Model: 4059181CLL

Aircraft Turbine Nozzle Segment

Special Features:

T.O. 2j-f100-14, fig 155, ind 32; 1.730-1.749 sq. In. Area; 1800 cycle; turbine stator support; replaced by p/ns 4056781cll and 4070251cll

Properties:

End Application
Aircraft eng f100
Design Type
Axial compressor
Criticality Code Justification
Feat
Part Name Assigned By Controlling Agency
Original name vane, compressor, aircraft gas turbine engine
Engine Section Location
Turbine
Stage Number
1
NSN
2840-01-125-3847
Part Number
4059181CLL
Description
Nozzle Segment,turbine,aircraft
CAGE
77445

A portion of a nozzle assembly, turbine, aircraft gas turbine engine. it consists of two or more nozzle, turbine, aircraft gas turbine engine cast as one piece.

Part 4059181CLL NSN 2840-01-125-3847

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50583
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:
--
Paclk Weight:
150.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XC2
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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