Model: 406-010-432-101

Main Rotor Antidrive Link Assembly

Properties:

General Description
Steel, rockwell hardness rating b scale 79 min, triangular shape w/clevis legs on bottom and bearing on apex, dim., 6.600 in. C to c distance between clevis and bearing, 2.372 in. Min, 2.376 max inner clevis w, 0.428 in. Min, 0.438 in. Max leg thk, two no. 406-310-406-105 bushings installed in clevis ends, one no. 406-310-403-101 bearing installed in. Apex, item used on main rotor controls 58d aircraft
NSN
1615-01-171-3861
Part Number
406-010-432-101
Description
Link Assembly,antidrive,main Rotor
CAGE
97499

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:
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
1.1000lbs
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:
H

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
RATING VARIABLE
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8803100060
  • SITC: 79291
  • End Use: Parts for military-type goods
  • NAICS: 336413
  • USDA: 1

Freight Class: Propellers and rotors and parts thereof, for use in military aircraft

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