Model: 105B5154P1

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
24.120 inches
Overall Length
Between 1.435 inches and 1.475 inches
Outside Diameter
25.900 inches
Mounting Hole Diameter
0.065 inches
Mounting Hole Quantity
1
End Application
Aircraft eng
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Stiffener-turb nozzle, stg1
Material
Steel
NSN
2840-00-972-6899
Part Number
105B5154P1
Description
Support,turbine Nozzle,aircraft
CAGE

A support used for a nozzle,turbine,aircraft gas turbine engine.

Part 105B5154P1 NSN 2840-00-972-6899

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
51909
FIIG:
A521B0
Concept No.:
1
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:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
270.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
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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