Model: 711311

Aircraft Gas Tu Compressor Blade

Special Features:

Original name blade, compressor rotor, turbine engine

Properties:

Overall Length
Between 3.072 inches and 3.081 inches
Overall Width
Between 1.212 inches and 1.222 inches
Material Thickness
Between 0.493 inches and 0.499 inches
End Application
Engine model j57
Design Type
Compressor
Hardness Rating
32.0 rockwell c blade and 38.0 rockwell c blade
Criticality Code Justification
Agav
Engine Section Location
Compressor
Material
Steel blade
Material Specification
Ams5616 assn standard single material response blade
NSN
2840-00-947-7114
Part Number
711311
Description
Blade,compressor,aircraft Gas Tu
CAGE
77445

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

Part 711311 NSN 2840-00-947-7114

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50531
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:
RV
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
50.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

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Phone: +1 470-231-0824
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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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