Model: 1385M24P05-118

Aircraft Gas Turbine Turbine Hub

Special Features:

Same as p/n 1385m24p05 but only to be used on the f118 engine

Properties:

End Application
F118-ge-100 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Czbj and feat
Engine Section Location
High pressure turbine
Material
Nickel alloy
Material Specification
Inconel 718 mfr ref single material response
NSN
2840-01-443-4068
Part Number
1385M24P05-118
Description
Hub,turbine,aircraft Gas Turbine
CAGE
07482

A component of a rotor, turbine, aircraft gas turbine engine. it is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a shaft, turbine, aircraft gas turbine engine. it may have provisions for installing bearings, and/or oil and air seals. see also disk and hub, turbine, aircraft gas turbine engine.

Part 1385M24P05-118 NSN 2840-01-443-4068

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50577
FIIG:
A10700
Concept No.:
App. Key:
G
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:
JU
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
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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