Model: 2-141-069-14

A Turbine Nozzle Assembly Spacer

Special Features:

0.330 inch flange on one end; opposite end of spacer is at a 66 degree angle

Properties:

Inside Diameter
Between 18.396 inches and 18.402 inches
Overall Length
4.050 inches
Outside Diameter
19.955 inches
End Application
2840-01-458-5361; t55 turboshaft engine
Part Name Assigned By Controlling Agency
Flange, fourth turbine nozzle, rear, pre-maching
Material
Stainless steel
NSN
2840-01-475-2794
Part Number
2-141-069-14
Description
Spacer,turbine Nozzle Assembly,a
CAGE
99193

A rigid item designed to maintain a predetermined space between two nozzle assembly, turbine, aircraft gas turbine engine. It may be a complete 360 degrees or a section thereof.

Part 2-141-069-14 NSN 2840-01-475-2794

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52430
FIIG:
A522X0
Concept No.:
App. Key:
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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
5.1 X 21.0 X 21.0
Paclk Weight:
56.0000lbs
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:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
120800
UFC:
61410
LTL:
RATING VARIABLE
LCL:
--
WCC:
590
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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