Model: 701604

Aircraft Gas Turbin Turbine Disk
Description:

Axial compressor design type, compressor engine section location, steel, ams 6415, rockwell c35-40 hardness, 2.028-2.039 in. Thk, 19.825-19.835 in. Od, 7.995-8.005 in. Id, 51 blade slots equally spacedaround od, sixteen 0.4205-0.4235 in. Holes equally spaced on 9.000 in.Centerline radius, sixteen 0.437-0.440 in. Holes equally spaced on 9.000in.Centerline radius .

Special Features:

Steel, ams 6415, rockwell c35-40 hardness, 2.028-2.039 in. Thk, 19.825-19.835 in. Od, 7.995-8.005 in. Id, 51 blade slots equally spacedaround od, sixteen 0.4205-0.4235 in. Holes equally spaced on 9.000 in.Centerline radius, sixteen 0.437-0.440 in. Holes equally spaced on 9.000in.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
2840-00-006-5309
Part Number
701604
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 701604 NSN 2840-00-006-5309

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:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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