4920-99-114-4886

Aircraft Engine Maintenance Fixture

4920991144886 991144886 S3S20319000 7M123BD HU16250-4 HU16250

A fixture designed to hold/position aircraft engine/engine components to facilitate inspection, maintenance, repair, testing and/or replacement of components. View more Aircraft Engine Maintenance Fixture

4920-99-114-4886 FIXTURE,ENGINE MAINTENANCE,AIRCRAFT 4920991144886 991144886

Managed by United Kingdom
NSN Created on 25 Apr 1991
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
4920-99-114-4886 FIXTURE,ENGINE MAINTENANCE,AIRCRAFT 4920991144886 991144886 1/1
NSN 4920-99-114-4886 (Generic Image) 1/1

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Aircraft Engine Maintenance Fixture 4920-99-114-4886 4920991144886 991144886 is a fixture designed
5306-99-625-9809 5306996259809 996259809 is an externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. the threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. the head is not designed to be held or driven with an inserted driver or by the thumb and fingers. a locking feature may be incorporated in the design of the head or threads. head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. for items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, bolt, shear. see also screw, cap, hexagon head and screw, machine.
5310-99-625-9810 5310996259810 996259810 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.

4920-99-114-4886 Demil Restrictions 4920-99-114-4886

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

4920-99-114-4886 is a Aircraft Engine Maintenance Fixture

4920-99-114-4886 End Users End Users 4920-99-114-4886

Malaysia (YW)
Australia (ZA)
France (ZF)
Republic of Korea (ZH)
United Kingdom (ZK)
United States of America (ZZ)

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4920-99-114-4886 Contracting Technical Data File (CTDF) Contracting Technical Data File (CTDF) 4920-99-114-4886 October 2021

Criticality and Quality

Critical Item Code:
Flight Safety:
Life Support:
Certified Samples:
Serialization:
First Article Test (FAT):
Certificate of Quality Compliance:
Production Lot Testing:
Special Testing:
Qualified Products List (QPL):

Commercial Properties

Government Furnished Material:
Government Furnished Tooling:
Government Furnished Property:
Price Evaluation Code:
Diminshing Manufacturing Sources:
Warranty:
Commerical Off The Shelf (COTS):
End Item Application:
Auctioning Candidate:
Source of Procurement:
Contract Option:

Restrictions

Boeing Rights Guard:
Export Controlled:
Controlled Technical Data Package (TDP):
Restricted Technical Data Package (TDP):
Contains Classified Material
Weapons System Indicator Code (WSIC):
Z

Packaging Requirements

Packaging Determination Table:
Packaging Review Code:
Y
Special Packaging Instruction Number (SPIN):
Special Packaging Instruction Number Revision:
Special Packaging Instruction Number Date:
Pallet Reference Number Required: