Model: 822666

Aircraft Gas Turb Compressor Hub

Properties:

Diameter
Between 4.870 inches and 4.890 inches
End Application
Tf33-p-7a aircraft engine
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Nickel alloy
Material Specification
Ams5660 assn standard single material response
Reference Data And Literature
2j-tf33-14 figure 19 index 5a
NSN
2840-01-471-7748
Part Number
822666
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 822666 NSN 2840-01-471-7748

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

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:
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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