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1 of 15 © 2020 TE Connectivity family of companies All Rights Reserved | Indicates Change *Trademark. TE Connectivity, TE connectivity (logo), and TE (logo) are trademarks. Other logos, product, and/or com pany names may be trademarks of their respective owners. Product Specification 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 108-151009
11 MAY 2020 Rev D
DEUTSCH* DT Series Connector System 1. SCOPE 1.1. Content This specification covers performance, tests and quality requirements for the TE Connectivit y (TE) DT Series Connector System. 1.2. Qualification When tests are performed on the subject product line, procedures specified in Test Requirements and Procedures Summary sections 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 subject product line was completed in 1987 and 2017. The Qualification Test Report number for this testing is 501-151032 (original version) and 501-151088 (snap cap version). These documentations are on file at and available from Product Engine ering, Industrial Commercial Transportation (ICT). 2. APPLICABLE DOCUMENTS AND FORMS The following documents and forms constitute a part of this specification to the extent sp ecified herein. Unless otherwise indicated, the latest edition of the document applies. 2.1. TE Connectivity (TE) Documents 109-1 General Requirements for Testing 114-151000 Application Specification for DEUTSCH Size 16 S&F Pin & Socket 114-151001 Application Specification for DEUTSCH Size 16 S&F Pin & Socket 114-151004 Application Specification for DEUTSCH Size 4-20 Solid Pin & Socket 114-151009 Application Specification for DEUTSCH DT Series Connector System 408-151008 Instruction Guide DEUTSCH Removal Tool DT-RT1 501-151032 DT Qualification Test Report 501-151088 DT 2&3 pin Snap Cap Qualification Test Report 502-151009 DT Ingress Protection Engineering Test Report Product Drawings (X = A, B, C, D keys, XXXX = product modification) DT04-2P-XXXX 2pin Receptacle DT13-2P-XXXX 2pin Receptacle, 90° Header DT04-3P-XXXX 3pin Receptacle DT13-4P-XXXX 4pin Receptacle, 90° Header DT04-4P-XXXX 4pin Receptacle DT13-6P-XXXX 6pin Receptacle, 90° Header DT04-6P-XXXX 6pin Receptacle DT13-08PX-XXXX 8pin Receptacle, 90° Header DT04-08PX-XXXX 8pin Receptacle DT13-12PX-XXXX 12pin Receptacle, 90° Header DT04-12PX-XXXX 12pin Receptacle DT15-2P-XXXX 2pin Receptacle, 180° Header DT06-2S-XXXX 2pin Plug DT15-3P-XXXX 3pin Receptacle, 180° Header DT06-3S-XXXX 3pin Plug DT15-4P-XXXX 4pin Receptacle, 180° Header DT06-4S-XXXX 4pin Plug DT15-6P-XXXX 6pin Receptacle, 180° Header DT06-6S-XXXX 6pin Plug DT15-08PX-XXXX 8pin Receptacle, 180° Header DT06-08SX-XXXX 8pin Plug DT15-12PX-XXXX 12pin Receptacle, 180° Header DT06-12SX-XXXX 12pin Plug
