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1560-01-241-8915

Aircraft Former

1560012418915 012418915 160D511108-43

A light, secondary structural member that does not completely partition various components such as the fuselage, boom, wing, and the like. It is designed to give cross-sectional shape and strength to the item of which it is a part. View more Aircraft Former

1560-01-241-8915 FORMER,AIRCRAFT 1560012418915 012418915

Managed by United States
NSN Created on 3 Oct 1986
Data Last Changed
August 2023
NATO Update Count
6
NATO Data Quality
1560-01-241-8915 FORMER,AIRCRAFT 1560012418915 012418915 1/1
NSN 1560-01-241-8915 (Generic Image) 1/1

1560-01-241-8915 Stock and Availability Marketplace 1560-01-241-8915

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1560-01-241-8915 Related Documents Related Documents 1560-01-241-8915 1+ Documents (More...)

United States (US) 4. 1560-01-241-8915 Marketplace Restrictions Approved Sources Datasheet Management
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RQST NE Updated Every Day 1560-01-241-8915 RQST Updated Every Day 1560-01-241-8915 RQST NE Restrictions

1560-01-241-8915 Demil Restrictions 1560-01-241-8915

DEMIL: Q | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC: 0

1560-01-241-8915 is a Aircraft Former that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a confirmed Commerce Control List Item (CCLI). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

1560-01-241-8915 HTS and ScheduleB Import and Export 1560-01-241-8915

1560-01-241-8915 End Users End Users 1560-01-241-8915

US Air Force (FUU5)
Effective Date:
1 Jun 2000
Former MOE Rule:
FAA5

1560-01-241-8915 Manufacturers Approved Sources 1560-01-241-8915

1560-01-241-8915 Technical Data Datasheet 1560-01-241-8915

Characteristic
Specifications
FIIG
A11400
Material [MATT]
Aluminum Alloy 7075
Material Document And Classification [MDCL]
Qq-A-250/13 Fed Spec Single Material Response
Aircraft Location [CZDJ]
Ventral Fin Assembly
Aircraft Mission Design Series [CZEK]
A-10A
Overall Length [ABHP]
14.000 Inches Nominal
Overall Width [ABMK]
11.000 Inches Nominal
Material Thickness [ABPX]
0.050 Inches Nominal

1560-01-241-8915 Management Data Management Data 1560-01-241-8915

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jul 2023
Department of the Air Force (DF)
EA
Subscribe
1
Jan 2023
Department of the Air Force (DF)
EA
Subscribe
1
Apr 2002
Department of the Air Force (DF)
EA
Subscribe
1
Jun 2000
Department of the Air Force (DF)
EA
Subscribe
1

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1560-01-241-8915 Freight Data Freight Information 1560-01-241-8915

1560-01-241-8915 has freight characteristics.. 1560-01-241-8915 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

1560-01-241-8915 Packaging Data Packaging Data 1560-01-241-8915

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
--

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
14.0" H x 6.8" W x 1.2" L
--
--
Over 10lb
Less than 85G
No Requirement

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
1
9.3" H x 6.3" W x 18.5" L
--
--
Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
--
--
--
ASTM-D5118, Type CF, Class Weather-Resistant, Corrugated Fiberboard Box
No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container
--
No Requirement