Model: 111R668G02

Aircraft Combustion Chamber Duct

Properties:

Overall Length
Between 6.540 inches and 6.600 inches
End Application
J-85 aircraft engine
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
NSN
2840-00-834-7639
Part Number
111R668G02
Description
Duct,combustion Chamber,aircraft
CAGE
07482

A cylindrical shaped item or a segment thereof designed to direct air into or around a chamber, combustion, aircraft gas turbine engine. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes.

Part 111R668G02 NSN 2840-00-834-7639

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52524
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:
PL
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
36.0 X 36.0 X 7.5
Paclk Weight:
50.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F006903727
SPI Rev.:
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:
77.5
WCC:
671
TCC:
Z
SHC:
9
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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