composite swing-arm emi/rfi strain relief
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Composite Swing-Arm EMI/RFI Strain Relief
Light Weight - Corrosion Free - Three-in-One
Straight, 45 and 90 Degrees
Integrated EMI/RFI Shield Sock
Inspection Window
Self-Locking Coupling Nut
Optional Composite Braid (319-065)
Brown or Black Material Electroless Nickel Shield Termination and Interface
No-Braid Version (627-122) Available Backshell Holding Tool
319-064 Composite Swing-Arm Strain-Relief
Non Corrosive
2000+ Hours Salt Spray Light Weight
40% Lighter than Aluminum 80% Lighter than SST
Vibration Dampening Superior Mechanical Properties Injection Mold Components for
Connectors & Accessories AIR4567, Type I, Grades A&B, Class 2 General Duty -65 to -175 Deg C
Composite Ultem 2300 (PEI)Reinforced with Glass
515
Performance Testing of Glenair Material
440-088 and 440-089 Series Shield Sock Parts Were Developed for the F-22 to Accelerate EMI Shield Termination
Assembly Times and Reduce the Weight of Interconnect Cabling
Origin of the Swing-Arm: The F-22 Composite Braid Sock Strain Relief
Electrical Resistance per AS85049, para 3.5.2 / 4.6.3 Vibration per AS85049 para 3.5.4 / 4.6.5.3 Half Sine Shock per AS85049 para 3.5.5 / 4.6.6.2 Transfer Impedance and Shielding Effectiveness Test Report
2004-1 Available From Factory Upon Request
Outstanding Mechanical, Environmental and EMI Performance
F-22 Shield Sock Performance Testing(Test Report No. 08-0204 Available from Factory Upon Request)
(1) Select Straight, 45 or 90 Degree Angle; (2) Insert Wire Bundle; (3) Mark Support Ring Location; (4) Apply Optional Tape Wrap;
(5) Slide Cable Shielding Over Support Ring and Trim to Fit.
EMI Shield Termination Procedure
(6) Evenly Space Shield Pigtails, if any, Around Support Ring;
(7) Slide Backshell Shield Sock Over Support Ring;
(8) Trim and Fold Braid in Place;
(9) Install Band; (10) Wrap Assembly
Area with High Temperature Tape
EMI Shield Termination Procedure
(11) Secure Loose Areas of Shield Sock with Ties or Lacing;
(12) Tighten Backshell to Connector with 600-091 Series Backshell Holding Tool and Torque to 40 to 120 Lbs. (See Catalog Torque Chart).
(13) Tighten Strain-Relief Saddle Bars to Correct Torque: 5.2 lbs Max for #4 Fastener and 10 lbs Max for #6 Fastener.
(14) Use Only Genuine Glenair Tools and Replacement Parts
EMI Shield Termination Procedure
Operates in a similar manner to the F-22 Shield Sock, but offers three-in-one straight, 45° and 90° design for SKU reduction
The Swing-Arm Advantage
The Swing-Arm is perfectly suited for new connector accessory design-ins for the next generation of manned and unmanned
aircraft
Approved for use at: Lockheed Martin Boeing Bell Helicopter Northrop Grumman Bombardier Embraer
Proven Performance Applications
Swing-Arm Qualification Testing Summary Results
Swing-Arm Qualification Testing Summary Results
Please see the April 2007 Issue of QwikConnect
Complete Product Overview EMI Shield Assembly Instructions Application References How to Order and Part Number
Development Same-Day Inventory Listing Qualification Test Report Available in Hard Copy or at
www.glenair.com
For More Information
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