Model: 6841214

Aircraft Gas Tur Compressor Disk
Description:

2.494 inches overall length, 10.361 inches diameter, t56 eng end item identification, axial compressor design type, 32.0 rockwell c disk hardness rating.

Special Features:

T.O. 2j-t56-14; compressor rotor assembly

Properties:

Overall Length
Between 2.494 inches and 2.498 inches
Diameter
Between 10.361 inches and 10.371 inches
End Application
T56 eng
Design Type
Axial compressor
Hardness Rating
32.0 rockwell c disk and 38.0 rockwell c disk
Criticality Code Justification
Czcj
Engine Section Location
Compressor
Stage Number
4
Material
Steel disk
Material Specification
Ams5613 assn standard single material response disk
NSN
2840-00-011-0678
Part Number
6841214
Description
Disk,compressor,aircraft Gas Tur
CAGE
63005

An item having provisions on the outer periphery for attaching a designated number of blade, compressor, aircraft gas turbine engine. it also has provisions for attachment to a hub, compressor, aircraft gas turbine engine and/or a shaft, turbine, aircraft gas turbine engine.

Part 6841214 NSN 2840-00-011-0678

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50567
FIIG:
A10700
Concept No.:
App. Key:
G
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:
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:
LVL_A:
E
LVL_B:
Q

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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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