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时间:2011-02-24 09:37来源:蓝天飞行翻译 作者:admin
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 Subtask 21-26-53-941-052
 C. Get Access
 (1) Put the access platform in position on the right side of the aircraft, below the valve.
 4. Procedure
_________ (Ref. Fig. 401/TASK 21-26-53-991-001) Subtask 21-26-53-020-053
 A. Removal of the Skin Air Outlet-Valve
 (1)
 Remove the screws (3) and release the valve (2).

 (2)
 Disconnect the electrical connector (5).

 (3)
 Remove the valve (2) and discard the O-ring (4).

 (4)
 Remove the sealant from the valve (2) and the disconnected duct (1).

 (5)
 Clean the areas where sealant was applied with CLEANING AGENTS (Material No. 11-004).


R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 21-26-53Page 406 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 (6)
 Put blanking caps on the disconnected electrical connectors.

 (7)
 Put a blanking plug on the air outlet.


R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 21-26-53Page 407 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C ALL

 

 TASK 21-26-53-400-001
1. Reason for the Job
R Installation of the Skin Air Outlet-Valve (22HQ) __________________ Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  access platform 3.1 m (10 ft. 2 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 09-019  USA AMS 3267/3
 LOW ADHESION CORROSION INHIBITING SEALANT
 (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
O-ring  21-26-01 15 -030
R 1EFF : ALL 1 21-26-53Page 408 1 1 Feb 01/05 1 1 1CES 1


 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
21-26-00-710-001 Operational Check of System via MCDU 21-26-00-710-001 Operational Check of System via MCDU 24-42-00-861-001 Energize the Ground Service Network from the External
 Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 21-26-53-991-001 Fig. 401
 3. Job Set-up
__________
 CAUTION : USE ONLY THE GROUND SERVICE NETWORK TO SUPPLY ELECTRICITY BECAUSE
_______ THE AVIONICS VENTILATION SYSTEM IS NOT SERVICEABLE. IF YOU ENERGIZE THE AIRCRAFT ELECTRICAL CIRCUITS WITHOUT THE VENTILATION SYSTEM YOU WILL CAUSE DAMAGE TO ELECTRICAL EQUIPMENT.
 Subtask 21-26-53-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the ground service network is energized
 (Ref. TASK 24-42-00-861-001).


 (2)
 Make sure that the access platform is in position on the right side of the aircraft, below the valve.


 Subtask 21-26-53-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR COND/AVNCS VENT/CTL 6HQ D06
R 1EFF : ALL 1 21-26-53Page 409 1 1 Feb 01/05 1 1 1CES 1


 4. Procedure
_________ (Ref. Fig. 401/TASK 21-26-53-991-001) Subtask 21-26-53-420-051 R A. Installation of the Skin Air Outlet-Valve
 (1)
 Do an inspection of the component interface and/or the adjacent area.

 (2)
 Apply SEALANTS (Material No. 09-019) between the structure (1) and the valve (2).

 (3)
 Install the new O-ring (4) in the groove of the valve (2).

 (4)
 Install the valve (2).

 (5)
 Install the screws (3) and tighten. NOTE : You must do the bonding with the screw at the top and the

____ screw at the bottom (Ref. TASK 20-28-00-912-004).
 
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