Testing is performed at an internationally recognized, independent research, engineering and evaluation laboratory who by contractual agreement with their clients does not allow the use of their name or logo because doing so may imply an endorsement of products or services. For this reason, all references to said independent third party lab have been removed. Should you require the full unedited version, please contact the company identified below. Mechanical Engineering Division March 31, 2010 SUMMARY OF TESTS PERFORMED Project Number: 18.04481.17.101 Company: Panasonic Computer Solutions Company Three Panasonic Way, 2F-12 Secaucus, NJ 07094 Attn: Angela MacNeill Equipment Tested: Panasonic CF-H1 Field Test Dates: January 2010 – March 2010 Notes: The test item was evaluated for ability to boot into the Microsoft Windows XP operating system following each of the tests described within this summary report or for the ability to play an audio/visual file during the test parameter application. A listing of summarized tests and results appear in the accompanying table. Full details will be provided in Report Number 18.04481.17.100.FR1. ® Report Written By: Eric Dornes Principal Engineer Structural Dynamics and Product Assurance Section Page 1 Summary of Tests Performed— Panasonic CF-H1 Field 03/31/10 Summary of Tests Performed on the Panasonic CF-H1 Test Description Test Parameters Altitude: Storage/Air Transport Altitude: Operation/Air Carriage Altitude: Storage/Air Transport Altitude: Operation/Air Carriage High Temperature: Storage High Temperature: Operation MIL-STD-810G, Method 500.5, Procedure I 15,000ft Non-Operating MIL-STD-810G, Method 500.5, Procedure II 15,000ft Operating MIL-STD-810G, Method 500.5, Procedure I 40,000ft Non-Operating MIL-STD-810G, Method 500.5, Procedure II 40,000ft Operating MIL-STD-810G, Method 501.5, Procedure I 160°F Non-Operating MIL-STD-810G, Method 501.5, Procedure II 140°F Operating MIL-STD-810G, Method 501.5, Procedure III High storage (non-operating) to high operating (test for operation) Test results are for battery operation MIL-STD-810G, Method 502.5, Procedure I -60°F Non-Operating MIL-STD-810G, Method 502.5, Procedure II -20°F Operating MIL-STD-810G, Method 503.5, Procedure I From 200°F to -60°F, three cycles MIL-STD-810G, Method 506.5, Procedure I 5.8in/hr rain, 70mph wind, 30 minutes per surface Unit operating MIL-STD-810G, Method 506.5, Procedure III 15 minute exposure, drip test MIL-STD-810G, Method 507.5, Procedure II (Aggravated) Temp. cycles 86°F to 140°F; 95%RH MIL-STD-810G, Method 510.5, Procedure I Blowing Dust (operating) Operating temperature of 140°F MIL-STD-810G, Method 510.5, Procedure II Blowing Sand (operating) Operating temperature of 140°F MIL-STD-810G, Method 511.5, Procedure I MIL-STD-810G, Method 514.6, Procedure I (Transportation) Panasonic provided conditions (operating) MIL-STD-810G, Method 514.6, Procedure I (Transportation) Category 24, General minimal integrity (nonoperating) MIL-STD-810G, Method 514.6, Procedure I (Transportation) Category 24, Helicopter minimal integrity (operating), 1 hr. per axis High Temperature: Tactical–Standby to Operational Low Temperature: Storage Low Temperature: Operation Temperature Shock Rain: Blowing Rain: Drip Humidity Sand and Dust: Dust Sand and Dust: Sand Explosive Atmosphere Vibration: General Vibration – operating Vibration: General Vibration – nonoperating Vibration: General Vibration – operating Page 2 Test Results Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Pass Summary of Tests Performed— Panasonic CF-H1 Field Test Description Vibration: General Vibration – nonoperating Shock: Functional Shock: Transit-Drop 48-inch Shock: Transit-Drop 60-inch Shock: Transit-Drop 72-inch Shock: Transit-Drop 48-inch Shock: Transit-Drop 60-inch Shock: Transit-Drop 72-inch Freeze / Thaw Test Parameters MIL-STD-810G, Method 514.6, Procedure I (Transportation) Category 24, Helicopter minimal integrity (nonoperating), 2 hours per axis MIL-STD-810G, Method 516.6, Procedure I 40g, 11ms Operating MIL-STD-810G, Method 516.6, Procedure IV 26 drops – 48in height on to 2in plywood – non operating All drops performed on the same unit MIL-STD-810G, Method 516.6, Procedure IV 26 drops – 60in height on to 2in plywood – non operating All drops performed on the same unit that was also subjected to all 48in drops MIL-STD-810G, Method 516.6, Procedure IV 26 drops – 72in height on to 2in plywood – non operating All drops performed on the same unit that was also subjected to all 48in and all 60in drops MIL-STD-810G, Method 516.6, Procedure IV 26 drops – 48in height on to 2in plywood – operating All drops performed on the same unit MIL-STD-810G, Method 516.6, Procedure IV 26 drops – 60in height on to 2in plywood – operating All drops performed on the same unit that was also subjected to all 48in drops MIL-STD-810G, Method 516.6, Procedure IV 26 drops – 72in height on to 2in plywood – operating All drops performed on the same unit that was also subjected to all 48in and all 60in drops MIL-STD-810G, Method 524, Procedure III (Rapid Temperature Change) Test effects include condensation Page 3 03/31/10 Test Results Pass Pass Pass Pass Pass Pass Pass Pass Pass