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2840-01-579-7627
Aircraft Gas Turbine Engine Front Frame Strut
2840015797627 015797627 277D1250-505 A3312-3
A rigid piece designed to resist pressure in the direction of its length. It is positioned between the inner and outer rings and is a main component of a FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Front Frame Strut
November 2023
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Related Documents 2840-01-579-7627 5+ Documents (More...)
RQST NE Updated Every Day 2840-01-579-7627 RQST Updated Every Day 2840-01-579-7627 RQST NE Related Documents
RQST NE Updated Every Day 2840-01-579-7627 RQST Updated Every Day 2840-01-579-7627 RQST NE Related Documents
2840015797627 015797627,277D1250-505 Effective Date:1 Nov 2009 Approved Sources 2840 https//www.nsnlookup.com
28/fsc-2840/uk 2840-99-322-3506 2840993223506993223506 /www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-579-7627
2840015797627 015797627,277D1250-505 2840-01-599-3001 2840-01-579-7627 https//www.nsnlookup.com
Documents 2840-14-574-0019 5+ Documents ( More... ) https//www.nsnlookup.com 2840-01-599-3001 2840-01-579-7627
2840015797627 015797627,277D1250-505 2840-01-531-0230 531-0119 2840-01-531-0230 2840-01-465-7453
2840-99-322-3506 2840-14-574-0019 2840-01-599-3001 2840-01-579-7627 99-968-3697 014620839,9341M87G07
2840-99-968-3697 0839 2840014620839 465-7453 2840-99-322-3506 2840-14-574-0019 2840-01-599-3001 2840-01-579-7627
015993186,M155064 2840-01-599-3177 2840-01-599-3186 2840-01-599-3001 574-0019 2840-01-599-3001 2840-01-579-7627
Restrictions 2840-01-579-7627
2840-01-579-7627 is a Aircraft Gas Turbine Engine Front Frame Strut that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilization requirements of this item are currently unknown as insufficent technical data is available. 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 2840-01-579-7627
- Schedule B
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- HTS Code
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End Users 2840-01-579-7627
- Australia (ZA01)
- Effective Date:
- 1 Nov 2009
Approved Sources 2840-01-579-7627
- Part Number
- Manufacturer
- Status
- 277D1250-505
- Manufacturer
- 51563 - Rohr, Inc. (Active)
- Primary Buy
- Primary Buy
- A3312-3
- 08844 - Marathonnorco Aerospace, Inc. (Active)
- Secondary Buy
- Secondary Buy
Datasheet 2840-01-579-7627
- Characteristic
- Specifications
- FIIG
- Specifications
- A526P0
- Special Features [FEAT]
- Strut, Hold Open Rod
- End Item Identification [AGAV]
- Used On Ge Cf-680 Aircraft Turbofan Engine Housing
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Freight Information 2840-01-579-7627
2840-01-579-7627 has freight characteristics managed by Australia.. 2840-01-579-7627 has a variance between NMFC and UFC when transported by rail and the description should be consulted.