Model: 204-011-737-5

Tail Rotor Trunnion Assembly

Properties:

General Description
Fsteel, ams6414 comp aisi 4340 body, cadmium-plated o/a except splines, steel inner race no. Ra42584 torrington, dim., 3.950 in. Min, 3.960 in. Max o/a lg, 1.630 in. Min, 1.700 in. Max center w, 0.9378 in. Min, 0.9382 in. Max left and right arm thickness, 1.845 in. Min, 1.855 in. Max left and right arm spherical radius, 1.150 in. Min, 1.160 in. Max left and right arm lg, 0.635 in. Diameter arm ends by 0.317 in. Lg, trunnion internal spline data, involute flat root spline, side bearing sliding class a fit, 40 teeth theoretical, 32/64 diametral pitch, 30.0 degrees pressure angle, 1.2500 in. Pitch dia, 1.2188 in. Min 1.2203 in. Min minor dia, 1.2915 in. Min, 1.2996 in. Max major dia, trunnion arms fitted w/torrington no. Ra24584 inner race
NSN
1615-00-132-4932
Part Number
204-011-737-5
Description
Trunnion Assembly,tail Rotor
CAGE

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:
X

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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