Model: 9184M51G18

Turbine Case And Nozzle Assembly

Special Features:

Original name case and nozzle, turbine, turbine engine

Properties:

Overall Length
11.659 inches
Overall Width
Between 5.683 inches and 5.703 inches
Diameter
Between 95.930 inches and 95.950 inches
End Application
Aircraft end tf39
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Titanium alloy
NSN
2840-01-118-3602
Part Number
9184M51G18
Description
Case And Nozzle Assembly,turbine
CAGE
07482

A nozzle assembly, turbine, aircraft gas turbine engine with a case (3), turbine, aircraft gas turbine engine.

Part 9184M51G18 NSN 2840-01-118-3602

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50539
FIIG:
A10700
Concept No.:
App. Key:
C
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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
111.8 X 104.8 X 31.9
Paclk Weight:
1,363.0000lbs
Item Weight:
992.0000lbs
Item Dim:
098009800163
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011183602
SPI Rev.:
C
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:
2
SHC:
R
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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