Model: 204-011-151-1

Main Rotor Bolt Assembly

Properties:

General Description
Steel, mil-s-5000 comp 4340 cond c1 bolt, cadmium-plated qq-p-416 type 2, class 1, aluminum alloy qq-a-225/6 comp 2024-t6 plug, dim., 10.450 in. Nom o/a lg, 3.210 in. Min, 3.211 in. Max left flange od, 0.250 in. Nom flange thickness, 2.4992 in. Min, 2.4999 in. Max bolt od, 1.240 in. Min, 1.255 in. Max w/across hexagon flats, 0.500 in. Nom hex head height, 0.875-14 unf 3b hex internal threads by 1.000 in. Lg, 2-12 un 2a right end external threads by 1.360 in. Lg, 2.000 in. Nom bolt id by 7.200 in. Lg, 1.5002 in. Right end id, plug for right end, 1.5012 in. O, 0.750 in. Lg, 0.120 in. Lg left end chamfer by 30.0 deg, used as bolt, blade, main rotor
NSN
1615-00-830-9736
Part Number
204-011-151-1
Description
Bolt Assembly,main 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:
GA
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
093470
UFC:
48940
LTL:
70.0
LCL:
70.0
WCC:
573
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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