Model: 6037T83P04

Aircraft Gas Tu Compressor Rotor

Special Features:

Blades are dovetailed; matl specification inconel 718

Properties:

Overall Length
Between 5.246 inches and 5.257 inches
Diameter
Between 11.825 inches and 11.835 inches
End Application
Tf-34-100a aircraft engine
Design Type
Axial compressor
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Original name spool, compressor rotor
Engine Section Location
Compressor
Stage Number
10
Material
Nickel alloy
NSN
2840-01-436-7055
Part Number
6037T83P04
Description
Rotor,compressor,aircraft Gas Tu
CAGE
99207

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. it consists of disks, blades, hubs, and the like. it is the moving part of compressor, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

Part 6037T83P04 NSN 2840-01-436-7055

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50587
FIIG:
A10700
Concept No.:
App. Key:
J
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:
OP
CRITL:
F

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
135625
UFC:
68120
LTL:
65.0
LCL:
--
WCC:
718
TCC:
Z
SHC:
9
ACC:
Office Supplies

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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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