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5365-01-525-5518

Machine Thread Bushing

5365015255518 015255518 4D0001-8T2

A straight nonfluid fitting with wrenching facilities on one end and external threads, other than pipe or hose series, on the other end. It has an unthreaded through hole in its axis which may be countersunk and/or counterbored on one or both ends. It is designed to accommodate a shaft, or the like, or used to reinforce a hole in a bulkhead, or the like. For similar items specifically designed for use in a stuffing box, see PACKING NUT. For nonfluid items with an internal thread, see INSERT, SCREW THREAD&#59; or ADAPTER BUSHING. Excludes REDUCER, BOSS&#59; and items designed to accommodate a tube or tube fitting. View more Machine Thread Bushing

5365-01-525-5518 BUSHING,MACHINE THREAD 5365015255518 015255518

Managed by United States
NSN Created on 15 Nov 2004
Data Last Changed
January 2023
NATO Update Count
4
NATO Data Quality
5365-01-525-5518 BUSHING,MACHINE THREAD 5365015255518 015255518 1/1
NSN 5365-01-525-5518 (Generic Image) 1/1

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5365-01-525-5518 Demil Restrictions 5365-01-525-5518

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

5365-01-525-5518 is a Machine Thread Bushing that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

5365-01-525-5518 End Users End Users 5365-01-525-5518

US Air Force (FBB5)
Effective Date:
1 Nov 2004

5365-01-525-5518 Manufacturers Approved Sources 5365-01-525-5518

5365-01-525-5518 Technical Data Datasheet 5365-01-525-5518

Characteristic
Specifications
FIIG
A540S0
End Item Identification [AGAV]
F/A C-17A
Hole Inside Diameter [BXBR]
0.509 Inches Minimum And 0.512 Inches Maximum
Material [MATT]
Titanium
Nominal Thread Size [CQJX]
0.7188 Inches
Screw Thread Length [AJYR]
0.634 Inches Minimum And 0.639 Inches Maximum
Slot Depth [AAZT]
0.015 Inches Minimum And 0.031 Inches Maximum
Slot Width [ABGC]
0.116 Inches Minimum And 0.146 Inches Maximum
Overall Length [ABHP]
0.935 Inches Minimum And 0.965 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]
Bushing, Machine Threaded
Special Features [FEAT]
Matl Has Polytetrafluoroethylene Coated
Thread Pitch Diameters [AAJE]
+0.6830 To 0.6863 Inches
Thread Series Designator [THSD]
Unjs
Thread Quantity Per Inch [CMLP]
2
Width Across Flats [ASDB]
0.985 Inches Minimum And 1.015 Inches Maximum
Wrenching Facility Shape [ACSL]
Hexagon
Thread Direction [AAJF]
Right-Hand

5365-01-525-5518 Management Data Management Data 5365-01-525-5518

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2018
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5365-01-525-5518 Freight Data Freight Information 5365-01-525-5518

5365-01-525-5518 has freight characteristics.. 5365-01-525-5518 has a variance between NMFC and UFC when transported by rail and the description should be consulted.