(Ref. Fig. 402A/TASK 53-25-11-991-002-A)
 **ON A/C ALL

 (Ref. Fig. 403/TASK 53-25-11-991-003)
 (1)
 Hold the fairing you want to remove. Remove the screws (1) and the washers (2) and keep them.

 (2)
 Identify and mark the position of the screws (1).

 (3)
 Remove the panel.

 Fairing - Right Access Panels Figure 402/TASK 53-25-11-991-002 
R  EFF : 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,  53-25-11 Page 407 Aug 01/05
 CES 

 Fairing - Right Access Panels Figure 402A/TASK 53-25-11-991-002-A 
R  EFF :  301-399,  53-25-11 Page 408 Aug 01/05
 CES 

 Fairing-Wing to Fuselage - Typical Installation Figure 403/TASK 53-25-11-991-003
R  EFF : CES  ALL  53-25-11 Page 409 Aug 01/05 

 TASK 53-25-11-400-001
 Installation of the Wing-to-Fuselage Fairings (191AT, 191AB, 192AT, 192AB)

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  Torque Wrench : range 0.00 to 1.20 m.daN
 (0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 11-003  USA ASTM D 740
 METHYL-ETHYL-KETONE (Ref. 20-31-00)

 C. Referenced Information -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-80-00-866-004  Extending the Slats on the Ground
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 53-25-11-991-001 Fig. 401
 **ON A/C 301-399,

 53-25-11-991-001-A  Fig. 401A
 EFF : ALL
53-25-11Page 410

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 53-25-11-991-002 Fig. 402
 **ON A/C 301-399,
 53-25-11-991-002-A Fig. 402A
 **ON A/C ALL
 53-25-11-991-003 Fig. 403
 3. Job Set-up
__________
 Subtask 53-25-11-869-050

 A. Aircraft Maintenance Configuration
 (1) Make sure that the slats are extended (Ref. TASK 27-80-00-866-004).
 (2) Make sure that the access platform is in position.
 Subtask 53-25-11-865-051

 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR COND/RAM/AIR/INLET 1HZ D10 106VU CSM/G /EV/MAN/SPLY 6XE B04
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 21HH W22 122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC 23HH W21 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 3HH X21
 EFF : ALL
53-25-11Page 411

R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 24HH Y21 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20 
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302, 
R  122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC  4HH  Y19 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 
R  122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC  2HH  Y18 
R  **ON A/C 106-149, 303-399, 
R  122VU  4HH  Y19
 **ON A/C ALL
 Subtask 53-25-11-210-050
 C. Inspection of the Structure.
 (1) Examine the seals on the panels you removed. If necessary, replace them.
　
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