Model: 35-10703-831

Aircraft Frame

Special Features:

Matl: clad sht; 0 temper; ht t4; opp -832

Properties:

Overall Length
8.000 inches
Overall Width
2.000 inches
Material Thickness
0.050 inches
Aircraft Location
Panel-engine wrap cowl, upper, assembly
Aircraft Mission Design Series
B-52h
Material
Aluminum alloy 2024
Material Specification
Qq-a-362 federal specification single material response
NSN
1560-01-152-1414
Part Number
35-10703-831
Description
Frame,aircraft
CAGE
81205

A principal transverse structural member of the fuselage, hull, nacelle, pod, and the like. It follows the periphery and provides shape and support by attachment to the longitudinal members or skin.

Part 35-10703-831 NSN 1560-01-152-1414

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
41024
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

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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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