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1560-00-518-2437
Aircraft Structural Component Support
1560005182437 005182437 52-42016-5
A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT; and RADIUS BLOCK. View more Aircraft Structural Component Support
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January 2023
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Related Documents 1560-00-518-2437 1+ Documents (More...)
United States (US) 4. 1560-00-518-2437 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-00-518-2437 RQST Updated Every Day 1560-00-518-2437 RQST NE Restrictions
Restrictions 1560-00-518-2437
1560-00-518-2437 is a Aircraft Structural Component Support 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 Item and must be mutilated to scrap. 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.
Import and Export 1560-00-518-2437
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-00-518-2437
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-00-518-2437
- Part Number
- Manufacturer
- Status
- 52-42016-5
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-00-518-2437
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- Mcdonnell P/N 53-42001-Series
- Relationship To Similar Equipment [RTSE]
- Similar To Mcdonnell Fitting P/N 53-42016-3
- Part Name Assigned By Controlling Agency [CXCY]
- Type/Model Designation:F-4F/Rf-4F/Gy/Phantom
- Special Features [FEAT]
- Steel Comp 4130,Mil-S-6758,Cond C; Cadmium Plated,Qq-P-416,Type 2,Class 2; Right Hand Angle Design; Baseflange 1.172 In. W By 1.547 In. Lg By 0.100 In. Thk; Left Side Flange 1.906 In. W By 1.760 In. Lg By 0.200 In. Thk; Surface Finish 125.0 Min Microinch; Heat Treated 180000 To 20000 Psi
- Supplementary Features [SUPP]
- Functional Description:Aft Hardpoint Fitting Inboard Strut Main Landing Gear Door
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Freight Information 1560-00-518-2437
1560-00-518-2437 has freight characteristics.. 1560-00-518-2437 has a variance between NMFC and UFC when transported by rail and the description should be consulted.