Model: 723688-103

Aircraft Combustion Chamber Case

Special Features:

T.O. 2j-j69-44, fig 16; repl p/n 723688-102; contains swirl vane p/n 713163

Properties:

Overall Length
Between 7.450 inches and 7.520 inches
End Application
J69-t-25a aircraft gas turbine engine
Hardness Rating
36.0 rockwell c vane
Criticality Code Justification
Czbj and abhp and feat
Part Name Assigned By Controlling Agency
Original name shell assembly, complete outer combustor
Engine Section Location
Combustion chamber
Material
Nickel alloy
NSN
2840-01-448-5790
Part Number
723688-103
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 723688-103 NSN 2840-01-448-5790

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:
017001700083
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:
120780
UFC:
08134
LTL:
70.0
LCL:
--
WCC:
593
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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