Model: 75A321274-2001

Aircraft Turbine Nozzle Retainer

Special Features:

Nha pn 75a321314; material stock 0.050 x 2.100 x 4.200

Properties:

End Application
Gr7/t10
Part Name Assigned By Controlling Agency
Retainer inlet eng bay cooling
Material
Aluminum alloy
Material Specification
Qq-a-250/13 cond 0 federal specification single material response
NSN
2840-01-483-5635
Part Number
75A321274-2001
Description
Retainer,turbine Nozzle,aircraft
CAGE
76301

An item specifically designed to position and/or restrain the movement of one or more nozzle, nozzle segment, or nozzle assembly, turbine, aircraft gas turbine engine. It may be the full 360 degrees required for one turbine stage or a segment thereof.

Part 75A321274-2001 NSN 2840-01-483-5635

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52405
FIIG:
A522S0
Concept No.:
App. Key:
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
A
ESD:
A
MMAC:
CRITL:
X

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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