Model: 4059312

Aircraft Gas Turbi Diffuser Case

Properties:

Overall Length
Between 17.818 inches and 17.822 inches
Diameter
Between 28.245 inches and 28.265 inches
End Application
F100-pw-100/200 aircraft gas turbine engine
Design Type
Axial compressor
Hardness Rating
36.0 rockwell c outer case
Part Name Assigned By Controlling Agency
Original name case, combustion chamber, aircraft gas turbine engine
Engine Section Location
Diffuser
NSN
2840-01-130-2407
Part Number
4059312
Description
Case,diffuser,aircraft Gas Turbi
CAGE
77445

A case that is an integral part of an engine, gas turbine, aircraft, designed to surround and protect a diffuser, aircraft gas turbine engine.

Part 4059312 NSN 2840-01-130-2407

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50549
FIIG:
A10700
Concept No.:
3
App. Key:
D
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:
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
38.2 X 38.2 X 29.7
Paclk Weight:
242.0000lbs
Item Weight:
130.0000lbs
Item Dim:
032003200210
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F013807752
SPI Rev.:
A
SPC Mkg:
ZZ
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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