Premium Information is available for this item - Upgrade for $1 a day
6615-01-558-9694
Automatic Pilot Flight Controller
6615015589694 015589694 5050051-0
A controller designed to control an aircraft through an automatic pilot in pitch, yaw, roll and coordinated turns. View more Automatic Pilot Flight Controller
January 2023
3
Marketplace 6615-01-558-9694
Request a Quotation from participating marketplace vendors
Related Documents 6615-01-558-9694 1+ Documents (More...)
United States (US) 4. 6615-01-558-9694 Marketplace Restrictions Approved Sources Datasheet Management
/fsc-6615/us 6615-01-558-9694 Automatic Pilot Flight Controller 015589694 5050051-0 A controller designed
Restrictions 6615-01-558-9694
6615-01-558-9694 is a Automatic Pilot Flight Controller 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 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 6615-01-558-9694
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 6615-01-558-9694
- Spain (YB01)
- Effective Date:
- 1 Nov 2007
Approved Sources 6615-01-558-9694
- Part Number
- Manufacturer
- Status
- 5050051-0
- Manufacturer
- 27914 - Honeywell International Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 6615-01-558-9694
- Characteristic
- Specifications
- FIIG
- Specifications
- A31700
- End Item Identification [AGAV]
- C130, Hercules
- Part Name Assigned By Controlling Agency [CXCY]
- Control Proc, Auto Flight 27914
Similar Supply Items to 6615-01-558-9694
Freight Information 6615-01-558-9694
6615-01-558-9694 has freight characteristics.. 6615-01-558-9694 has a variance between NMFC and UFC when transported by rail and the description should be consulted.