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2510-01-550-6147
Vehicular Structural Frame
2510015506147 015506147 H-7M2-10
A rigid metallic structure designed to accommodate an appropriate vehicular chassis, body or equipment. View more Vehicular Structural Frame
January 2023
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Related Documents 2510-01-550-6147 1+ Documents (More...)
Vehicular Structural Frame 2510015506147 H-7M2-10 A rigid metallic structure designed to accommodate
Day 2510-01-550-6147 RQST NE Restrictions Restrictions 2510-01-550-6147 DEMIL: A | DEMILI : 1 | CRITICALITY
Restrictions 2510-01-550-6147
2510-01-550-6147 is a Vehicular Structural Frame 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2510-01-550-6147
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2510-01-550-6147
- Canada (ZC01)
- Effective Date:
- 1 Apr 2007
Approved Sources 2510-01-550-6147
- Part Number
- Manufacturer
- Status
- H-7M2-10
- Manufacturer
- 56833 - Brackett Aircraft Company, Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 2510-01-550-6147
- Characteristic
- Specifications
- FIIG
- Specifications
- A507S0
- Special Features [FEAT]
- Name Assigned By Manufacturer Upper Leg Assembly; Next Higher Assembly Model Ht-88 Military/Civilian Helicopter Tow Bar
NATO Stock Numbers Related to 2510-01-550-6147
Freight Information 2510-01-550-6147
2510-01-550-6147 has freight characteristics managed by the Department of the Air Force.. 2510-01-550-6147 has a variance between NMFC and UFC when transported by rail and the description should be consulted.