Model: 206-010-195-1

Main Rotor Nut Lock

Properties:

General Description
Aluminum alloy qq-a-250/4 comp 2024-t4 or 2024-t3, anodized fw4001 bell helicopter co, dim., 1.100 in. Nom lg, 0.732 in. Min, 0.737 in. Max w, 0.190in. Nom thick, lower left and right corners cut at 45 degrees angle by 0.425 in. Lg, top center recessed 0.192 in. Min, 0.197 in. Max deep by 0.900 in. Min, 0.920 in. Max wide w/inside corners rounded by 0.125 in. Radius, one hole 0.265 in. Min, 0.270 in. Max diameter drilled through 0.250 in. From bottomand 0.550 in. From right side, one hole0.046 in. Min, 0.052 in. Max diameter drilled at 45 degrees angle to left side cut 0.120 in. From left edge and 0.200in. From top of cut
NSN
1615-00-121-6450
Part Number
206-010-195-1
Description
Lock,nut,main Rotor
CAGE

Material Classification

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
011790
UFC:
04720
LTL:
RATING VARIABLE
LCL:
--
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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