Model: 1465M50G08

A Inner Augmentor Nozzle Section

Special Features:

2j-f110-4, fig 2-78/2-73

Properties:

Overall Length
Between 22.090 inches and 22.170 inches
End Application
F110ge129 aircraft engine
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Flap, exhaust nozzle-divergent
Material
Steel
NSN
2840-01-381-5393
Part Number
1465M50G08
Description
Augmentor Nozzle Section,inner,a
CAGE
07482

A rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.

Part 1465M50G08 NSN 2840-01-381-5393

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
53241
FIIG:
A526N0
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:
Y

Freight Classification

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