Model: 232-31074-9

Airframe Structural Panel

Properties:

End Application
Agm-86b
Criticality Code Justification
Text
Functional Description
Engine inlet panel on section 55 of missile body
Reference Data And Literature
T.O.21m-agm86-4-1 fig 22-18
General Description
Fits opposite -8 p/n; material is 0.125 thick 2024-0 per qq-a-250/5 sht clad; hardness critical item
NSN
1420-01-139-6617
Part Number
232-31074-9
Description
Panel,structural,airframe
CAGE

A preformed item which may be any shape, having a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose any portion of the fuselage or to fabricate partitions or compartments within a wing, empennage, fuselage or nacelle. It may have holes drilled or cut to accommodate items, but will have no items mounted on it, except bracket(s) or other facilities for its own mounting or support. It may be mounted by fasteners, bonding, or welding. Excludes cover, access; floor (1), aircraft; core material, cellular, structural; cover, access, guided missile; panel, structural, aircraft.

Part 232-31074-9 NSN 1420-01-139-6617

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
40936
FIIG:
A23900
Concept No.:
App. Key:
A
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:
GF
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Q
LVL_B:
Q

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
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  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 336415
  • USDA: 1

Freight Class: Parts for guided missiles

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