Wedge Lock PN's sold separately but are required for DT functionality 2.2. Industry Documents DIN 40050-9: Road vehicles Degrees of Protection (l P Code) DIN 72551-6: Road Vehicles —Low-Tension Cables—Part 6: Single-Core, Unscreened with Thin Insulation Wall; Dimensions, Materials, Marking EIA-364: Electrical Connector/Socket Test Procedures Including Environmental Classific ations IEC-60512: Electronic Equipment - Tests and Measurements IEC-60529: Degrees of Protection Provided by Enclosures (IP Code) ISO 6722: Road Vehicles —60 V and 600 V Single-Core Cables—Dimensions, Test Methods, and Requirements SAE J1128: Low Voltage Primary Cable SAE J2030 : Heavy-Duty Electrical Connector Performance Standard DT16-6SX-XXXX 6pin Plug 2303812 2pin Receptacle, Snap Cap DT16-15SX-XXXX 15pin Plug 2303813 3pin Receptacle, Snap Cap DT16-18SX-XXXX 18pin Plug 2303815 2pin Plug, Snap, Cap 2303816 3pin Plug, Snap Cap DTF13-2PX-XXXX 2pin Receptacle, 90º Header, Flangeless DTF13-3PX-XXXX 3pin Receptacle, 90º Header, Flangeless DTF13-4PX-XXXX 4pin Receptacle, 90º Header, Flangeless DTF13-6PX-XXXX 6pin Receptacle, 90º Header, Flangeless DTF13-8PX-XXXX 8pin Receptacle, 90º Header, Flangeless DTF13-12PX-XXXX 12pin Receptacle, 90º Header, Flangeless DTF15-12PX-XXXX 12pin Receptacle, 180º Header, Flangeless W2P-XXXX 2pin Rcpt Wedge Lock W2SX-XXXX 2pin Plug Wedge Lock W3P-XXXX 3pin Rcpt Wedge Lock W3S-XXXX 3pin Plug Wedge Lock W4P-XXXX 4pin Rcpt Wedge Lock W4SX-XXXX 4pin Plug Wedge Lock W6P-XXXX 6pin Rcpt Wedge Lock W6S-XXXX 6pin Plug Wedge Lock W8P-XXXX 8pin Rcpt Wedge Lock W8S-XXXX 8pin Plug Wedge Lock W12P-XXXX 12pin Rcpt Wedge Lock W12S-XXXX 12pin Plug Wedge Lock 1011-344-0205 2pin Dust Cap 1011-345-0305 3pin Dust Cap 1011-346-0405 4pin Dust Cap 1011-347-0605 6pin Dust Cap 1011-348-0805 8pin Dust Cap 1011-349-1205 12pin Dust Cap
- REQUIREMENTS 3.1. Design and Construction Product shall be of the design, construction, materials and physical dimensions sp ecified on the applicable product drawing. 3.2. Ratings Voltage: 250 VAC/VDC Current (Amp) 14 AWG [2.00 mm²]: 13 A 16 AWG [1.00 mm²]: 13 A 18 AWG [0.80 mm²]: 10 A 20 AWG [0.50 mm²]: 7.5 A Temperature: -55°C to +125°C Ingress Protection (Inline) : IP68 and IP6K9K (with rear protection, such as backshell) Ingress Protection (Header): Not Tested Flammability (Inline) : UL Recognized. Parts are made out of V-0 material and have been successfully tested to the 12 mm Flame Test per Standard UL-94. Flammability (Header) : V-0 3.3. Test Requirements and Procedures Summary (Original Version) Unless otherwise specified, all tests shall be performed at ambient environmental condi tions. NOTE a) See Appendix A for Additional Test Requirements for Original Version b) See Appendix B for Test Requirements and Procedures Summary for Snap Cap Version c) See Appendix C for Procedure Comparison Chart VISUAL 3.3.1. Examination of Product A. Procedure: EIA-364- 18 B. Method: Visually inspected for use of materials, proper construction, correct part number and insert markings and over-all quality of workmanship. Poor molding fabrication, loose mater ials, damaged or improperly manufactured contacts, galling of metal parts, nicks and burrs of metal parts, torn seals or cracked plastic were considered adequate basis for rejection. C. Requirement: The connectors shall be correctly constructed, marked and shall show good qua lity and workmanship.
