2. Description
___________
 A. HPT shroud and stage 1 LPT nozzle assembly The HPT shroud and stage 1 LPT nozzle assembly consists of the shroud/nozzle support and HPT shrouds, and the stage 1 nozzles, inner air seal, and stationary air seal.
 (1) The shroud/nozzle support forms the outer shell of the assembly and provides an air space or manifold area between the outer shell and the combustion case. High pressure compressor (HPC) bleed air is introduced into the manifold area to provide cooling for the HPT shrouds and the LPT nozzles.

 (2) The HPT shrouds have a smooth abrasive rub surface that is tolerant to localized blade tip rubs and has good resistance to erosion from hot exhaust gases. The shrouds are held in place on the support by retainers and are individually replaceable.

 F 『 EEFF : ALL E Page 172-53-00
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E

 HPT Shroud and Stage 1 LPT Nozzle Assembly
 Figure 001
 F EEFF :  ALL  『E 72-53-00 Page 2 
E  E  Feb 01/98
 E  E
 ECES  E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 (3) The assembly has 28 LPT nozzle segments, each having 3 vanes. The nozzle segments are installed in the shroud/nozzle support and are held in place on the nozzle inner air seal by the stationary air seal which is bolted on the aft face of the inner air seal. The assembly is bolted between the LPT case forward flange and the combustion case aft flange. Borescope ports at 5.30 and 8.30 o'clock positions (ALF) are provided in the support to allow inspection of the nozzle area.
 F 『 EEFF : ALL E Page 372-53-00
 E E Feb 01/98 E E ECES E

 F  『
 E  C F M  E
 E  E

 E 56-5B E E E HPT SHROUD AND STAGE 1 LPT NOZZLE ASSEMBLY - INSPECTION/CHECK

_____________________________________________________________
 TASK 72-53-00-290-003
 Borescope/Inspection of the Stage 1 Low-Pressure Turbine Nozzle Assembly
 1. Reason for the Job
__________________
R Inspection of the low pressure turbine (LPT) nozzle is limited to the areas R that can be seen with a rigid borescope. Insert the borescope through the R borescope ports located on stage 1 LPT nozzle support. If no defects are R found then the borescope inspection is complete. If defects are found then R look at the high-pressure turbine (HPT) shrouds.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific access platform 1 m (3 ft. 3 in.)
 No specific Torque Wrench : range 36.00 to 220.00 lbf.in

 (0.40 to 2.60 m.daN)
 856A1320 1 BORESCOPE KIT
 856A1322 1 BORESCOPE - LIGHT SOURCE SET
 856A1323 1 MONITOR, RESOLUTION BORESCOPE

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2101 USA MIL-T-5544 graphite grease (Ref. 70-30-00) Material No. CP2619 * Never Seez-Pure Nickel, Special (Ref. 70-30-00) Material No. CP8001 * lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00) Material No. CP8002 * lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00)
 F 『 EEFF : ALL E Page 60172-53-00
 E E Nov 01/02 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E
 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 72-00-00-200-025 Over-Serviceable-Limit Extensions 72-53-00-290-004 Borescope/Inspection of the High-Pressure Turbine
 Shroud 78-30-00-081-041 Make the Thrust Reverser Serviceable after Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
 Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors NDTM 72-00-00 72-53-00-991-300 Fig. 601 72-53-00-991-301 Fig. 602
 3. Job Set-up
__________
 Subtask 72-53-00-941-052
 A. Safety Precautions
 (1) On the center pedestal, on the ENG panel 115VU:
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM ENGINE 發動機 2(73)