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1680-01-517-8747

Inertia Lock Shoulder Harness Reel

1680015178747 015178747 HR30100

A rotary device designed to be installed in an aircraft to automatically control the extension and retraction of a shoulder harness attachment cable or webbing. It incorporates an inertia locking mechanism that restrains the forward movement of flight personnel in the event of abrupt deceleration of the aircraft. It may include the attachment cable or webbing and the manually or electrically operated controls. View more Inertia Lock Shoulder Harness Reel

1680-01-517-8747 REEL,SHOULDER HARNESS,INERTIA LOCK 1680015178747 015178747

Managed by United States
NSN Created on 23 Feb 2004
Data Last Changed
May 2023
NATO Update Count
3
NATO Data Quality
1680-01-517-8747 REEL,SHOULDER HARNESS,INERTIA LOCK 1680015178747 015178747 1/1
NSN 1680-01-517-8747 (Generic Image) 1/1

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1680-01-517-8747 Related Documents Related Documents 1680-01-517-8747 3+ Documents (More...)

Documents 1680-01-621-4428 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-517-8747
Inertia Lock Shoulder Harness Reel 015178747 1680-01-517-8747 1680015178747 015178747 is a rotary
01-621-4428 Inertia Lock Shoulder Harness Reel 103528-4RNCC: 3 | RNVC: 2 | DAC: 4 9 Sep 2013 1680-01-517-8747
1680-01-487-3993 1680014873993 014873993 is a rotary device designed to be installed in an aircraft to automatically control the extension and retraction of a shoulder harness attachment cable or webbing. it incorporates an inertia locking mechanism that restrains the forward movement of flight personnel in the event of abrupt deceleration of the aircraft. it may include the attachment cable or webbing and the manually or electrically operated controls.

1680-01-517-8747 Demil Restrictions 1680-01-517-8747

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

1680-01-517-8747 is a Inertia Lock Shoulder Harness Reel 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.

1680-01-517-8747 HTS and ScheduleB Import and Export 1680-01-517-8747

1680-01-517-8747 End Users End Users 1680-01-517-8747

Singapore (YJ01)
Effective Date:
1 Feb 2004
Norway (ZT01)
Effective Date:
1 Nov 2005

1680-01-517-8747 Manufacturers Approved Sources 1680-01-517-8747

1680-01-517-8747 Technical Data Datasheet 1680-01-517-8747

Characteristic
Specifications
FIIG
T312-E
End Item Identification [AGAV]
Kc-135 Aircraft
Part Name Assigned By Controlling Agency [CXCY]
Reel Assembly, Inertia

1680-01-517-8747 Related Items NATO Stock Numbers Related to 1680-01-517-8747

1680-01-517-8747 Freight Data Freight Information 1680-01-517-8747

1680-01-517-8747 has freight characteristics managed by Singapore.. 1680-01-517-8747 has a variance between NMFC and UFC when transported by rail and the description should be consulted.