6068T36P04

Turbine Engine Cooling Plate

NSN 2840-01-612-0143

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
UOM:
NIIN:
016120143

Product Features

72-41-00 rotor assembly-stages 1 and 2 low stress gas generator turbine, plate stage 2 turbine aft cooling, this item has replaced 6068t36p01.

Technical Specifications of NSN

NSN:
2840-01-612-0143
Item Name:
Bypass Duct Plate Retaining Seal
Cage Code:
99204

Other Related Parts

No other part numbers with same form, fit, and function found.

Part Identification

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
42000
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
Status:
A

Part Materials

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

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Definition Definition of approved item name (AIN): "Bypass Duct Plate Retaining Seal"

An item of various cross sections used to exhaust heat from the gas generator turbine rotor of a turbine engine.

MOE Major Organizational Entities

Entity
DSOR
User:
SPAIN Spain
DSOR:
Import / Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

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


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