941-059

 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice in the cockpit to tell persons not to operate the slat controls.

 Subtask 27-84-61-860-052
 B. Aircraft Maintenance Configuration
 **ON A/C 001-049, 051-061, 101-105, 201-203,

 (Ref. Fig. 601/TASK 27-84-61-991-007)

 Slat No. 1, Tracks 1 and 2 - Attachment Details
 Figure 601/TASK 27-84-61-991-007

R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-84-61Page 603 1 1 May 01/05 1 1 1CES 1R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,

 (Ref. Fig. 601A/TASK 27-84-61-991-007-A)
 **ON A/C ALL

 (Ref. Fig. 602/TASK 27-84-61-991-008)
 (1)
 Remove the No. 1 Slat (Ref. TASK 27-84-63-000-001).

 (2)
 Remove the applicable Slat track (Ref. TASK 27-84-61-000-001).

 (3)
 For the Slat tracks 1 and 2:

 (a)
 Remove the nut (7), the washer (6) and the bolt (9).

 (b)
 Remove the nut (16), the washer (15) and the bolt (32).

 (c)
 Remove the nut (29), the locking plate (30), the nut (20), the washers (18) and (19), the bolt (28) and the eccentric bush (27).

 (d)
 Remove the links (4) and (10) and the bolt (31).

 (e)
 Remove the adjustment link (22). NOTE : The bolts (1) and (33) and their related nuts and washers

____ were removed when the Slat No. 1 was removed.
 (4) For the Slat tracks 3 and 4:
 (a)
 Remove the nut (15), the locking plate (16), the nut (8), the washer (7), the bolt (14) and the eccentric bush (13).

 (b)
 Remove the links (4) and (18) and the bolt (17). NOTE : The bolts (1) and (20) were removed when the Slat No. 1

____
 was removed.

 4. Procedure.
__________
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 (Ref. Fig. 601/TASK 27-84-61-991-007)

 Slat No. 1, Tracks 1 and 2 - Attachment Details Figure 601A/TASK 27-84-61-991-007-A
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-84-61Page 605 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 Slat No. 1, Tracks 3 and 4 - Attachment Details Figure 602/TASK 27-84-61-991-008
 1EFF : 1 1R 1CES  ALL  1 11 1 27-84-61 Page 606 Feb 01/01

R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 601A/TASK 27-84-61-991-007-A)
 **ON A/C ALL
 (Ref. Fig. 602/TASK 27-84-61-991-008)
 Subtask 27-84-61-220-052
 A. Dimensional Check of the Slat-to-Track Attachment Fittings, Track 1 thru 4
 (1) Fits and clearance dimensions
 NOTE : The limits on the chrome-plated surfaces only apply when there
____ is a layer of chrome on the bearing surfaces.
 -------------------------------------------------------------------------------| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | B | 19.009 | 19.030 | | | 18.977 | | | | OD 1 |(0.7483) |(0.7492) | | |(0.7471) | | | | | | | 0.027 | 0.069 | | | 0.133 | | | | | (0.0010)| (0.0027)| | |(0.0052)| | B | 19.057 | 19.078 | | | | 19.110 | | | ID 2 |(0.7502) |(0.7511) | | | |(0.7523) | | -------------------------------------------------------------------------------
Subtask 27-84-61-220-053
 B. Dimensional Check of the Slat-to-Track Attachment Fittings, Track 1 thru 4
 (1) Fits and clearance dimensions
 NOTE : The limits on the chrome-plated surfaces only apply when there
____ is a layer of chrome on the bearing surfaces.

 -------------------------------------------------------------------------------
| 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | B | 19.009 | 19.030 | | | 18.993 | | | | OD 1 |(0.7483) |(0.7492) | | |(0.7477) | | | | | | | 0.007 | 0.041 | | | 0.073 | | | | | (0.0002)| (0.0016)| | |(0.0028)| | B | 19.037 | 19.050 | | | | 19.066 | | | ID 3 |(0.7494) |(0.7500) | | | |(0.7506) | | -------------------------------------------------------------------------------
　
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