Model: 206-011-802-1

Tail Rotor Yoke Assembly

Properties:

General Description
Aluminum alloy ams 4135 comp 2014-t6, surface treatment chemical film per bps fw4182, dim., 12.580 in. Mim, 129602 in. Max o/a lg, 2.240 in. Nom o/a w, 4.352 in. Nom o/a ht, 1.938 in. Nom w across tangs, 0.408 in. Nom tang outside w, 1.122 im. Nom tang inside w, 4.285 im. Nom inside tang depth, two holes in-line drilled through each tang 0.4995 in. Mim, 0.5000 in. Max diameter 0.800 and 2.800 im. From each end, eight no. 206-010-425-9 bushings inserted in tang holes w/flanges on tang inside, one hole 1-kl15 in. Mim, 1.5625 in. Max diameter drilled through yoke center parallel to tang holes
NSN
1615-00-121-6464
Part Number
206-011-802-1
Description
Yoke Assembly,tail 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:
U
ESD:
ESD:
MMAC:
CRITL:
F

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
572
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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