Model: 1441M68G12

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
Between 13.648 inches and 13.652 inches
Overall Length
7.464 inches
Outside Diameter
Between 22.590 inches and 22.610 inches
Mounting Hole Diameter
Between 0.419 inches and 0.430 inches
Mounting Hole Quantity
62
End Application
Aircraft eng f110ge129
Criticality Code Justification
Agav
Material
Steel
NSN
2840-01-308-7038
Part Number
1441M68G12
Description
Support,turbine Nozzle,aircraft
CAGE
07482

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

Part 1441M68G12 NSN 2840-01-308-7038

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:
A
ESD:
ESD:
MMAC:
PR
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
30.0 X 30.0 X 10.0
Paclk Weight:
30.0000lbs
Item Weight:
20.0000lbs
Item Dim:
023002300090
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011878176
SPI Rev.:
A
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
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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