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时间:2011-03-22 06:55来源:蓝天飞行翻译 作者:admin
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 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific container 1 l (0.2641 USgal)
 No specific access platform 4.0 m (13 ft. 1 in.)

 1EFF : ALL 1 28-25-41Page 422 1 1 May 01/05R 1 1 1CES 1


 B. Referenced Information -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------28-00-00-910-001 Fuel Safety Procedures

R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 28-25-41-991-007 Fig. 405
 **ON A/C 051-051,
 28-25-41-991-007-A Fig. 405A
 **ON A/C ALL
 3. Job Set-up
__________ R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 405/TASK 28-25-41-991-007)
 **ON A/C 051-051,

 (Ref. Fig. 405A/TASK 28-25-41-991-007-A)
 **ON A/C ALL

 Subtask 28-25-41-941-060
 A. Safety Precautions
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.

_______
 (1)
 You must obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you do work on the fuel system.

 (2)
 Put the safety barriers in position.


 1EFF : ALL 1 28-25-41Page 423 1 1 Aug 01/05 1 1 1CES 1


 Refuel/Defuel Coupling Element Assembly - Location and Detail
 Figure 405/TASK 28-25-41-991-007

R 1EFF : 001-049, 052-099, 101-149, 151-199, 1 28-25-41Page 424 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1R Refuel/Defuel Coupling Element Assembly - Location and Detail R Figure 405A/TASK 28-25-41-991-007-A


R 1EFF : 051-051, 1 28-25-41Page 425 1 1 May 01/05 1 1 1CES 1 Subtask 28-25-41-865-052


 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21

R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 28-25-41-010-060
 C. Get Access
 (1) Put the access platform below the refuel/defuel coupling 40QM.
 (2) Remove the access panel 622HB.
 **ON A/C 051-051,

 Subtask 28-25-41-010-060-A
 C. Get Access
 (1) Put the access platform below the applicable refuel/defuel coupling 100QM(40QM).
 (2) Remove the applicable access panel 522HB(622HB).
 **ON A/C ALL

 4. Procedure
_________ R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 405/TASK 28-25-41-991-007)
 **ON A/C 051-051,

 (Ref. Fig. 405A/TASK 28-25-41-991-007-A)
 1EFF : ALL 1 28-25-41Page 426 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL


 WARNING : DO NOT GET AIRCRAFT FUEL:
_______
 -
IN YOUR MOUTH

 -
IN YOUR EYES


 -ON YOUR SKIN FOR A LONG TIME.
 AIRCRAFT FUEL IS POISONOUS.


R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 28-25-41-020-058
 A. Removal of the Refuel/Defuel Coupling Element Assembly
 (1) If the check-valve in the element assembly is operational, continue as follows:
 (a)
 Open the access door 192MB.

 (b)
 On the refuel/defuel panel 800VU: 1 Lift the guard and put the MODE SELECT switch in the REFUEL


_
 position.

 2 Lift the guard and put the RIGHT REFUEL VALVES switch in the
_
 SHUT position.

 (c)
 Remove the coupling cap (8) from the coupling (1). NOTE : The coupling cap (8) will hang by the chain (9) from the

____
 shroud-ring (5).


 (d)
 Remove the bolt (7) that attaches the attachment tag (10) to the shroud-ring (5).


 NOTE : The attachment tag (10) will stay connected to the chain
____
 (9).

 (e)
 Remove the coupling cap (8) together with the chain (9).

 (f)
 Put a container below the coupling (1).
 
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