Model: 9526M12G01

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
Between 28.940 inches and 28.944 inches
Overall Length
Between 2.174 inches and 2.178 inches
Outside Diameter
Between 32.212 inches and 32.216 inches
Mounting Hole Diameter
Between 0.309 inches and 0.318 inches
Mounting Hole Quantity
79
End Application
Aircraft eng f110
Criticality Code Justification
Agav
Material
Steel
NSN
2840-01-171-2482
Part Number
9526M12G01
Description
Support,turbine Nozzle,aircraft
CAGE
07482

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

Part 9526M12G01 NSN 2840-01-171-2482

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:
39.0 X 39.0 X 3.5
Paclk Weight:
18.0000lbs
Item Weight:
10.0000lbs
Item Dim:
032303230025
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F013133364
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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