Premium Information is available for this item - Upgrade for $1 a day

6610-01-415-1623

Angle Indicator

6610014151623 014151623 2552-11

An indicator designed to display the angular relatioship of two reference points. View more Angle Indicator

6610-01-415-1623 INDICATOR,ANGLE 6610014151623 014151623

Managed by United States
NSN Created on 21 Jun 1995
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
6610-01-415-1623 INDICATOR,ANGLE 6610014151623 014151623 1/1
NSN 6610-01-415-1623 (Generic Image) 1/1

6610-01-415-1623 Stock and Availability Marketplace 6610-01-415-1623

Need Help?
Request a Quotation from participating marketplace vendors

6610-01-415-1623 Related Documents Related Documents 6610-01-415-1623 5+ Documents (More...)

your web browser . 2320-14-291-2461Truck Tractor2320142912461 142912461 25521101 TB015M3H TB015M3H2 2552-11
Angle Indicator 6610014151623 014151623 for $1 a day Upgrade your Account Upgrade 6610-01-415-1623Angle
Indicator6610014151623 014151623 2552-11 Request a Quotation from participating marketplace vendors
https//www.nsnlookup.com /nato/nato-stock-numbers/inc Angle Indicator (INC 38916) 6 10 Oct 1995 6610-01-415-1623
1560-01-206-7868 1560012067868 012067868 is a rigid item of various shapes permanently attached to a structure of an aircraft, designed to provide access for inspection, service, replacement of components and/or adjustments. it is designed to be attached by means of hinges or similar device. it may include self-closing features and have a quick release or other type latching to permit access with a minimum of effort. it may include an observation window. excludes cover, access&#59; cover access, aircraft&#59; door, access&#59; door, aircraft and all doors not specifically designed to provide access for the purposes listed above.
5305-00-144-3821 5305001443821 001443821 is an externally threaded fastener whose threaded portion is of one nominal diameter, no 0 (0.060 in./1.5 mm) or larger, designed to be held or driven with either a wrench or an inserted driver or both (excluding internal socket or internal multiple spline types), in sizes below no. 10 (0.190 in./5 mm). no. 10 and larger sizes must have a head designed for any type inserted driver (excluding internal socket or internal multiple spline types), but may also be designed for external wrenching. a locking feature may be incorporated in the design of the head or threads. excludes bolt, clevis; bolt, externally relieved body; screw, externally relieved body; and screw, assembled washer. see also, screw, instrument; bolt, machine; bolt, internal wrenching; and screw, cap socket head.

6610-01-415-1623 Demil Restrictions 6610-01-415-1623

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

6610-01-415-1623 is a Angle Indicator that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.

6610-01-415-1623 HTS and ScheduleB Import and Export 6610-01-415-1623

6610-01-415-1623 End Users End Users 6610-01-415-1623

Norway (ZT01)
Effective Date:
1 Jun 1995

6610-01-415-1623 Manufacturers Approved Sources 6610-01-415-1623

6610-01-415-1623 Technical Data Datasheet 6610-01-415-1623

Characteristic
Specifications
FIIG
A53200
Special Features [FEAT]
Simulated Pitch/Trim

6610-01-415-1623 Related Items NATO Stock Numbers Related to 6610-01-415-1623

6610-01-415-1623 Freight Data Freight Information 6610-01-415-1623

6610-01-415-1623 has freight characteristics.. 6610-01-415-1623 has a variance between NMFC and UFC when transported by rail and the description should be consulted.