Model: 1559M63G04

Aircraft Compressor Disk And Hub

Special Features:

T.O 2j-f110-14, fig 67, ind 5; repl p/n 1559m63g02; hpcr stg 1-2 spool oil drain holes are enlarged 1.48 larger than the current elliptical holes to allow better drainage

Properties:

Overall Length
Between 6.425 inches and 6.455 inches
Diameter
Between 17.225 inches and 17.229 inches
End Application
F110-ge-129 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Abhp and abmz and feat
Part Name Assigned By Controlling Agency
Original name spool, compressor rotor
Engine Section Location
Compressor
Material
Titanium alloy
NSN
2840-01-447-2868
Part Number
1559M63G04
Description
Disk And Hub,compressor,aircraft
CAGE
07482

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

Part 1559M63G04 NSN 2840-01-447-2868

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:
PR
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
21.0 X 21.0 X 8.0
Paclk Weight:
45.0000lbs
Item Weight:
35.0000lbs
Item Dim:
015501550068
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F012326379
SPI Rev.:
B
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:
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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