Model: 37E501086P118

Aircraft Gas Turbine Rotor Blade

Special Features:

0.251-0.253 in. Diameter of 1 hole

Properties:

Overall Length
4.510 inches
Overall Width
Between 1.238 inches and 1.242 inches
End Application
Aircraft eng j85
Design Type
Compressor
Part Name Assigned By Controlling Agency
Blade, turbine engine
Engine Section Location
Low pressure compressor
Stage Number
1
Material
Steel blade
Material Specification
B50t1130m mfr ref single material response blade
NSN
2840-01-089-2764
Part Number
37E501086P118
Description
Blade,turbine Rotor,aircraft Gas
CAGE
99207

An item mounted on a disk, turbine, aircraft gas turbine engine. it is designed to create the flow of air in the turbine section of an engine, gas turbine, aircraft.

Part 37E501086P118 NSN 2840-01-089-2764

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50535
FIIG:
A10700
Concept No.:
App. Key:
A
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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