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108-2086 Product Specification 07 May 12 Rev F .187 and .250 Series AMPLIVAR* FASTON* Flag Receptacle 1. SCOPE 1.1. Content This specification covers performance, tests and quality requirements for the .187 and .250 Series AMPLIVAR* FASTON* Flag Receptacles. 1.2. Qualification When tests are performed on the subject product line, procedures specified in Figure 1 shall be used. All inspections shall be performed using the applicable inspection plan and product drawing. 1.3. Qualification Test Results Successful qualification testing on the .187 series product line was completed on 31Mar03. Additional testing was completed on 05Oct04. Successful qualification for the .250 series product line was completed on 08Mar12. The Qualification Test Report number for this testing is 501-552. This documentation is on file at and available from Engineering Practices and Standards (EPS). 2. APPLICABLE DOCUMENTS The following documents form a part of this specification to the extent specified herein. Unless otherwise specified, the latest edition of the document applies. In the event of conflict between the requirements of this specification and the product drawing, the product drawing shall take precedence. In the event of conflict between the requirements of this specification and the referenced documents, this specification shall take precedence. 2.1. 2.2. Documents ● 109-197: AMP Test Specifications vs EIA and IEC Test Methods ● 114-2152: AMPLIVAR FASTON Flag Receptacles ● 501-552: .187 and .250 Series AMPLIVAR* FASTON* Flag Receptacle Commercial Standards ● EIA-364: Electrical Connector/Socket Test Procedures Including Environmental Classifications ● UL-310: Electrical Quick-Connect Terminals 3. REQUIREMENTS 3.1. Design and Construction Product shall be of the design, construction and physical dimensions specified on the applicable product drawing. 3.2. Materials Materials used in the construction of this product shall be as specified on the applicable product drawing. 3.3. 3.4. Ratings ● Voltage: 240 volts AC ● Current: See Figure 4 for applicable current carrying capability ● Temperature: -40 to 105°C Performance and Test Description Product is designed to meet the electrical, mechanical and environmental performance requirements specified in Figure 1. Unless otherwise specified, all tests shall be performed at ambient environmental conditions per EIA-364. ©2012 Tyco Electronics Corporation, a TE Connectivity Ltd. company All Rights Reserved | Indicates Change This controlled document is subject to change. For latest revision and Regional Customer Service, visit our website at www.te.com PRODUCT INFORMATION 1-800-522-6752 *Trademark. TE Connectivity, TE connectivity (logo), and TE (logo) are trademarks. Other logos, product and/or company names may be trademarks of their respective owners. 1 of 6 108-2086 3.5. Test Requirements and Procedures Summary Test Description Requirement Procedure Initial examination of product. Meets requirements of product drawing. EIA-364-18. Visual and dimensional (C of C) inspection per product drawing. Final examination of product. Meets visual requirements. EIA-364-18. Visual inspection. ELECTRICAL Low level contact resistance. 2.5 milliohms maximum. ∆R 2.0 milliohms maximum. EIA-364-23. Subject specimens to 100 milliamperes maximum and 20 millivolts maximum open circuit voltage. See Figure 3. Temperature rise vs current. 30°C maximum temperatu re rise at EIA-364-70, specified current. Method 1. Stabilize at a single current level until 3 readings at 5 minute intervals are within 1°C. See Figure 4. Current cycling. Temperature rise of the conductor th during the 500 cycle shall not be more than 15°C higher than the th temperature rise during the 24 cycle, and neither rise shall be more than 85°C. EIA-364-55. Subject specimens to 500 cycles of 45 minutes current ON and 15 minutes current OFF. See Figure 4. MECHANICAL Vibration, random. No discontinuities of 1 microsecond EIA-364-28, or longer duration. Test Condition VII, See Note. Condition D. Subject mated specimens to 3.10 G's rms between 20-500 Hz. 15 minutes in each of 3 mutually perpendicular planes. See Figure 5. Mechanical shock. No discontinuities of 1 microsecond EIA-364-27, or longer duration. Method H. See Note. Subject mated specimens to 30 G's half-sine shock pulses of 11 milliseconds duration. 3 shocks in each direction applied along 3 mutually perpendicular planes, 18 total shocks. See Figure 5. Figure 1 (continuted) Rev F 2 of 6 108-2086 Test Description Requirement Procedure Durability. See Note. EIA-364-9. Mate and unmate specimens for 6 cycles at a maximum rate of 500 cycles per hour. Mating force. 