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1560-01-528-7411
Aircraft Structural Component Fitting
1560015287411 015287411 5HA41223-108
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
May 2023
3
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RQST NE Restrictions 1560-01-528-7411 DEMIL: D | DEMILI : 7 | CRITICALITY : Y | HMIC : P | PMIC : A
Restrictions 1560-01-528-7411
1560-01-528-7411 is a Aircraft Structural Component Fitting that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. The DCMO has forced the Demilization requirements for this item as the ICP has not collaborated. 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 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.
Import and Export 1560-01-528-7411
- Schedule B
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- HTS Code
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End Users 1560-01-528-7411
- US Air Force (FLL5)
- Effective Date:
- 1 Mar 2005
Approved Sources 1560-01-528-7411
- Part Number
- Manufacturer
- Status
- 5HA41223-108
- Manufacturer
- 81755 - Lockheed Martin Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-528-7411
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- F-22 Raptor
- Aircraft Location [CZDJ]
- Fitting, Aft Idler Hinge,Main Weapons Bay Door
- Aircraft Mission Design Series [CZEK]
- F-22
- Material Thickness [ABPX]
- 3.500 Inches Nominal
- Material [MATT]
- Aluminum Alloy 2124
- Overall Length [ABHP]
- 24.000 Inches Nominal
- Overall Width [ABMK]
- 9.000 Inches Nominal
- Special Features [FEAT]
- Dim. Are Stock Material; Durability Critical System; C/O: -106 Hinge And Nas77a5-027 Bushings(4); M/F: 2124-T8151 Alum Plate
Management Data 1560-01-528-7411
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Freight Information 1560-01-528-7411
1560-01-528-7411 has freight characteristics.. 1560-01-528-7411 has a variance between NMFC and UFC when transported by rail and the description should be consulted.