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1560-01-208-3210
Aircraft Structural Component Support
1560012083210 012083210 AND10134-1003 205-030-899-65S
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
January 2023
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205 https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-01-208-3210 Aircraft Structural Component
Support Account Upgrade 1560-01-208-3210Aircraft Structural Component Support1560012083210 012083210
Component Support -T3511 AND10134-1003 AMS10134-1003 https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540
/QQ-A-200/3-T3511 AND10134-1003 AMS10134-1003 LS10134-1003 QQ-A-200/3 9540PL0900340 AMS-QQ-A-200
AND10134-1003 ANGLE,STRUCTURAL 10 EA NS Request Quotation Updated Every Day 9540-01-261-6223 RQST NE
ANGLE,STRUCTURAL 10 EA NS Request Quotation /QQ-A-200/3-T3511 AND10134-1003 AMS10134-1003 LS10134
Aircraft Structural Component Support -T3511 AND10134-1003 AMS10134-1003 LS10134-1003 QQ-A-200/
3 9540PL0900340 9540PL1823575 https//www.nsnlookup.com AND10134-1003 /QQ-A-200/3-T3511 AND10134-1003
Quotation Subscribe to View Vendor Details... 1242517 ANGLE,STRUCTURAL 1 EA NS Request Quotation AND10134-1003
603 FT NS Request Quotation QQ-A200/11 ANGLE,STRUCTURAL 16 FT NS Request Quotation QQ-A-200/11 AND10134-1003
Restrictions 1560-01-208-3210
1560-01-208-3210 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 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. The precious metals content of this item is unknown.
Import and Export 1560-01-208-3210
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-208-3210
- Brazil (YA01)
- Effective Date:
- 1 Jul 2001
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Jul 2003
Approved Sources 1560-01-208-3210
- Part Number
- Manufacturer
- Status
- 205-030-899-65S
- Manufacturer
- 97499 - Bell Textron Inc (Active)
- Primary Buy
- Primary Buy
- AND10134-1003
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- 205-030-899-65S
- D0216 - General Atomics Aerotec Systems Gmbh (Active)
- Secondary Buy
- Secondary Buy
Datasheet 1560-01-208-3210
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- End Item Identification [AGAV]
- 1520-00-859-2670
- Nondefinitive Spec/Std Data [ZZZT]
- 2024 Alloy And 13.000In. Length And Aluminumalloy Material And 1003 Number And Angle Shape And 4 Temper
- Part Name Assigned By Controlling Agency [CXCY]
- Type/Model Designation:Uh-1D
- Special Features [FEAT]
- Aluminum Alloy 2024 Qq-A-250/5,T4; 0.063 In. Matl Thk; Base Flange 1.0000 In. Lg; Left Flange 0.750 In. Lg; 13.000 In. Lg O/A; L Cross Section; W/O Holes; Right Appl
- Supplementary Features [SUPP]
- Functional Description:Stiffener Fin Tail Boom
NATO Stock Numbers Related to 1560-01-208-3210
Freight Information 1560-01-208-3210
1560-01-208-3210 has freight characteristics managed by Germany.. 1560-01-208-3210 has a variance between NMFC and UFC when transported by rail and the description should be consulted.