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时间:2011-02-24 09:55来源:蓝天飞行翻译 作者:admin
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 (8) Remove the ram-air outlet (6). R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 21-61-52-020-052-A
 A. Removal of the Ram-Air Outlet
 (Ref. Fig. 403A/TASK 21-61-52-991-007-A)

 (1)
 Remove the clamp (2) and disconnect the sleeve (1).

 (2)
 Remove the screws (6) and the washers (7).

 (3)
 Hold the ram-air outlet (5) and:


 (a) For the left ram-air outlet, 1 Remove the bolts (12), (13), (15), (16) and (18) and the
_
 washers (4).

 NOTE : Identify the bolts for use in the installation
____ procedure.
 (b) For the right ram-air outlet, 1 Remove the bolts (12), (14), (15), (17) and (18) and the
_
 washers (4).

 NOTE : Identify the bolts for use in the installation
____ procedure.
 (4)
 Put blanking plugs on the disconnected line ends.

 (5)
 Remove the ram-air outlet (5).

 


 INTENTIONALLY BLANK


R 1 1


21-61-52Page 429
1 1 Feb 01/05 1 1 1CES 1


 Ram Air Outlet
 Figure 403A/TASK 21-61-52-991-007-A12 (SHEET 1)

R 1EFF : 004-049, 055-099, 101-149, 151-199, 1 21-61-52Page 430 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Ram Air Outlet
 Figure 403A/TASK 21-61-52-991-007-A22 (SHEET 2)

R 1EFF : 004-049, 055-099, 101-149, 151-199, 1 21-61-52Page 431 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL


 TASK 21-61-52-400-003
 Installation of the Ram-Air Outlet
 WARNING : MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM
_______
 FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE.
 HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.

 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN
_______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 NOTE : The procedure is the same for the left ram-air outlet and the right
____
 ram-air outlet.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)

 

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
Material No. 08-004A USA MIL-A-46106 TYPE I
 ADHESIVE SEALANT (Ref. 20-31-00)
 Material No. 11-003 USA ASTM D 740
 METHYL-ETHYL-KETONE (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
12-33-21-618-001 Pre-conditioning through the HP Ground Connection 12-33-21-618-001 Pre-conditioning with the APU 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)-21-61-00-710-001 Operational Test of the Pack Temperature-Control System 21-61-51-400-001 Installation of the Air-Inlet Flap Actuator 8HH and
 28HH 21-61-52-000-001 Removal of the Air-Outlet Flap Actuator 9HH (29HH) 21-61-52-000-002 Removal of the Ram-Air Outlet Flap 21-61-52-400-002 Installation of the Ram-Air Outlet Flap 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure 53-35-13-400-002 Installation of the Quick-Release Access Panels on the Belly Fairing Structure
 **ON A/C 001-003, 051-054,
 21-61-52-991-007 Fig. 403
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 
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