Model: 220263Y1

Turbine Engine Turbine Rotor Case

Special Features:

Steel ams 6412, stg 3, 20.278 min 20.281 max in. Dia, 1.951 min 1.973 max in. W, rockwell c32-36 hardness.

Properties:

End Application
Aircraft eng j-65
General Description
Steel ams 6412, stg 3, 20.278 min 20.281 max in. Dia, 1.951 min 1.973 max in. W, rockwell c32-36 hardness
NSN
2840-00-028-7411
Part Number
220263Y1
Description
Case,turbine Rotor,turbine Engine
CAGE
0AHP5

Inc 61679 cancelled/replaced by ,inc 50554, fiig a10700, app-key d ,inc 50553, fiig a10700, app-key d ,on 021513 ~(all except usa) a case designed to surround a turbine rotor,turbine engine. Excludes case and nozzle,turbine,turbine engine.

Part 220263Y1 NSN 2840-00-028-7411

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61679
FIIG:
A23900
Concept No.:
3
App. Key:
A
Cond. Code:
2
Status:
C

Material Classification

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