Model: 9084M40P01

Aircraft Gas Turb Compressor Hub

Special Features:

Orig name hub, compressor frame

Properties:

Overall Length
Between 1.100 inches and 1.140 inches
Overall Width
Between 0.860 inches and 0.920 inches
Material Thickness
0.185 inches
End Application
Aircraft eng tf-39
Design Type
Compressor
Criticality Code Justification
Apgf and czbj and abhp and abmk and abpx
Engine Section Location
Compressor
Material
Steel hub
Material Specification
B50tf14, cl-a mfr ref 1st material response hub
NSN
2840-01-144-2473
Part Number
9084M40P01
Description
Hub,compressor,aircraft Gas Turb
CAGE
07482

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 9084M40P01 NSN 2840-01-144-2473

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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114990
UFC:
58952
LTL:
70.0
LCL:
--
WCC:
593
TCC:
Z
SHC:
Z
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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