Model: 5104T40P01

Nonairc Component Mounting Plate

Special Features:

Having one hole centered on plate with a 0.395 to a 0.415 inch diameter; having four holes, one centered on each corner approximately 0.300 to 0.310 inches from edges, each with a 0.143 to a 0.146 inch diameter; having two holes offset from center at 29 degrees across length, 1.500 inches from center, each with a 0.330 to a 0.338 inch diamter

Properties:

Overall Length
Between 4.300 inches and 4.350 inches
Overall Width
Between 1.660 inches and 1.700 inches
Material Thickness
Between 0.091 inches and 0.109 inches
End Application
F/a18-e/f f414 ge-400 engine
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Plate, stiffening
Material
Titanium alloy
Material Specification
Ams 4911 assn standard single material response
NSN
2835-01-518-4528
Part Number
5104T40P01
Description
Plate,component Mounting,nonairc
CAGE
99207

A metallic item of various shapes designed to reduce vibration and to secure a component part of an engine gas turbine, nonaircraft to the engine case or housing as modified. for mounting accessories to the outside of the engine, see plate mounting.

Part 5104T40P01 NSN 2835-01-518-4528

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50355
FIIG:
A530F0
Concept No.:
App. Key:
Cond. Code:
1
Status:
A

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:
Y

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Schedule B and Export
  • Schedule B: 8411994000
  • SITC: 71499
  • End Use: Industrial engines
  • NAICS: 333611
  • USDA: 1

Freight Class: Parts of nonaircraft gas turbines

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