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1560-01-148-7251

Aircraft Former

1560011487251 011487251 25-2600-17

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

1560-01-148-7251 FORMER,AIRCRAFT 1560011487251 011487251

Managed by United States
NSN Created on 9 Mar 1983
Data Last Changed
May 2023
NATO Update Count
4
NATO Data Quality
1560-01-148-7251 FORMER,AIRCRAFT 1560011487251 011487251 1/1
NSN 1560-01-148-7251 (Generic Image) 1/1

1560-01-148-7251 Stock and Availability Marketplace 1560-01-148-7251

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1560-01-148-7251 Related Documents Related Documents 1560-01-148-7251 1+ Documents (More...)

25-2600-17 A light, secondary structural member that does not completely partition various components
United States (US) 4. 1560-01-148-7251 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-148-7251 RQST Updated Every Day 1560-01-148-7251 RQST NE Restrictions

1560-01-148-7251 Demil Restrictions 1560-01-148-7251

DEMIL: Q | DEMILI: 3 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC:

1560-01-148-7251 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. 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.

1560-01-148-7251 HTS and ScheduleB Import and Export 1560-01-148-7251

1560-01-148-7251 End Users End Users 1560-01-148-7251

US Air Force (FXX5)
Effective Date:
1 Apr 1991

1560-01-148-7251 Manufacturers Approved Sources 1560-01-148-7251

1560-01-148-7251 Technical Data Datasheet 1560-01-148-7251

Characteristic
Specifications
FIIG
A11400
Material [MATT]
Aluminum Alloy 7075
Material Document And Classification [MDCL]
Qq-A-277 T6 Fed Spec Single Material Response
Aircraft Location [CZDJ]
Angle,Extruded,Rib No. 2 Installation-Inboard Strut
Special Features [FEAT]
Opposite 25-2600-18
End Item Identification [AGAV]
B-52

1560-01-148-7251 Management Data Management Data 1560-01-148-7251

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Apr 1995
Department of the Air Force (DF)
EA
Subscribe
1
Mar 1995
Department of the Air Force (DF)
EA
Subscribe
1

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1560-01-148-7251 Freight Data Freight Information 1560-01-148-7251

1560-01-148-7251 has freight characteristics.. 1560-01-148-7251 has a variance between NMFC and UFC when transported by rail and the description should be consulted.