3.3.2. Insulation Resistance A. Procedure: MIL-STD-1344, Method 3003.1 B. Method: Using a 500 VDC megohmmeter check each contact to all other contacts and the shell electrically connected together. C. Requirement: 1000 MΩ minimum at 25C. 3.3.3. Dielectric Withstanding Voltage A. Procedure: MIL-STD-1344, Method 3001.1 B. Method: Check each contact to all other contacts and the shell electrically connected togethe r for breakdown / flashover when subjected to a 1500 VAC test potential for a period of 1 minute. C. Requirement: No evidence of breakdown or flashover or current leakage in excess of 2.0 milliampers. 3.3.4. Contact Resistance A. Procedure: MIL-STD-1344, Method 3004.1 B. Method: 15A for 16AWG C. Requirement: Maximum voltage drop across a 6 inch wire/contact assembly shall be 89mV max for 16AWG. 3.3.5. Contact Resistance A. Procedure: MIL-STD-1344, Method 3004.1 B. Method: 15A for 16AWG C. Requirement: Maximum voltage drop across a 6 inch wire/contact assembly shall be 89mV max for 16AWG. MECHANICAL 3.3.6. Maintenance Aging A. Procedure: MIL-STD-1344, Method 2002.1 B. Method: Subject 10% of the cavities to 10 cycles of inserting and removing its respective con tact. Insert by hand, remove using removal tool. C. Requirement: There shall be no visible change or damage to the contact cavities. 3.3.7. Contact Retention A. Procedure : MIL-STD-1344, Method 2007.1 B. Method: Subject each wired contact to an applied load of 25 lbf for a period of 15 seconds in a direction tending to push the contact out of the rear of the connector. C. Requirement: The contact shall remain in place 3.3.8. Durability A. Procedure: MIL-STD-1344, Method 2016 B. Method: The connector shall be mated and unmated for a total of 100 complete cycles at room temperature. C. Requirement: No evidence of damage to the contacts, contact plating, connector housing or seals which may be detrimental to reliable connector performance.
3.3.9. Vibration A. Procedure : MIL-STD-1344, Method 2005.1 B. Method: Sine Sweep: 10 to 2000 Hz Sweep Cycle: 20 minutes Initial Displacement: .07 inch DA Maximum Acceleration: 20G Test Duration: 12 hours Time Per Axis X, Y, Z: 4 hours Test Current first 3 hours each axis: 16 AWG: 13A C. Requirement: No discontinuity in excess of 1.0 μs at 100 mA during the last hour of each axis. Shall meet visual requirements, show no physical damage and meet requirements of additional tests as needed. 3.3.10. Shock A. Procedure : MIL-STD-1344, Method 2004.1 B. Method: 10 cycles of ½ sine pluses, 50g±15%, 11±1 ms duration X and Z axis are to be tested. C. Requirement: No discontinuity in excess of 1.0 μs at 100 mA during the last hour of each axis. Shall meet visual requirements, show no physical damage and meet requirements of additional tests as needed. ENVIRONMENTAL 3.3.11. Temperature Life A. Procedure : MIL-STD-1344, Method 1005.1 B. Method: The wired mated connectors shall be subjected to 100 hours at 125°C. Insulation resistance shall be measured immediately after removing sample from the oven. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Meet 500 MΩ minimum 3.3.12. Salt Spray A. Procedure : MIL-STD-1344, Method 1001.1 B. Method: Connector shall be fully mated, then submerged in a fine mist of 5% by weight of salt solution for 96 hour. C. Requirement: There should be no evidence of corrosion on the connector or terminals after the connector is removed from the test and cleaned with tap water. 3.3.13. Fluid Immersion A. Procedure : MIL-STD-1344, Method 1016 B. Method: Subject each connector to one fluid only. The wired mated connectors shall be submerged in the fluids below at ambient temperature. Each connector shall be submerged for 5 minutes, then removed from the fluid to air dry for 24 hours. This cycle is to be completed a total of 5 cycles. Motor Oil 30 weight Brake Fluid (disc type 1) Gasoline Diesel Fuel #2 Antifreeze Solution (Max Protection) Transmission Oil 90 weight C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test.
3.3.14. Thermal Shock A. Procedure : MIL-STD-1344, Method 1003.1 B. Method: Cycle mated connectors for 30 minutes at –55°C followed by 30 minutes at +125°C with 2 minute max transfer time. Repeat for 5 cycles. Insulation resistance measured during last heat cycle. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Meet 500 MΩ minimum 3.3.15. Moisture A. Procedure: Not Applicable B. Method: The wired mated connectors shall be immersed in 3 feet of water for 24 hours. C. Requirement: Connectors shall show no sign of moisture inside the cavities or connector interior.
