Model: 701708

Aircraft Gas Tur Compressor Disk
Description:

1.482 inches overall length, 19.825 inches diameter, j57 aircraft engine end item identification, axial compressor design type.

Special Features:

10.995-11.005 in. Id.; 101 blade s lots eq sp around od; 16 0.420-0.423 holes eq sp on 8.000 in. C/l rad.; 16 0.433-0.440 in. Holes eq sp on 8.000 in. C/l rad.

Properties:

Overall Length
Between 1.482 inches and 1.493 inches
Diameter
Between 19.825 inches and 19.835 inches
End Application
J57 aircraft engine
Design Type
Axial compressor
Hardness Rating
35.0 rockwell c disk and 40.0 rockwell c disk
Engine Section Location
Compressor
Material
Steel disk
Material Specification
Ams6415 assn standard single material response disk
NSN
2840-00-006-5305
Part Number
701708
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 701708 NSN 2840-00-006-5305

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:
X

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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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