Model: 8860180-A781002

Aircraft Gas Tur Compressor Disk

Special Features:

Was disk, axial compressor, turbineengine

Properties:

Overall Length
Between 4.038 inches and 4.066 inches
Diameter
Between 19.785 inches and 19.795 inches
End Application
Engine model tf33
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Titanium alloy disk
Material Specification
Pwa1215 assn standard single material response disk
NSN
2840-00-269-5146
Part Number
8860180-A781002
Description
Disk,compressor,aircraft Gas Tur
CAGE

An item having provisions on the outer periphery for attaching a designated number of blade, compressor, aircraft gas turbine engine. it also has provisions for attachment to a hub, compressor, aircraft gas turbine engine and/or a shaft, turbine, aircraft gas turbine engine.

Part 8860180-A781002 NSN 2840-00-269-5146

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50567
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:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
24.8 X 24.8 X 5.5
Paclk Weight:
87.0000lbs
Item Weight:
72.0000lbs
Item Dim:
019901990043
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F007821497
SPI Rev.:
A
SPC Mkg:
ZZ
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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