Model: 596901

Aircraft Compressor Disk And Hub

Special Features:

Do not use cadmium plated tools on material; was disk and hub, axial compressor, turbine engine

Properties:

Overall Length
Between 5.870 inches and 5.895 inches
Diameter
Between 8.035 inches and 8.045 inches
End Application
Aircraft eng tf-33
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Titanium alloy disk
Material
Titanium alloy hub
Material Specification
Ams4938 assn standard single material response disk
Material Specification
Ams4938 assn standard single material response hub
NSN
2840-00-871-5175
Part Number
596901
Description
Disk And Hub,compressor,aircraft
CAGE
77445

An item that consists of a disk, compressor, aircraft gas turbine engine and a hub, compressor, aircraft gas turbine engine.

Part 596901 NSN 2840-00-871-5175

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50561
FIIG:
A10700
Concept No.:
App. Key:
F
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:
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
12.5 X 12.5 X 14.5
Paclk Weight:
9.1000lbs
Item Weight:
6.1000lbs
Item Dim:
008000800060
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XA4
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

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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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