4920-14-489-4059
Aircraft Maintenance Alignment Jig
4920144894059 144894059 J05655-07-1000 411334-001
A jig designed to align aircraft components during maintenance and/or test procedures. View more Aircraft Maintenance Alignment Jig
Managed by France
NSN Created on 16 Jul 1997
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 4920-14-489-4059
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Related Documents 4920-14-489-4059 5+ Documents (More...)
5315-14-479-2720 5315144792720 144792720 is a headless, generally cylindrically-shaped item having a straight, smooth, solid body, with or without a drilled hole(s). it has an outside diameter equal to or less than its length. its length must not exceed twelve inches (304 mm); for items whose length exceeds twelve inches (304 mm); see rod,straight,headless. it is used for aligning or transfer of torque and/or thrust, by fitting into corresponding holes of another item. see also pin,straight,threaded.
5315-14-521-2361 5315145212361 145212361 is a headed, cylindrically-shaped metal item having a shank and/or shoulder offset from the geometric center of the head. if shouldered, a portion of the shank and/or shoulder may be concentric with the head.
3040-14-521-2364 3040145212364 145212364 is an axle having two or more different diameters (greater than 0.031 inches (0.79 millimeter)) along its length. it must have one or more of the following conditions: a specified surface finish designation in the range 1 to 125 microinches (0.025 to 3.2 micrometers), periphersl flat(s), circular groove(s), keyway(s), splines, threads, or holes. the ends and/or sholders may be machined to accommodate bearings couplings and the like. it is not designed for use in aligning by fitting into corresponding holes of another item. for items used to transmit motion see shaft(1), shoulder. for items not having any of the above conditions see pin, shoulder, headless. excludes shaft(1),straight; and axle(1), straight.
5310-14-521-2365 5310145212365 145212365 is a washer having a centrally located hole with a solid or laminated cross-section and two flat parallel bearing surfaces. the hole must be 75 percent or less than the largest dimension and the bearing surface finish is greater than 32 microinch (0.8 micrometer). the thickness cannot exceed 25 percent of the largest outside dimension. when the largest outside dimension is less than 1/4 inch or 6mm, the thickness must be 0.006 inches (0.15mm) or greater and for items 1/4 inch (6mm) or larger, the thickness must be 0.016 inches (0.4mm) or greater. the maximum tolerance is applied to dimensions and used as a determining factor. items with separable lamination use shim. for items fabricated from ceramic or electrically rated materials by specification or industry standards use insulator (1), washer. excludes disk, valve, graphite impregnated and lubricated items.
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Aircraft Maintenance Alignment Jig (INC 52378)
-271-6816 Aircraft Maintenance Alignment Jig M57T50166RNCC: 3 | RNVC: 2 | DAC: 4 14 Jun 2011 4920-14-489-4059
Restrictions 4920-14-489-4059
End Users 4920-14-489-4059
- France (ZF)
Approved Sources 4920-14-489-4059
- Part Number
- Manufacturer
- Status
- J05655-07-1000
- Manufacturer
- F3018 - Naval Group Site D'angouleme-Ruelle (Active)
- Primary Buy
- Primary Buy
- 411334-001
- F3018 - Naval Group Site D'angouleme-Ruelle (Active)
- Canceled/Obsolete
- Canceled/Obsolete
NATO Stock Numbers Related to 4920-14-489-4059
4920-16-004-0543 4920-14-569-2823 4920-99-770-8569 4920-98-205-0106 4920-99-741-4155 4920-16-001-8539 4920-99-760-1222 4920-40-000-3345 4920-99-794-6555 4920-14-569-2826 4920-01-198-2025 4920-66-160-5596 4920-99-741-4184 4920-00-021-7719 4920-00-103-9920 4920-01-060-1792 4920-14-576-2562 4920-14-569-2820