0-4600-407

Inertia Lo Shoulder Harness Reel

NSN 1680-00-330-8109

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

003308109

Technical Specifications of NSN

Overall Height:

4.250 inches

Overall Width:

4.875 inches

Mounting Hole Diameter:

0.257 inches

Mounting Hole Quantity:

Cable Diameter:

0.188 inches

Reel Type:

Unidirectional

Reel Location:

Left hand

Shoulder Harness Attachment Type For Which Designed:

Cable

Cable Travel Length On Drum:

18.000 inches

Shoulder Harness Attachment:

Included

Shoulder Harness Attachment Extended Length:

26.500 inches

Manual Lock Control Type:

Cable connection

Center To Center Distance From Reel To Control Handle Shaft:

24.000 inches

Electrically Operated Control:

Not included

Electrical Connector:

Not included

Nondefinitive Specification/std Data:

Ma1 type

NSN:

1680-00-330-8109

Item Name:

Reel,shoulder Harness,inertia Lo

Cage Code:

02860

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

MILR8236BASGTYPEMA1

Cage Code:

81349

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

19338

FIIG:

T312-E

Concept No.:

App. Key:

Cond. Code:

Status:

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

133300

UFC:

63220

LTL:

92.5

LCL:

100.0

WCC:

671

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Inertia Lo Shoulder Harness Reel"

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.