Model: 1385M97G06

Aircraft Gas Combustion Chamber

Special Features:

T.O. 2j-f110-4, figure 67, index 6; used on the combustion/diffuser nozzle, hpt shroud

Properties:

Overall Length
Between 7.392 inches and 7.527 inches
Diameter
30.141 inches
End Application
Aircraft eng f110
Engine Section Location
Combustion chamber
NSN
2840-01-388-9062
Part Number
1385M97G06
Description
Chamber,combustion,aircraft Gas
CAGE
07482

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 1385M97G06 NSN 2840-01-388-9062

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:
PR
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
45.0 X 38.0 X 14.5
Paclk Weight:
162.0000lbs
Item Weight:
62.5000lbs
Item Dim:
030503050080
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011465727
SPI Rev.:
D
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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