Model: SR11701A

Aircraft Seat Strut Assembly

Properties:

End Application
B-1b aircraft
General Description
Made from 4130 steel bar, mil-s-6758, condition f4, heat 125 ksi min; tube material 2024-t3 ww-t-700/3, wall thickness and outside diameter as indicated; length 12.63; rod assembly test tension load of 1500 pounds; a compression load of 460 pounds; instrutor seat aft station
Fsc Application Data
Seat, aircraft
NSN
1680-01-163-6724
Part Number
SR11701A
Description
Strut Assembly,aircraft Seat
CAGE
97393

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
EK
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8803300060
  • SITC: 79295
  • End Use: Parts for military-type goods
  • NAICS: 336413
  • USDA: 1

Freight Class: Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof)

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