Model: 6050T65G01

Tur Centrifugal Compressor Rotor

Special Features:

Stage 1 blade; stage 3 blade; stage 2 lever arm.

Properties:

End Application
2840-01-266-0346, engine, gas turbine
Functional Description
Hpc module
Reference Data And Literature
Ge ecp g404-c-42, page 11
General Description
Stage 1 blade; stage 3 blade; stage 2 lever arm
Type/model Designation
F404-ge-400
NSN
2840-01-266-0344
Part Number
6050T65G01
Description
Compressor Rotor,centrifugal,tur
CAGE
99207

Inc 60245 cancelled/replaced by ,inc 50588, fiig a10700, app-key j ,inc 50587, fiig a10700, app-key j ,on 021513 ~(all except usa). An item consisting of a series of blades on one or both sides of the rotor disk extending from the axis of rotation radially to the rim of the disk. It is designed to centrifugally cause the air between the blades to move outward to the rim of the compressor section of a turbine engine.

Part 6050T65G01 NSN 2840-01-266-0344

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60245
FIIG:
A23900
Concept No.:
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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