710411

Aircraft Gas Turb Compressor Hub

NSN 2840-00-929-4378

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
N/A
UOM:
1 EA
NIIN:
009294378

Product Features

Original name hub, compressor rotor, turbine engine

Detail Specifications

Overall Length:
Between 16.500 inches and 16.570 inches
Diameter:
Between 18.740 inches and 18.760 inches
End Application:
Engine model tf33
Criticality Code Justification:
Agav
Engine Section Location:
Compressor
Material:
Nickel alloy
Material Specification:
Ams 5660 assn standard single material response
NSN:
2840-00-929-4378
Item Name:
Hub,compressor,aircraft Gas Turb
Cage Code:
50748

Manufacturer Part Numbers

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
710411
Cage Code:
77445
RNCC:
3
RNVC:
2
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
530082
Cage Code:
77445
RNCC:
5
RNVC:
2
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
710411
Cage Code:
50381
RNCC:
5
RNVC:
2
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
822623
Cage Code:
77445
RNCC:
5
RNVC:
2
RNAAC:
ZZ
Status:
A
MSDS:
SADC:

Part Identification

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50573
FIIG:
A10700
Concept No.:
App. Key:
G
Cond. Code:
1
Status:
A

Part Materials

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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
24.3 X 24.3 X 18.5
Paclk Weight:
50.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F009113075
SPI Rev.:
C
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
197339
UFC:
96710
LTL:
65.0
LCL:
60.0
WCC:
593
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Pricing & Availability

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Privacy | Terms

Definition Definition of approved item name (AIN): "Aircraft Gas Turb Compressor Hub"

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.

MOE Major Organizational Entities

Entity
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
DSOR:
FT
Import / Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft


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