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1680-01-394-5706

Aircraft Seat Leg Assembly

1680013945706 013945706 103031-1

A rigid metallic item which, in conjunction with a frame, aids in the support of SEAT (1), AIRCRAFT. It must have provisions for guide attachment hardware. See SEAT (1), AIRCRAFT EJECTION. View more Aircraft Seat Leg Assembly

1680-01-394-5706 LEG ASSEMBLY,SEAT,AIRCRAFT 1680013945706 013945706

Managed by United States
NSN Created on 10 Aug 1994
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1680-01-394-5706 LEG ASSEMBLY,SEAT,AIRCRAFT 1680013945706 013945706 1/1
NSN 1680-01-394-5706 (Generic Image) 1/1

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1680-01-394-5706 Related Documents Related Documents 1680-01-394-5706 5+ Documents (More...)

103031-1 A rigid metallic item which, in conjunction with a frame, aids in the support of SEAT (1),
United States (US) 4. 1680-01-394-5706 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1680-01-394-5706 RQST Updated Every Day 1680-01-394-5706 RQST NE Related Documents
1680-01-477-4215 1680-01-700-7616 1680-14-464-9504 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-394-5706
Aircraft Seat Leg Assembly 1680013945706 Assembly 1680013520039 611-6470 1680-01-477-4213 1680-
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1680-01-476-1522 1680-01-477-4215 1680-01-700-7616 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-394-5706
Aircraft Seat Leg Assembly 1680013945706 Seat Leg Assembly 1680013520039 611-6470 1680-01-477-4213
611-6470 1680-01-477-4213 1680-01-476-1522 1680-01-477-4215 1680-01-700-7616 1680-14-464-9504 1680-01-394-5706
Documents 1680-01-477-4215 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-394-5706
Aircraft Seat Leg Assembly 1680013945706 352-0039 Aircraft Seat Leg Assembly 1680013520039 611-
611-6470 1680-01-477-4213 1680-01-476-1522 1680-01-477-4215 1680-01-700-7616 1680-14-464-9504 1680-01-394-5706
Documents 1680-01-476-1522 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-394-5706
Aircraft Seat Leg Assembly 1680013945706 -1680/us 1680-01-352-0039 Aircraft Seat Leg Assembly 1680013520039
611-6470 1680-01-477-4213 1680-01-476-1522 1680-01-477-4215 1680-01-700-7616 1680-14-464-9504 1680-01-394-5706

1680-01-394-5706 Demil Restrictions 1680-01-394-5706

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

1680-01-394-5706 is a Aircraft Seat Leg Assembly 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.

1680-01-394-5706 HTS and ScheduleB Import and Export 1680-01-394-5706

1680-01-394-5706 End Users End Users 1680-01-394-5706

US Air Force (FBB5)
Effective Date:
1 May 2000
Former MOE Rule:
FECX

1680-01-394-5706 Manufacturers Approved Sources 1680-01-394-5706

1680-01-394-5706 Technical Data Datasheet 1680-01-394-5706

Characteristic
Specifications
FIIG
A23900
Material [MATT]
Aluminum Alloy
Overall Length [ABHP]
1.530 Inches Nominal
Overall Width [ABMK]
0.858 Inches Nominal
Special Features [FEAT]
Material 2024-T351;Qq-A-225/6;Or 2024-T4;Qq-A-200/3;Pivot,Leg Assy.
End Item Identification [AGAV]
C-17 Globmaster Aircraft

1680-01-394-5706 Management Data Management Data 1680-01-394-5706

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2010
Department of the Air Force (DF)
EA
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1680-01-394-5706 Freight Data Freight Information 1680-01-394-5706

1680-01-394-5706 has freight characteristics.. 1680-01-394-5706 has a variance between NMFC and UFC when transported by rail and the description should be consulted.