Model: 205-011-707-1

Retainer Assembly Plate

Properties:

General Description
Aluminum alloy qq-a-250/4 comp 2024-t351, anodized per bps 4001 bellhelicopter co, dim., isosceles triangle shaped retainer 3.680 in. Nom highw/base 3.800 in. Nom w, 0.290 in. Thick, aperture center 1.150 in. From base1.494 in. Min, 1.496 in. Max dia, 2.040 in. Min, 2.042 in. Max diameter counterboreon left side by 0.122 in. Min, 0.128 in. Max deep, one bushing hole 0.3750 in.Nom diameter located on vertical centerline 2.150 in. From base, bushing p/n23-006-15-17-16 fscm 97499 inserted into hole, bushing id 0.2500 in. Nom, twomounting holes 0.283 in. Nom diameter located 0.525 in. From base and 1.150 in.Either side of vertical centerline, one mounting hole 0.283 in. Diameter located2.400 in. From base on verticae centerline, base ends chamfered 0.700 in.High by 0.750 in. W, apex flattened to 0.500 in. W, max surface finish, id andcounterbore 63 microinches aa, all other surfaces 125 microinches aa
NSN
1615-00-438-2049
Part Number
205-011-707-1
Description
Plate,retainer Assembly
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:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
92.5
WCC:
671
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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