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时间:2011-03-27 12:50来源:蓝天飞行翻译 作者:航空
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 27-54-61-400-001 Installation of the Inboard Flap
 27-54-61-400-003 Installation of the Inboard Double-Slotted Flap

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 57-52-00-991-029 Fig. 628
 **ON A/C 301-399,

 57-52-00-991-029-A Fig. 628A
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 57-52-00-941-082

 A. Safety Precautions
 (1) Put a warning notice on the flap/slat control lever (panel 114VU) to tell persons not to operate the flaps.
 (2) Put the safety barriers in position. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-52-00-010-081
 B. Get Access
 (1)
 Put the access platform below the applicable zone 573 or 673.

 (2)
 Remove the inboard flap (Ref. TASK 27-54-61-000-001).

 


 **ON A/C 301-399,
 Subtask 57-52-00-010-081-A
 B. Get Access
 (1) Put the access platform below the applicable zone 573 or 673.
 (2) Remove the inboard flap (Ref. TASK 27-54-61-000-003).
 **ON A/C ALL

 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 628/TASK 57-52-00-991-029)
 **ON A/C 301-399,

 (Ref. Fig. 628A/TASK 57-52-00-991-029-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.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-52-00-220-065
 A. Dimensions of the Joint that Connects the Flap to the Flap Carriage (Track 1).
 (1) Do a check of the dimensions that follow:


 Inboard Flap - Fits and Clearances (Tracks 1 and 2)
 Figure 628/TASK 57-52-00-991-029

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page A664 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Inboard Flap - Fits and Clearances (Tracks 1 and 2) R Figure 628A/TASK 57-52-00-991-029-A


 1EFF : 301-399, 1 57-52-00Page A665 1 1 May 01/04 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | A | 50.740 | 50.770 | | | 50.689 | | | | OD 2 |(1.9976) |(1.9988) | | |(1.9956) | | | | | | | 0.030 | 0.072 | | | 0.174 | | | | | (0.0011)| (0.0028)| | |(0.0068)| | A | 50.800 | 50.812 | | | | 50.863 | | | ID 1 |(2.0000) |(2.0004) | | | |(2.0024) | | -------------------------------------------------------------------------------
Subtask 57-52-00-220-066
 B. Dimensions of the Joint that Connects the Flap to the Flap Carriage
 (Track 2).

 (1) Do a check of the dimensions that follow:
 -------------------------------------------------------------------------------| 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 | 31.975 | 31.991 | | | 31.945 | | | | OD 5 |(1.2588) |(1.2594) | | |(1.2576) | | | | | | | 0.009 | 0.050 | | | 0.110 | | | | | (0.0003)| (0.0019)| | |(0.0043)| | B | 32.000 | 32.025 | | | | 32.055 | | | ID 4 |(1.2598) |(1.2608) | | | |(1.2620) | | -------------------------------------------------------------------------------
Subtask 57-52-00-220-067
 C. Dimensions of the Joint that Connects the Flap to the Flap Carriage
 (Track 2).

 (1) Do a check of the dimensions that follow:
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page A666 1201-299, 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | B | 39.975 | 39.991 | | | 39.945 | | | | OD 4 |(1.5738) |(1.5744) | | |(1.5726) | | | | | | | 0.009 | 0.050 | | | 0.110 | | | | | (0.0003)| (0.0019)| | |(0.0043)| | B | 40.000 | 40.025 | | | | 40.055 | | | ID 3 |(1.5748) |(1.5757) | | | |(1.5769) | | -------------------------------------------------------------------------------
 
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