Model: 9539M85G12

A Inner Augmentor Nozzle Section

Properties:

End Application
F110-ge, 129
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Flap, exhaust nozzle-primary
NSN
2840-01-616-1301
Part Number
9539M85G12
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 9539M85G12 NSN 2840-01-616-1301

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:
PR
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
6.3 X 6.3 X 15.5
Paclk Weight:
6.2000lbs
Item Weight:
5.0000lbs
Item Dim:
013000530030
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000003E08
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
573
TCC:
Z
SHC:
9
ACC:
Construction Materials

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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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