Model: 25-2321-823

Aircraft Structural Plate

Properties:

Overall Length
4.200 inches
Overall Width
1.500 inches
Material Thickness
0.063 inches
Aircraft Location
Fairing instl trailing edge inboard strut
Aircraft Mission Design Series
B-52
Material
Aluminum alloy 2024
Material Specification
Qq-a-362 t3 federal specification single material response
NSN
1560-01-150-7312
Part Number
25-2321-823
Description
Plate,structural,aircraft
CAGE
81205

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 25-2321-823 NSN 1560-01-150-7312

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:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
30.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

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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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