Model: 68R332005-2008

Aircraft Structural Plate

Properties:

Overall Length
12.060 inches
Overall Width
2.400 inches
Material Thickness
0.500 inches
Aircraft Location
Fuselage-empenage support beam, cover access-sill
Aircraft Mission Design Series
F-15
Material
Titanium alloy
Material Specification
Mil-t-9046, type 3, comp c, annealed military specification single material response
NSN
1560-01-325-4051
Part Number
68R332005-2008
Description
Plate,structural,aircraft
CAGE
76301

A flat or preformed item of metallic or nonmetallic material. It may vary in shape and its surface may be smooth and/or serrated. Its thickness is small in comparison to both its length and width. It is designed to be mounted upon a surface or between two surfaces. Its primary function is to strengthen, join, or separate aircraft structural parts. Excludes plate, mending; shim; and spacer, plate.

Part 68R332005-2008 NSN 1560-01-325-4051

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
31495
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:
FX
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013560
UFC:
05690
LTL:
60.0
LCL:
60.0
WCC:
576
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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