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4920-01-444-4181

Aircraft Composite Repair Mold

4920014444181 014444181 CTII-2535-MPC

A contoured fixture designed to facilitate the layup, forming, and curing of composite aircraft skin sections. View more Aircraft Composite Repair Mold

4920-01-444-4181 MOLD,COMPOSITE REPAIR,AIRCRAFT 4920014444181 014444181

Managed by United States
NSN Created on 6 May 1997
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
4920-01-444-4181 MOLD,COMPOSITE REPAIR,AIRCRAFT 4920014444181 014444181 1/1
NSN 4920-01-444-4181 (Generic Image) 1/1

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4920-01-444-4181 Related Documents Related Documents 4920-01-444-4181 5+ Documents (More...)

CTII-2535-MPC A contoured fixture designed to facilitate the layup, forming, and curing of composite
/fsc-4920/us 4920-01-444-4181 Aircraft Composite Repair Mold 4920014444181 CTII-2535-MPC A contoured
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4920-01-444-4181 Demil Restrictions 4920-01-444-4181

DEMIL: D | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

IUID Required

4920-01-444-4181 is a Aircraft Composite Repair Mold that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

4920-01-444-4181 End Users End Users 4920-01-444-4181

US Air Force (FGG4)
Effective Date:
1 May 1997

4920-01-444-4181 Manufacturers Approved Sources 4920-01-444-4181

4920-01-444-4181 Technical Data Datasheet 4920-01-444-4181

Characteristic
Specifications
FIIG
A23900
Material [MATT]
Epoxy/Fiberglass Composite & Steel
Overall Length [ABHP]
84.000 Inches Nominal
Overall Width [ABMK]
84.000 Inches Nominal
Overall Height [ABKW]
108.000 Inches Nominal
General Characteristics Item Description [TEXT]
Mold Is Layed Up With Quartz Material And Cured In An Autoclave;Manufactured From An Epoxy/Fiberglass Composite, Layed Up In The Oml Mold Using A Wax Sheet Offset
Special Features [FEAT]
1500Lbs
End Item Identification [AGAV]
Mc-130H
Functional Description [FTLD]
This Mold Is Required To Fabricate Replacement Component Pieces For Repair Of Damage To The Intermediate Skinin Class Iv Repairs; Used To Fabricatethe Complete Or Sections Of The Intermediate Skin
Reference Data And Literature [RDAL]
Serd No. 6119; To 35D8-7-4-1
Part Name Assigned By Controlling Agency [CXCY]
Intermediate Skin Mold

4920-01-444-4181 Management Data Management Data 4920-01-444-4181

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Dec 2019
Department of the Air Force (DF)
EA
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1

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4920-01-444-4181 Freight Data Freight Information 4920-01-444-4181

4920-01-444-4181 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133300. A Sub NMFC of Z. It has a NMFC Description of MACHINERY/MACHINES NOI. 4920-01-444-4181 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 4920-01-444-4181 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 4920-01-444-4181 is not classified as a special type of cargo when transported by water. 4920-01-444-4181 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.