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1680-01-575-6251

Aircraft Seat

1680015756251 015756251 2158-1S1020DL

INC: 11554 Aircraft Seat

1680-01-575-6251 SEAT,AIRCRAFT 1680015756251 015756251

Managed by United States
NSN Created on 9 Jul 2009
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
1680-01-575-6251 SEAT,AIRCRAFT 1680015756251 015756251 1/1
NSN 1680-01-575-6251 (Generic Image) 1/1

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2158-1S1020DL Managed by United States NSN Created on 9 Jul 2009 Data Last Changed January 2023 NATO
Update Count 3 NATO Data Quality NSN 1680-01-575-6251 (Generic Image) 1/1 1.
RQST NE Updated Every Day 1680-01-575-6251 RQST Updated Every Day 1680-01-575-6251 RQST NE Restrictions

1680-01-575-6251 Demil Restrictions 1680-01-575-6251

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

1680-01-575-6251 is a Aircraft Seat 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.

1680-01-575-6251 HTS and ScheduleB Import and Export 1680-01-575-6251

1680-01-575-6251 End Users End Users 1680-01-575-6251

Australia (ZA01)
Effective Date:
1 Jul 2009

1680-01-575-6251 Manufacturers Approved Sources 1680-01-575-6251

1680-01-575-6251 Technical Data Datasheet 1680-01-575-6251

Characteristic
Specifications
FIIG
T312-A
End Item Identification [AGAV]
Airbus A330 And A340
Part Name Assigned By Controlling Agency [CXCY]
Attendant Aircraft Seat

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1680-01-575-6251 Freight Data Freight Information 1680-01-575-6251

1680-01-575-6251 has freight characteristics managed by Australia.. 1680-01-575-6251 has a variance between NMFC and UFC when transported by rail and the description should be consulted.