Model: 4055386

Aircraft Gas Combustion Chamber

Special Features:

F100 fracture critical part

Properties:

Overall Length
Between 12.110 inches and 12.210 inches
Diameter
Between 24.990 inches and 25.010 inches
End Application
Aircraft eng f100-pw-100
Criticality Code Justification
Feat
Engine Section Location
Combustion chamber
NSN
2840-01-088-7104
Part Number
4055386
Description
Chamber,combustion,aircraft Gas
CAGE
77445

The portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.

Part 4055386 NSN 2840-01-088-7104

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50337
FIIG:
A530F0
Concept No.:
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:
NZ
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
30.1 X 30.1 X 20.6
Paclk Weight:
103.0000lbs
Item Weight:
45.0000lbs
Item Dim:
026502650130
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011796905
SPI Rev.:
B
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
TCC:
2
SHC:
3
ACC:
Arms/Weapons

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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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