1730-99-257-6676

Aircraft Maintenance Ladder

1730992576676 992576676 EU1205G011-041 1MEVGRS

A ladder designed specifically for performing maintenance on tail sections, antennas, and other parts of an aircraft. It is usually equipped with facilities for attachment to the aircraft. View more Aircraft Maintenance Ladder

1730-99-257-6676 LADDER,AIRCRAFT MAINTENANCE 1730992576676 992576676

Managed by United Kingdom
NSN Created on 3 Jul 2004
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
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NSN 1730-99-257-6676 (Generic Image) 1/1

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1730-99-257-6676 Related Documents Related Documents 1730-99-257-6676 5+ Documents (More...)

1730-66-153-8299 1730-01-286-8856 1730-12-370-5623 https//www.nsnlookup.com /fsg-17/fsc-1730/uk 1730-99-257-6676
Aircraft Maintenance Ladder 1730992576676 786-9284 1730-33-209-4597 1730-12-186-8809 1730-16-005
Maintenance Ladder 1730992730488 786-9284 1730-33-209-4597 www.nsnlookup.com /fsg-17/fsc-1730/uk 1730-99-257-6676
Aircraft Maintenance Ladder 1730992576676 786-9284 1730-33-209-4597 www.nsnlookup.com /fsg-17/fsc
14-472-9035 Aircraft Maintenance Ladder 332A95-0081-10RNCC: 3 | RNVC: 2 | DAC: 2 16 Nov 1994 1730-99-257-6676
5306-99-562-5930 5306995625930 995625930 is an externally threaded fastener whose unthreaded portion is of a specified grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten-thousandths (0.0015) of an inch (0.038 mm) or less. the nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. the head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. a locking feature may be incorporated in the design of the head or threads. for items having close tolerance, and fabricated from material having 160,000 pounds per square inch (1100 megapascals) minimum tensile strength, see bolt, shear. for items fabricated from material having less than 160,000 pounds per square inch (1100 megapascals) minimum tensile strength and not having a close tolerance, see bolt, machine.

1730-99-257-6676 Demil Restrictions 1730-99-257-6676

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1730-99-257-6676 is a Aircraft Maintenance Ladder

1730-99-257-6676 End Users End Users 1730-99-257-6676

United Kingdom (ZK)

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