66.72 N [15 lbf] maximum. EIA-364-13. Measure force necessary to mate specimens at a maximum rate of 12.7 mm [.5 in] per minute. Unmating force. 22.24 N [5 lbf] minimum for 1 unmating. th 13.3 N [3 lbf] minimum for 6 unmating. EIA-364-13. Measure force necessary to unmate specimens at a maximum rate of 12.7 mm [.5 in] per minute. Termination tensile strength. See Figure 4. EIA-364-8. Determine crimp tensile at a maximum rate of 25.4 [1 in] per minute. st ENVIRONMENTAL Humidity-temperature cycling. See Note. EIA-364-31, Method III. Subject specimens to 10 cycles (10 days) between 25 and 65°C at 80 to 100% RH. Temperature life. See Note. EIA-364-17, Method A, Test Condition 4, Test Time Condition C. Subject mated specimens to 105°C for 500 hours. NOTE NOTE Shall meet visual requirements, show no physical damage, and meet requirements of additional tests as specified in the Product Qualification and Requalification Test Sequence shown in Figure 2. Figure 1 (end) Rev F 3 of 6 108-2086 3.6. Product Qualification and Requalification Test Sequence Test Group (a) Test or Examination 1 2 3 4 Test Sequence (b) Initial examination of product 1 1 Low level contact resistance 3,7 2,8 Temperature rise vs current 1 4,9 2,4 Current cycling 3 Vibration 5 Mechanical shock 6 Durability 4 Mating force 2 Unmating force 8 7 3 Termination tensile strength 2 Humidity-temperature cycling 5 Temperature life 6 Final examination of product NOTE 1 9 10 3 5 (a) See paragraph 4.1.A. (b) Numbers indicate sequence in which tests are performed. Figure 2 4. QUALITY ASSURANCE PROVISIONS 4.1. Qualification Testing A. Specimen Selection Specimens shall be prepared in accordance with applicable Instruction Sheets and shall be selected at random from current production. Test Groups 1, 2, and 4 shall consist of a minimum of six specimens. Test Group 3 shall consist of a minimum of five specimens. B. Test Sequence Qualification inspection shall be verified by testing specimens as specified in Figure 2. 4.2. Requalification Testing If changes significantly affecting form, fit or function are made to the product or manufacturing process, product assurance shall coordinate requalification testing, consisting of all or part of the original testing sequence as determined by development/product, quality and reliability engineering. 4.3. Acceptance Acceptance is based on verification that the product meets the requirements of Figure 1. Failures attributed to equipment, test setup or operator deficiencies shall not disqualify the product. If product failure occurs, corrective action shall be taken and specimens resubmitted for qualification. Testing to confirm corrective action is required before resubmittal. Rev F 4 of 6 108-2086 4.4. Quality Conformance Inspection The applicable quality inspection plan shall specify the sampling acceptable quality level to be used. Dimensional and functional requirements shall be in accordance with the applicable product drawing and this specification. Figure 3 Low Level Contact Resistance Measurement Points .187 Series Wire Size Wire Gage CMA Rev F Current (amperes) Copper Aluminum Tensile (N [lbf]) Copper Aluminum 24 23.5 23 22.5 455 511 566 635 2.3 2.5 2.6 2.8 1.5 1.6 1.7 1.8 22.24 [5] 25.58 [5.75] 28.91 [6.5] 32.25 [7.25] 6.67 [1.5] 7.78 [1.75] 8.90 [2] 10.01 [2.25] 22 21.5 21 708 795 888 3 3.2 3.4 1.9 2.1 2.2 35.59 [8] 41.15 [9.25] 46.71 [10.5] 11.12 [2.5] 13.34 [3] 15.57 [3.5] 20.5 992 3.6 2.3 52.27 [11.75] 16.68 [3.75] 20 19.5 19 1116 1246 1391 4 4.6 5.3 2.6 3 3.4 57.83 [13] 66.72 [15] 73.40 [16.5] 17.79 [4] 21.13 [4.75] 24.47 [5.5] 18.5 1560 6.1 3.9 83.40 [18.75] 27.85 [6.26] 18 17.5 17 1747 1962 2190 7 7.7 8.3 4.5 5 5.4 93.41 [21] 104.10 [23.4] 117.88 [26.5] 31.14 [7] 34.47 [7.75] 37.81 [8.5] 16.5 2460 9 5.8 133.45 [30] 43.37 [9.75] 16 15.5 15 2746 3136 3446 10 11.3 12.4 6.5 7.3 8 147.90 [33.25] 169.03 [38] 186.83 [42] 48.93 [11] 56.05 [12.6] 62.28 [14] 14.5 3869 13.6 8.8 211.29 [47.5] 69.39 [15.6] 14 4330 15 9.7 235.76 [53] 77.84 [17.5] 5 of 6 108-2086 .250 Series: Wire Size Wire Dia. (mm) 0.60 0.85 1.00 1.10 NOTE NOTE CMA Current ( amperes) Copper Tensile N (lbf) Copper 566 1120 1550 1875 2.6 4 6.1 8.1 30 (6.5) 59 (13) 83 (18.8) 116 (26) 1. CMA values are based on standard magnet wire with single film coating. 2. Current values for standard copper wire gages are from UL 310, others are rated based on their respective CMA. 3. Current values for aluminum wires are 64.5% of the copper wire of equivalent gage. 4. Tensile values are calculated at 50% of the bare wire tensile. Figure 4 Current Carrying/Tensile Capability Figure 5 Vibration and Mechanical Shock Mounting Fixture Rev F 6 of 6