Model: 774659

Aircraft Gas Turb Compressor Hub

Special Features:

P/n will never be procured; p/n 635498 will be removed, if no cracks identified, will be reidentified to this p/n

Properties:

Overall Length
12.726 inches
Diameter
Between 16.741 inches and 16.743 inches
End Application
Tf-33 aircraft gas turbine eng
Design Type
Axial compressor
Criticality Code Justification
Abhp and abmz and czbj and feat
Engine Section Location
Compressor
Material
Steel
Material Specification
Ams6415 assn standard single material response
Reference Data And Literature
T.O. 2j-tf33-34, fig 6, ind 51
NSN
2840-01-458-2762
Part Number
774659
Description
Hub,compressor,aircraft Gas Turb
CAGE
77445

A component of a rotor, compressor, 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, compressor, aircraft gas turbine engine.

Part 774659 NSN 2840-01-458-2762

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50573
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:
RV
CRITL:
Y

Freight Classification

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