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5340-01-398-8733

Rod End Clevis

5340013988733 013988733 17G130022-7

A forked part, having transverse hole(s) or slot(s) in each arm (prong) to accommodate a bolt, pin, or the like, and having a connection facility opposite the fork. It is designed to be attached to a shaft, rod, turnbuckle or the like by welding, threading, and/or pinning. May include provisions for locking. See also YOKE, UNIVERSAL JOINT and CONNECTOR, ROD END. For items specifically designed for aviation, see CLEVIS, ROD END, AVIATION. View more Rod End Clevis

5340-01-398-8733 CLEVIS,ROD END 5340013988733 013988733

Managed by United States
NSN Created on 10 Nov 1994
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5340-01-398-8733 CLEVIS,ROD END 5340013988733 013988733 1/1
NSN 5340-01-398-8733 (Generic Image) 1/1

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5340-01-398-8733 Related Documents Related Documents 5340-01-398-8733 3+ Documents (More...)

17G130022-7 A forked part, having transverse hole(s) or slot(s) in each arm (prong) to accommodate a
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5340-01-398-8733 Demil Restrictions 5340-01-398-8733

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

5340-01-398-8733 is a Rod End Clevis 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 may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

5340-01-398-8733 End Users End Users 5340-01-398-8733

US Air Force (FBB5)
Effective Date:
1 Dec 1999
Former MOE Rule:
FEKZ

5340-01-398-8733 Manufacturers Approved Sources 5340-01-398-8733

5340-01-398-8733 Technical Data Datasheet 5340-01-398-8733

Characteristic
Specifications
FIIG
A264A0
Material [MATT]
Aluminum Alloy 6061 Overall
Material Document And Classification [MDCL]
Qq-A-250/11 Fed Spec Single Material Response Overall
Securing Pin Hole Diameter [AKYE]
2.0350 Inches Nominal
Hole Shape [BCLP]
Round

5340-01-398-8733 Management Data Management Data 5340-01-398-8733

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

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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5340-01-398-8733 Freight Data Freight Information 5340-01-398-8733

5340-01-398-8733 has freight characteristics.. 5340-01-398-8733 has a variance between NMFC and UFC when transported by rail and the description should be consulted.