Model: 638E259P6

Aircraft Gas Turbi Turbine Shaft

Properties:

Overall Length
Between 4.843 inches and 4.845 inches
Diameter
Between 8.461 inches and 8.469 inches
End Application
Aircraft eng
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Shaft stub, compressor rotor, front
Engine Section Location
Compressor
Material
Steel
NSN
2840-00-110-8019
Part Number
638E259P6
Description
Shaft,turbine,aircraft Gas Turbi
CAGE
07482

An item designed to transfer rotary motion from a rotary, turbine, aircraft gas turbine engine to a rotor, compressor, aircraft gas turbine engine and/or a rotor, fan, aircraft gas turbine engine. It may include the hub, turbine, aircraft gas turbine engine. It may include provisions for mounting bearings and/or seals.

Part 638E259P6 NSN 2840-00-110-8019

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50601
FIIG:
A10700
Concept No.:
App. Key:
K
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:
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
77.5
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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