Model: 32-21109-68

Aircraft Spar

Properties:

Material
Titanium alloy
Material Specification
Ams 4911 assn standard single material response
NSN
1560-00-899-6072
Part Number
32-21109-68
Description
Spar,aircraft
CAGE
76301

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 32-21109-68 NSN 1560-00-899-6072

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:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013515
UFC:
05660
LTL:
60.0
LCL:
--
WCC:
571
TCC:
Z
SHC:
Z
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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