Model: 4067613

Aircraf Compressor Vane Assembly

Properties:

Diameter
19.073 inches
End Application
F100-pw-220 turbofan gas turbine engine
Part Name Assigned By Controlling Agency
Compressor 13th stage stator-exit vane assembly
Engine Section Location
Diffuser
Material
Titanium alloy vane
Reference Data And Literature
T.O.2j-f100-24, figure 137
NSN
2840-01-205-8481
Part Number
4067613
Description
Vane Assembly,compressor,aircraf
CAGE
77445

A stationary item designed for the purpose of directing air at the proper angle and velocity from a rotor, compressor, aircraft gas turbine engine. It has provisions for attaching to a case, compressor, aircraft gas turbine engine. It may have an inner support shroud. The assembled item forms a complete circle.

Part 4067613 NSN 2840-01-205-8481

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50607
FIIG:
A10700
Concept No.:
App. Key:
L
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:
NZ
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
23.4 X 23.4 X 3.4
Paclk Weight:
8.0000lbs
Item Weight:
4.5000lbs
Item Dim:
019401940014
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
095190
UFC:
49790
LTL:
70.0
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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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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