F 『
E C F M E
E E
E 56-5B E
E E
C. Install the fuel nozzles (Ref. TASK 73-11-40-400-002).
5. Close-up
________ Subtask 72-42-00-410-076
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the thrust reverser doors: (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
(3) Remove the access platform(s). Subtask 72-42-00-440-059
B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-30-00-081-041).
Subtask 72-42-00-410-077
C. Close Access
(1) Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
(2) Remove the warning notice(s).
F 『 EEFF : ALL E Page 63272-42-00
E E Feb 01/04 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
TURBINE SECTION - DESCRIPTION AND OPERATION
___________________________________________
1. General
_______
The modules of the turbine are the high pressure turbine and the low
pressure turbine.
A. High pressure turbine module (Ref. Fig. 001) The HPT module consists of 1-stage nozzle and rotor. The nozzles are supported by the HPT case, the rotor is attached to the high pressure compressor rotor.
B. Low pressure turbine module (Ref. Fig. 002) The LPT module consists of 4-stage turbine, rotor, nozzles, stator case and rear frame. The rotor is connected to the fan. Surrounding the stator case is a clearance control manifold system.
F 『 EEFF : ALL E Page 172-50-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
High Pressure Turbine Section
Figure 001
F 『 EEFF : ALL E Page 272-50-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E TURBINE SECTION - REMOVAL/INSTALLATION
Low Pressure Turbine Rotor/Stator Assembly
Figure 002
F EEFF : ALL 『E 72-50-00 Page 3
E E Feb 01/98
E E
ECES E
F 『
E C F M E
E E
E 56-5B E
E E
______________________________________
TASK 72-50-00-920-001
Remove and Discard Life Limited Parts of the High Pressure Turbine and Low
Pressure Turbine
1. Reason for the Job
__________________
Refer to the MPD TASK: 725000-C2
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
71-00-00-000-042 Removal of the Power Plant
71-00-00-400-042 Installation of the Power Plant
ESM 05-11-03
ESM 05-11-04
ESM 72-00-52
ESM 72-00-54
3. Job Set-up
__________
Subtask 72-50-00-010-051
A. Remove the engine (Ref. TASK 71-00-00-000-042).
4. Procedure
_________
Subtask 72-50-00-020-051
A. Remove and discard life limited parts of the high pressure turbine (Ref. ESM 72-00-52) and the low pressure turbine and (Ref. ESM 72-00-54).
NOTE : (Ref. ESM 05-11-03) and (Ref. ESM 05-11-04) for time limits.
____
5. Close-up
________
Subtask 72-50-00-410-051
A. Install the engine (Ref. TASK 71-00-00-400-042).
F 『 EEFF : ALL E Page 40172-50-00
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
HPT NOZZLE ASSEMBLY - DESCRIPTION AND OPERATION
_______________________________________________
1. General
_______ (Ref. Fig. 001, 002) The high pressure turbine (HPT) nozzle is a single-stage air cooled assembly that mounts in the combustion case and directs the gas flow from the combustion chamber onto the blades of the HPT rotor at the optimum angle. The major parts of the nozzle are 21 nozzle segments and inner support. The aft support and seal assembly, while not integral components of the HPT nozzle module are included since they attach to the HPT stator parts. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM ENGINE 发动机 2(50)
