Model: 723688-102

Aircraft Combustion Chamber Case

Properties:

Overall Length
8.300 inches
Diameter
Between 17.000 inches and 17.100 inches
End Application
Aircraft eng j69-t-25a
Criticality Code Justification
Agav
Engine Section Location
Combustion chamber
Material
Nickel alloy
NSN
2840-01-192-2385
Part Number
723688-102
Description
Case,combustion Chamber,aircraft
CAGE
03104

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

Part 723688-102 NSN 2840-01-192-2385

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50545
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:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
22.5 X 22.5 X 12.5
Paclk Weight:
15.0000lbs
Item Weight:
12.0000lbs
Item Dim:
017001700084
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000001D66
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
029780
UFC:
14570
LTL:
300.0
LCL:
--
WCC:
692
TCC:
Z
SHC:
Z
ACC:
Trailers/Vehicles

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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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