Model: 37D401329G007

Aircraft Gas Turbi Turbine Rotor

Properties:

End Application
J-85 aircraft engine
Design Type
Axial compressor
Criticality Code Justification
Apgf and czbj and agav
Engine Section Location
Turbine
Reference Data And Literature
T.O. 2j-j85-64
Fsc Application Data
C-135 aircraft series
NSN
2840-00-906-5303
Part Number
37D401329G007
Description
Rotor,turbine,aircraft Gas Turbi
CAGE
99207

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

Part 37D401329G007 NSN 2840-00-906-5303

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50591
FIIG:
A10700
Concept No.:
App. Key:
J
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:
19.0 X 19.0 X 9.5
Paclk Weight:
50.7000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F000754314
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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