Model: 9136M74G02

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
33.588 inches
Overall Length
5.630 inches
Outside Diameter
Between 38.913 inches and 38.923 inches
Mounting Hole Diameter
Between 0.295 inches and 0.305 inches
Mounting Hole Quantity
33
End Application
Engine, aircraft, turbofan, model tf39-ge1a
Criticality Code Justification
Agav
Material
Steel
NSN
2840-00-505-8387
Part Number
9136M74G02
Description
Support,turbine Nozzle,aircraft
CAGE
07482

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

Part 9136M74G02 NSN 2840-00-505-8387

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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
43.5 X 43.0 X 7.3
Paclk Weight:
63.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F005058387
SPI Rev.:
A
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
052460
UFC:
30360
LTL:
60.0
LCL:
60.0
WCC:
576
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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