Model: 6877092

Aircraft Gas Turbi Turbine Rotor

Special Features:

Cres ems73648-2, fscm 73342, 48 blades, 6.409 in. Min, 6.411 in. Maxod, external spline located on hub end, 17 teeth, 0.557 in. Min, 0.562 in.Max od, 0.5313 in. Nom pitch dia, 30 degrees pressure angle, 0.8438-32 unjsexternal thd located 1.112 in.Min, 1.132 in. Max distance from hub end, 0.210 in. Nom thd lg

Properties:

End Application
T-63 series engines
NSN
2840-00-217-6691
Part Number
6877092
Description
Rotor,turbine,aircraft Gas Turbi
CAGE
73342

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

Part 6877092 NSN 2840-00-217-6691

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50591
FIIG:
A10700
Concept No.:
App. Key:
J
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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
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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