Model: 2-23238-1

Aircraft Spar

Properties:

Overall Length
Between 4.9210 inches and 49.250 inches
Aircraft Mission Design Series
T-38
Material
Aluminum alloy 7075
Material Specification
Qq-a-200/11 t6 federal specification single material response
NSN
1560-00-139-0852
Part Number
2-23238-1
Description
Spar,aircraft
CAGE
0JRC1

A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil.

Part 2-23238-1 NSN 1560-00-139-0852

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
41028
FIIG:
A11400
Concept No.:
App. Key:
A
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:
P
PMIC:
A
ESD:
ESD:
MMAC:
XE
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
011760
UFC:
04705
LTL:
200.0
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8803909060
  • SITC: 79297
  • End Use: Parts for military-type goods
  • NAICS: 336419
  • USDA: 1

Freight Class: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)

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