Model: 759312

Aircraft Gas Tur Compressor Disk

Special Features:

Original name disk, axial compressor, turbine engine

Properties:

Overall Length
Between 1.160 inches and 1.170 inches
Diameter
Between 22.236 inches and 22.246 inches
End Application
Engine model j57
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Steel disk
Material Specification
Pwa749 assn standard single material response disk
Surface Treatment
Nickel disk and cadmium disk
Surface Treatment Specification
Ams2416-4 assn standard single treatment response disk
NSN
2840-00-286-2505
Part Number
759312
Description
Disk,compressor,aircraft Gas Tur
CAGE
77445

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 759312 NSN 2840-00-286-2505

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:
--
Paclk Weight:
3,500.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F000065306
SPI Rev.:
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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