Model: 4-3908-8

Aircraft Spar

Special Features:

Heat treat t62 per ams 2270 or bac5602 stock size bac 1517-441 x 59.0

Properties:

Material Thickness
0.040 inches
End Application
B-52 aircraft
Side For Which Designed
Both sides
Part Name Assigned By Controlling Agency
Spar installation aft bomb door upper
Aircraft Mission Design Series
B52
Material
Aluminum alloy 7075
Material Specification
Ams-qq-a-250/13 assn standard single material response
NSN
1560-01-605-7129
Part Number
4-3908-8
Description
Spar,aircraft
CAGE
81205

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 4-3908-8 NSN 1560-01-605-7129

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:
A
ESD:
A
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
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:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
011760
UFC:
04705
LTL:
200.0
LCL:
--
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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