5935-17-106-3891
Electrical Receptacle Connector
5935171063891 171063891 4011334059707 413502
An electrical fitting with electrical contacts constructed to be affixed to the end of a cable, conduit, coaxial line, cord, wire (includes printed/etched), PRINTED WIRING BOARD, or the like for convenience in joining with another electrical connector(s) or PRINTED WIRING BOARD. It is designed to be mounted on a bulkhead, chassis, panel, wall, PRINTED WIRING BOARD, or the like. Excludes LAMPHOLDER; JACK, TELEPHONE; JACK, TIP; INSERT ELECTRICAL CONNECTOR; INSERT MODULE, ELECTRICAL CONNECTOR; CONNECTOR BODY (as modified) and SOCKET, PLUG-IN ELECTRONIC COMPONENTS. See also WIRING HARNESS (as modified) and CABLE ASSEMBLY (as modified). For items with termination wires of more than four inches in length, see LEAD ASSEMBLY, ELECTRICAL. For items without inserts, see SHELL, ELECTRICAL CONNECTOR. View more Electrical Receptacle Connector
Managed by Netherlands
NSN Created on 29 Apr 1992
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
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Related Documents 5935-17-106-3891 5+ Documents (More...)
2007 5940-17-055-3545 Grounding Terminal Strip 11.0901RNCC: 3 | RNVC: 2 | DAC: 4 21 Jul 1984 5935-17-106-3891
1240-12-175-9065 1240121759065 121759065 LAGERBUECHSE
1560-01-246-9014 1560012469014 012469014 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.
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5905-00-485-8837 Precision Wire Wound Variable Resistor
5905-00-485-8837 5905004858837 004858837 is a resistor in which a sliding or rolling contact moves over an exposed area of the resistive element to change the ohmic value of the output. the functional tolerance (linearity) of the output is equal to or less than plus or munus 1 percent on linear outputs. specified outputs such as sine, cosine, tangent, etc., shall be considered to be precision. for items having manually positioned taps designed to be set and fixed prior to use, see resistor, adjustable, for items with step by step variation, see rheostat and resistor, step by step. for tandem-mounted items designed to function together as an attenuator (and rated accordingly), see attenuator, variable. excludes resistor (1), variable, nonwire wound, nonprecision; resistor (1), variable, nonwire wound, precision; and resistor (1), variable, wire wound, nonprecision.
1560-01-246-9015 1560012469015 012469015 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.
Restrictions 5935-17-106-3891
End Users 5935-17-106-3891
- Netherlands (ZN)
Approved Sources 5935-17-106-3891
- Part Number
- Manufacturer
- Status
- 4011334059707
- Manufacturer
- H5892 - Gunneman B.V. (Active)
- Primary Buy
- Primary Buy
- 413502
- H5892 - Gunneman B.V. (Active)
- Primary Buy
- Primary Buy
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