Model: 206-011-803-5

Tail Rotor Trunnion Assembly

Properties:

General Description
Aluminum alloy qq-a-225/6 comp 2024-t4 or comp 2024-t351, hard anodizebps fw4387, dim., 2.840 in. Min, 2.850 in. Max o/a lg, 1.400 in. Nom center spherical dia, 1.0015 in. Min, 1.0020 in. Max left and right end od, 0.500-13unc class 3b internal threads in. Left and right ends, ends counterbored 0.610 in. Diameter by 0.187 in. Deep, trunnion internal spline data, flat root.Slidingside fit, modified spline, 32 teeth, 32/64 diametral pitch, 30.0 degrees pressure angle, 0.9688 in. Min, 0.9700 in. Max minor dia, 1.0288 in. Min, 1.0328 in. Max major dia, 1.000 in. Pitch dia, one no. Rza11978 stud threaded into each arm end, one no. 206-011-807-1 liner installed on eaach arm od
NSN
1615-00-121-6392
Part Number
206-011-803-5
Description
Trunnion 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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
5.0 X 5.0 X 3.7
Paclk Weight:
0.4000lbs
Item Weight:
3.0000lbs
Item Dim:
003000300017
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

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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