Model: 206-011-251-1

Tip Support Assembly Weight

Properties:

General Description
Aluminum alloy qq-a-591 comp 380, dim., 4.790 in. Min, 4.830 in. Max lg3.010 in. Nom lg raised center section, 0.625 in. Nom high raised centersection, two holes 0.063 in. Diameter drilled thru, tap drilled 0.650 in. Deep, tapped w/0.250-28 unf class 3b threads 0.500 in. Deep, 1.638 and 2.738 in.From top w/1.100 in. Center to center distance, two no. 206-011-255-1 studstorqued into threaded holes per bps 4018 type x bell helicopter co, fourholes drilled through side of raised surface 0.250 in. From edge at 1.200 in.279.5 deg, 1.860 in., 82.5 deg, 2.350 in., 272 degrees 40 min, 3.080 in. And zero degfrom top to hold no. Ms124696 inserts
NSN
1615-00-376-0297
Part Number
206-011-251-1
Description
Weight,tip Support Assembly
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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
8.0 X 6.0 X 1.2
Paclk Weight:
0.3000lbs
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:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013120
UFC:
05380
LTL:
100.0
LCL:
100.0
WCC:
713
TCC:
Z
SHC:
9
ACC:
Construction Materials

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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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