Model: 4054752CLE

Aircraft Turbine Nozzle Segment

Special Features:

T.O. 2j-f100-14, fig 153, ind 22; 2.412-2.432 sq. In. Area; 1800 cycle; turbine disk and hub; supersedes p/n 4051852cle

Properties:

Overall Length
Between 2.258 inches and 2.282 inches
End Application
Aircraft eng f100
Design Type
Axial compressor
Part Name Assigned By Controlling Agency
Original name vane, compressor, aircraft gas turbine engine
Engine Section Location
Turbine
Stage Number
2
Material
Steel
NSN
2840-01-120-1949
Part Number
4054752CLE
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 4054752CLE NSN 2840-01-120-1949

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
140.0000lbs
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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