Model: 576659

Turbine Engine Afterburner Band

Properties:

General Description
Stainless steel, ams 5508, rockwell c35-40 hardness, 40.246 in. Id, 40.380 in. Od, 0.980 in. W, 0.062 in. Thick, thirtyseven 0.110 in. Diameter holesequally spaced around od
Fsc Application Data
Aircraft jet engine, tf30
NSN
2840-00-929-9854
Part Number
576659
Description
Band,afterburner,turbine Engine
CAGE
77445

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:
PQ
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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