Model: 109R556G25

Turbine Engine Afterburner

Special Features:

Components include 1 nozzle, 1 duct, 4 acuators, 4 blankets, 2 manifolds, 3 shafts, 5 tubes, 1 spacer

Properties:

End Application
Engine model j79
NSN
2840-00-133-5089
Part Number
109R556G25
Description
Afterburner,turbine Engine
CAGE
07482

A chamber in which additional fuel is injected into, the exhaust gases, and reheating the gases to develop increased thrust. It consists of combustion area, flame holders, injection nozzles and an exhaust ejector.

Part 109R556G25 NSN 2840-00-133-5089

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60031
FIIG:
A530F0
Concept No.:
App. Key:
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:
N

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
138.0 X 60.0 X 65.0
Paclk Weight:
2,337.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
8013210644
SPI Rev.:
SPC Mkg:
03
LVL_A:
F
LVL_B:
F

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:
Trailers/Vehicles

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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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