Model: 702051CL5

Aircraft Gas Tur Compressor Vane

Special Features:

T.O. 2j-j60-4; 0.892-0.901 flow area; turbine nozzle, casc, oulet duct; made of colbalt alloy

Properties:

Overall Length
Between 2.614 inches and 2.663 inches
Overall Width
Between 1.104 inches and 1.124 inches
End Application
J60 aircraft engine
Blade Attachment Method
Pin
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
Stage Number
1
Material
Steel vane
Material Specification
Ams5385 assn standard single material response vane
NSN
2840-00-076-9779
Part Number
702051CL5
Description
Vane,compressor,aircraft Gas Tur
CAGE
77445

A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.

Part 702051CL5 NSN 2840-00-076-9779

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50611
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:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
6.3 X 6.3 X 10.5
Paclk Weight:
0.1000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XA1
SPI Rev.:
SPC Mkg:
00
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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