Model: 701608

Aircraft Gas Turbin Turbine Disk
Description:

Axial compressor design type, compressor engine section location, rockwell c35-40 hardness; 1.482-1.493 inch thickness; 19.825-19.835 inch od; 101 blade slots equally spaced around od; 16 0.4205-0.4235 inch holes equally spaced on 8 inch centerline radius; 16 0.437-0.440 inch holes equally spaced on 8.0 inch centerline radius .

Special Features:

Rockwell c35-40 hardness; 1.482-1.493 inch thickness; 19.825-19.835 inch od; 101 blade slots equally spaced around od; 16 0.4205-0.4235 inch holes equally spaced on 8 inch centerline radius; 16 0.437-0.440 inch holes equally spaced on 8.0 inch centerline radius

Properties:

Design Type
Axial compressor
Engine Section Location
Compressor
Material
Steel
Material Specification
Ams 6415 assn standard single material response
Fsc Application Data
Aircraft jet engine, j57
NSN
2840-00-006-2791
Part Number
701608
Description
Disk,turbine,aircraft Gas Turbin
CAGE
77445

An item having provisions on the outer periphery for attaching a designated number of blade, turbine rotor, aircraft gas turbine engine. It also has provisions for attachment to a hub, turbine, aircraft gas turbine engine.

Part 701608 NSN 2840-00-006-2791

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50571
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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
011790
UFC:
04720
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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