1. Composite Swing-Arm EMI/RFI Strain Relief

2.  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

3.  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

4. 515 Performance Testing of Glenair Material

5.  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

6.  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)

7.  (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

8.  (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

9.  (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

10. 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

11. 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

12. Swing-Arm Qualification Testing Summary Results

14.  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