Model: 25-2371-26

Aircraft Structural Plate

Properties:

Overall Length
88.000 inches
Overall Width
43.000 inches
Material Thickness
0.020 inches
Side For Which Designed
Right side
Aircraft Location
Panel assembly on trailing edge, outborad strut
Aircraft Mission Design Series
B-52
Material
Aluminum alloy 2024
Material Specification
Qq-a-362 t3 federal specification single material response
NSN
1560-01-163-6801
Part Number
25-2371-26
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 25-2371-26 NSN 1560-01-163-6801

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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
106280
UFC:
54650
LTL:
50.0
LCL:
50.0
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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