Model: 8860187-C719409

Aircraft Gas Tur Compressor Disk

Special Features:

Original name disk, axial compressor, turbine engine

Properties:

Overall Length
Between 1.354 inches and 1.365 inches
Diameter
Between 20.016 inches and 20.027 inches
End Application
Engine model tf33
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Titanium alloy disk
Material Specification
Ams4928 assn standard single material response disk
NSN
2840-00-268-4016
Part Number
8860187-C719409
Description
Disk,compressor,aircraft Gas Tur
CAGE
98748

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 8860187-C719409 NSN 2840-00-268-4016

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:
RV
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
24.4 X 24.4 X 3.4
Paclk Weight:
18.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F001763734
SPI Rev.:
D
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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