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时间:2011-03-27 08:47来源:蓝天飞行翻译 作者:admin
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 53-35-11-991-019 Fig. 412 **ON A/C ALL R Post SB 27-1117 For A/C 001-001,051-052,
 53-35-11-991-019-A Fig. 412A
 53-35-11-991-020 Fig. 413
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 53-35-11-010-050

 A. Get Access
 (1) Open the MLG doors (Ref. TASK 32-12-00-010-001). 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.
 (2)
 Put the warning notice in position to tell persons not to operate the flight controls.

 (3)
 Put the adjustable access platform in position.


 EFF : ALL
53-35-11Page 403


 Subtask 53-35-11-864-050
 B. Aircraft Maintenance Configuration
 (1)
 Extend the slats (Ref. TASK 27-80-00-866-004)

 (2)
 Depressurize the Green, the Yellow and the Blue hydraulic systems (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-00-864-003).


 Subtask 53-35-11-865-050
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 105VU ELEC/HOT BUS/702PP SPLY 5PB2 D02 105VU ELEC/HOT BUS/701PP SPLY 5PB1 D01 105VU ELEC/HOT BUS/702PP SPLY 12PB2 E02 105VU ELEC/HOT BUS/701PP SPLY 12PB1 E01 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 4. Procedure
_________
 **ON A/C 001-049, 051-099, 101-149, 201-299,
 (Ref. Fig. 401/TASK 53-35-11-991-001)
R **ON A/C 151-199, 401-499,
 (Ref. Fig. 401A/TASK 53-35-11-991-001-A)
 **ON A/C 301-399,
 (Ref. Fig. 401B/TASK 53-35-11-991-001-B)
 EFF : ALL
53-35-11Page 404


 Fairings - Wing-to-Fuselage (LH) Figure 401/TASK 53-35-11-991-001 
R  EFF :  001-049, 051-099, 101-149, 201-299,  53-35-11 Page 405 May 01/05
 CES 

 

 Fairings - Wing-to-Fuselage (LH) Figure 401A/TASK 53-35-11-991-001-A 
R  EFF :  151-199, 401-499,  53-35-11 Page 406 Aug 01/05
 CES 

 

R R  Fairings - Wing-to-Fuselage (LH) Figure 401B/TASK 53-35-11-991-001-B 
R  EFF :  301-399,  53-35-11 Page 407 May 01/04
 CES 

 

 **ON A/C 001-049, 051-099, 101-149, 201-299,
 (Ref. Fig. 402/TASK 53-35-11-991-002) R **ON A/C 151-199, 401-499,
 (Ref. Fig. 402A/TASK 53-35-11-991-002-A)
 **ON A/C 301-399,

 (Ref. Fig. 402B/TASK 53-35-11-991-002-B)
 **ON A/C ALL

 (Ref. Fig. 403/TASK 53-35-11-991-003, 404/TASK 53-35-11-991-010, 405/TASK 53-35-11-991-011, 406/TASK 53-35-11-991-012)
 **ON A/C 301-399,
 (Ref. Fig. 407/TASK 53-35-11-991-013)
 **ON A/C ALL

 (Ref. Fig. 408/TASK 53-35-11-991-014, 409/TASK 53-35-11-991-015, 410/TASK 53-35-11-991-004)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 53-35-11-020-050
 A. Removal of the Root Fillet Fairing of the Fairing Panel 191BT (192BT) (Ref. Fig. 411/TASK 53-35-11-991-017)
 (1)
 Extend the slats (Ref. TASK 27-80-00-866-004).

 (2)
 Hold the root fillet fairing (1) and remove the screws (3) and the washers (2).

 (3)
 Remove the root fillet fairing (1).


 EFF : ALL
53-35-11Page 408


 Fairings - Wing-to-Fuselage (RH) Figure 402/TASK 53-35-11-991-002 
R  EFF :  001-049, 051-099, 101-149, 201-299,  53-35-11 Page 409 May 01/05
 CES 

 

 Fairings - Wing-to-Fuselage (RH) Figure 402A/TASK 53-35-11-991-002-A 
R  EFF :  151-199, 401-499,  53-35-11 Page 410 Aug 01/05
 CES 

 

R R  Fairings - Wing-to-Fuselage (RH) Figure 402B/TASK 53-35-11-991-002-B 
R  EFF :  301-399,  53-35-11 Page 411 May 01/04
 CES 

 

 Panel 191BT (192BT) Figure 403/TASK 53-35-11-991-003
R  EFF : CES  ALL  53-35-11 Page 412 May 01/04 
 
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