Model: 68A332013-2004

Aircraft Stiffener Rib

Special Features:

Next higher assembly, 68a332001, u/o f-15a cum 1-blk 11, f-15b cum 1-blk 11, dim.Stock material

Properties:

Overall Length
7.600 inches
Overall Width
1.500 inches
Material Thickness
0.045 inches
Side For Which Designed
Right side
Aircraft Location
Former-fs837, aft closure beam
Aircraft Station Number
Fs837
Aircraft Mission Design Series
F-15a, b
Material
Titanium alloy
Material Specification
Mil-t-9046, type3, cmpsnc, anl military specification 1st material response
NSN
1560-01-467-4188
Part Number
68A332013-2004
Description
Rib,stiffener,aircraft
CAGE
76301

A vertical, relatively short, rib located in a fuselage, nacelle, pod, and the like. It follows the periphery and provides additional rigidity. It may join various components such as stringers, longerons, and the like. It is supplementary to the frames and blukheads. See also rib (1), airfoil.

Part 68A332013-2004 NSN 1560-01-467-4188

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
41027
FIIG:
A11400
Concept No.:
1
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

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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