Model: 4321065

Aircraft Gas Diffuser Case Plug

Special Features:

Ap 8 (3 each) provides access between 9th-stage rotor, exit guide vanes, and diffuser; to hpt vanes, inside diameter (id) and outside diamter (od) of combustor; and gas generator (gg) fuel nozzles, and lpt vanes

Properties:

End Application
F119-pw-100 engine on f-22 aircraft
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Plug assembly of--instrumentation boss (ap 8)
NSN
2840-01-484-5564
Part Number
4321065
Description
Plug,diffuser Case,aircraft Gas
CAGE
77445

A usually round item of various cross sections designed for temporary installation into a hole in a case, diffuser, aircraft gas turbine engine for the purpose of preventing air from escaping during engine operation. When removed, the hole is for inserting inspection probes, borescopes and the like. It may be grooved or tapered for installation and removal. It may include spacers, springs, rivets and the like.

Part 4321065 NSN 2840-01-484-5564

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52957
FIIG:
A525D0
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:
ESD:
MMAC:
RF
CRITL:
Y

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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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