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时间:2011-03-27 08:52来源:蓝天飞行翻译 作者:admin
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 (4) Aft fairing The aft fairing is a removable secondary structure composed of two sections : - a main fairing situated at the rear of the pylon box - a movable fairing underneath the flap.
 (5) Lower fairing The lower fairing is a removable secondary structure situated between the pylon box and the engine nozzle.
 (6) Pylon-to-nacelle junction

 

 Engine Pylon Description
 Figure 001
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 Engine Pylon Stations - Description
 Figure 002
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 B. Systems The pylon supports all the following systems related to the engine :
 (1)
 Electrical and hydraulic
 (Ref. Fig. 003)


 (2)
 Fire extinguishing/detection and air system
 (Ref. Fig. 004)


 (3)
 Fuel (Ref. Fig. 005) All pylon bottom surfaces adjacent to the nacelle are fire walls.


 C. Compartment (Ref. Fig. 005) For safety purposes the engine pylon is divided into 7 compartments, each houses a particular type of equipment
 -------------------------------------------------------------------------------| DESIGNATION | ZONE | SYSTEMS | |--------------------------------- |----------|-------------------------------| |Forward | A | Flammable Fluids (Fuel, | |Fairing | | Hydraulics) | | | B1 | Bleed Air (High And Low | | | | Temperatures) | | | B2 | Electrics | |----------------------------------|----------|-------------------------------| |Pylon Box | C | Hydraulics Without Couplings | | | | Extinguishers | |----------------------------------|----------|-------------------------------| |Rearward Secondary | D | Hydraulics | |Structure | | Limited electrics | |----------------------------------|----------|-------------------------------| |Lower Fairing | E | None | |----------------------------------|----------|-------------------------------| |Pylon to Wing | F | Fuel (No Couplings) | |Center Fillets | | Electrics | | | | Bleed Air (Low Temperature) | -------------------------------------------------------------------------------


 Electrical and Hydraulic Installation
 Figure 003
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 Fire Extinguishing/Detection and Air System Installation
 Figure 004

 

R Fuel System and System Segregation through Compartments Figure 005
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 D. Ventilation and Drainage (Ref. Fig. 006) Each compartment is separately ventilated, separately drained overboard. The air of each zone is renewed
 (1)
 Compartment A Air inlet through the edges of the removable panels (not sealed). Air exit and overboard drain at the trailing edge.

 (2)
 Compartment B1 Air bleed from precooler supply ducting. Air exit through louvers fitted with an overtemperature detector. Drain : unsealed structure.

 (3)
 Compartment B2
 Vent and drain : unsealed structure.


 (4)
 Compartment C Air intake incorporated in the access door located on the side of the pylon between RIBs 2 and 3.

 (5)
 Compartment D
 Vent and drain : unsealed structure.


 (6)
 Compartment E
 Vent and drain : unsealed structure.


 (7)
 Compartment F Vented with the wing vent system. Air exits through a hole in the secondary structure on the side of the pylon panel between RIBs 5 and 7. Air exit and overboard drain at the trailing edge.

 


 Ventilation and Drainage
 Figure 006
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 PYLONS - REMOVAL/INSTALLATION
_____________________________
 TASK 54-50-00-000-001
 Removal of the Pylons
 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.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 
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