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1560-00-025-5369

Aircraft Hinge

1560000255369 000255369 175795

An item attached to the aircraft structure, flight controls, and the like to permit a rotating, pivoting motion between two or more parts. Includes provisions for a pin or pins, bushings, bearings, and the like in which pivoting motion occurs. See also HINGE (1), DOOR, AIRCRAFT. View more Aircraft Hinge

1560-00-025-5369 HINGE,AIRCRAFT 1560000255369 000255369

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
16
NATO Data Quality
1560-00-025-5369 HINGE,AIRCRAFT 1560000255369 000255369 1/1
NSN 1560-00-025-5369 (Generic Image) 1/1

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1560-00-025-5369 Related Documents Related Documents 1560-00-025-5369 5+ Documents (More...)

175795 An item attached to the aircraft structure, flight controls, and the like to permit a rotating
United States (US) 4. 1560-00-025-5369 Marketplace Restrictions Approved Sources Datasheet Management
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1560-00-025-5369 Demil Restrictions 1560-00-025-5369

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: P | PMIC: U | EDC: | ADPEC:

1560-00-025-5369 is a Aircraft Hinge that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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. The precious metals content of this item is unknown.

1560-00-025-5369 HTS and ScheduleB Import and Export 1560-00-025-5369

1560-00-025-5369 End Users End Users 1560-00-025-5369

Canada (ZC01)
Effective Date:
1 Apr 1991
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
Portugal (ZP01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991
Turkey (ZW01)
Effective Date:
1 Dec 1995

1560-00-025-5369 Manufacturers Approved Sources 1560-00-025-5369

1560-00-025-5369 Technical Data Datasheet 1560-00-025-5369

Characteristic
Specifications
FIIG
A11800
Aircraft Location [CZDJ]
Flap,Stabilizer
Aircraft Mission Design Series [CZEK]
T-33
Material Document And Classification [MDCL]
Mil-S-6050 Mil Spec Single Material Response
Material [MATT]
Steel
Overall Length [ABHP]
4.150 Inches Nominal
Overall Width [ABMK]
1.500 Inches Nominal

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1560-00-025-5369 Freight Data Freight Information 1560-00-025-5369

1560-00-025-5369 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 095190. A Sub NMFC of Z. It has a NMFC Description of HARDWARE, NOI. 1560-00-025-5369 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 1560-00-025-5369 is rated as class 70 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 49790 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 713 for ocean manifesting and military sealift. 1560-00-025-5369 is not classified as a special type of cargo when transported by water. 1560-00-025-5369 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.