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5365-01-543-1422
Machine Thread Bushing
5365015431422 015431422 54542
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; or ADAPTER BUSHING. Excludes REDUCER, BOSS; and items designed to accommodate a tube or tube fitting. View more Machine Thread Bushing
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United States (US) 4. 5365-01-543-1422 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 5365-01-543-1422 RQST Updated Every Day 5365-01-543-1422 RQST NE Related Documents
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Restrictions 5365-01-543-1422
5365-01-543-1422 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.
End Users 5365-01-543-1422
- US Air Force (FBB5)
- Effective Date:
- 1 Aug 2006
Approved Sources 5365-01-543-1422
- Part Number
- Manufacturer
- Status
- 54542
- Manufacturer
- 99643 - Eaton Aerospace Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 5365-01-543-1422
- Characteristic
- Specifications
- FIIG
- Specifications
- A540S0
- End Item Identification [AGAV]
- C-17A Aircraft
- Countersink Angle In Deg [AATA]
- 45.0
- Countersink Depth [ADBD]
- 0.025 Inches Minimum And 0.040 Inches Maximum
- Countersink Location [BQDD]
- Threaded End And Wrenching End
- Hole Inside Diameter [BXBR]
- 0.765 Inches Minimum And 0.785 Inches Maximum
- Material Document And Classification [MDCL]
- Sae-Ams-Qq-A-225/8 Fed Spec Single Material Response
- Material [MATT]
- Aluminum Alloy 6061
- Nominal Thread Size [CQJX]
- 1.063 Inches
- Screw Thread Length [AJYR]
- 0.370 Inches Nominal
- Overall Length [ABHP]
- 0.640 Inches Minimum And 0.660 Inches Maximum
- Part Name Assigned By Controlling Agency [CXCY]
- Retainer Nut
- Special Features [FEAT]
- Threads Are Unjef Series; Has A 0.150 Wide Grove Located Above The Threads, Dia Of Grove Area 0.971 To 0.981; Contains 2 Lockwire Holes 0.046 Dia Located 180 Deg Apart In The Wrenching Faclity End, 0.065 From The Top Edge And 0.078 From The Outside Edge; Threaded End Outside Edge Chamfered 45 Deg X 0.045
- Thread Quantity Per Inch [CMLP]
- 18
- Thread Tolerance Class [CTTC]
- 3A External
- Width Across Flats [ASDB]
- 0.970 Inches Minimum And 1.030 Inches Maximum
- Thickness [ABNM]
- 0.120 Inches Minimum And 0.140 Inches Maximum
- Thread Direction [AAJF]
- Right-Hand
Management Data 5365-01-543-1422
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Nov 2018
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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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Freight Information 5365-01-543-1422
5365-01-543-1422 has freight characteristics.. 5365-01-543-1422 has a variance between NMFC and UFC when transported by rail and the description should be consulted.