Model: 851641

Aircraft Compressor Disk And Hub

Special Features:

Used on the rotor front compressor

Properties:

Overall Height
6.500 inches
Diameter
15.000 inches
End Application
Tf33-pw-102/a & b aircraft gas turbine-fan engines
Design Type
Axial compressor
Part Name Assigned By Controlling Agency
Original name hub, compressor, aircraft gas turbine engine
Engine Section Location
Low pressure compressor
Stage Number
1
Material
Titanium alloy hub
Reference Data And Literature
T.O. 2j-tf33-34, fig 5, ind 1
NSN
2840-01-362-7057
Part Number
851641
Description
Disk And Hub,compressor,aircraft
CAGE
77445

An item that consists of a disk, compressor, aircraft gas turbine engine and a hub, compressor, aircraft gas turbine engine.

Part 851641 NSN 2840-01-362-7057

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50561
FIIG:
A10700
Concept No.:
App. Key:
F
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:
RV
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
25.1 X 25.1 X 10.8
Paclk Weight:
78.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F007757520
SPI Rev.:
C
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
77.5
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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