2840-25-118-2798

Plain Stud

2840251182798 251182798

A headless fastener not exceeding 12 inches (304.8 mm) in length, threaded externally on both ends with threads of the same nominal diameter. The maximum diameter of the unthreaded portion must not be greater than the nominal thread diameter plus 0.020 inches (0.508 mm). The unthreaded portion must be without locking or wrenching provisions. It may be thread relieved. See also ROD, THREADED END and ROD, CONTINUOUS THREAD. View more Plain Stud

2840-25-118-2798 STUD,PLAIN 2840251182798 251182798

Managed by Norway
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-25-118-2798 STUD,PLAIN 2840251182798 251182798 1/1
NSN 2840-25-118-2798 (Generic Image) 1/1

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Restrictions 2840-25-118-2798 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https
CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-118-2798
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Norway (NO) 2840-25-135-9270 and Components from Norway (NO) Turbine Engine Compressor Blade 2840-25-118-2798
www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-147-8577 https//www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-118-2798
Plain Stud 2840251182798 251182798 Turbine Engine Compressor Blade 2840-25-118-2798 https//www.nsnlookup.com
CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com /fsg-28/fsc-2840/no 2840-25-118-2798
Plain Stud 2840251182798 251182798 CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com
25-131-6511 Va Fitting Assembly 2840-25-131-6483 Aircraft Gas Turbine Engine Compressor Blade 2840-25-118-2798

2840-25-118-2798 Demil Restrictions 2840-25-118-2798

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-25-118-2798 is a Plain Stud

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