3.4 Product Qualification and Requalification Test Sequence (Original Version)
a) Specimens shall be prepared in accordance with applicable Application Specificat ion and shall be selected at random from current production. b) Groups 1-6. Specimens shall consist of 3-position connectors with DEUTSCH solid termina l system size 16 nickel plated pin and socket contacts with 16 AWG GXL wire. c) Numbers indicate sequence in which tests are performed. TEST or EXAMINATION TEST GROUP (a) 1 2 3 4 5 6 TEST SEQUENCE (b) Examination of Product 1 1 1 1 1 1 Insulation Resistance 2 2 2 2 2 2 Dielectric Withstanding Voltage 3 3 3 3 3 3 Maintenance Aging 4 4 Temperature Life 4 4 4 Contact Retention 5 5 Durability 5 6 4 Salt Spray 6 7 5 Moisture 6 5 5 Fluid Immersion 7 7 8 6 6 6 Thermal Shock 8 8 7 Vibration 9 9 7 Shock 10 10 8 Contact Resistance 11 9 11 9 7 8 Final Examination 12 10 12 10 8 9
3.5 Appendix A. Additional Test Requirements (Original Version) ELECTRICAL 3.5.1. Low Level Contact Resistance A. Procedure: EIA-364- 23 B. Method: Test with applied voltage not to exceed 20 mV open circuit and the test current s hall be limited to 100 mA. The resistance of an equal length of wire (reference wire) shall be subtracted from the same reel as used for the connector wiring. C. Requirement: 16 AWG [1.00 mm²]: 6.0 mΩ max 18 AWG [0.80 mm²]: 7.5 mΩ max 20 AWG [0.50 mm²]: 11. 0 mΩ max 3.5.2. Contact Resistance A. Procedure: EIA-364-6 B. Method: Using test currents as defined. The resistance of an equal length wire (reference wire) shall be subtracted from the actual readings to determine the added resistance of the terminal. The reference wire shall be from the same reel as used for the connector wiring. Test Currents: 14 AWG [2.00 mm²]: 13A 16 AWG [1.00 mm²]: 13A 18 AWG [0.80 mm²]: 10A 20 AWG [0.50 mm²]: 7.5A C. Requirement: 60mV (Solids) and 100mV (S&F) voltage drop MECHANICAL 3.5.3. Vibration A. Procedure : Not Applicable B. Method: Sine Sweep: 10 to 2000 Hz Initial Displacement: 1.78 mm DA Maximum Acceleration: 20G Test Duration: 12 hours Time Per Axis X, Y, Z: 4 hours Test Current first 3 hours each axis: 14-16 AWG [2.00-1.00 mm²]: 10A 18 AWG [0.80 mm²]: 8A 20 AWG [0.50 mm²]: 5A C. Requirement: There shall be no discontinuity in excess of one (1) μs at 20mV and 100 mA during the last hour of each axis. Shall meet visual requirements, show no physical damage and meet requirements of additional tests as needed.
3.5.4. Impact A. Procedure: Not Applicable B. Method: Wired mated connector shall be dropped from a height of 1.2m on a cement floor. This action is to be completed a total of five (5) times. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Small chips and dents that do not adversely affect the connector shall be disregarded. 3.5.5. Contact Retention A. Procedure : Not Applicable B. Method: Apply a pulling force to the wire bundles that exit the rear of the connector for a period of one (1) minute. The amount of load is to be 111N, times the number of cavities, up to a maximum of 445N. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. ENVIRONMENTAL 3.5.6. Temperature Life A. Procedure : MIL-STD-202, Method 108, Test Condition D B. Method: The wired mated connectors shall be subjected to 1000 hours at +125 ±3°C without current flowing. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. 3.5.7. Fluid Immersion A. Procedure: Not Applicable B. Method: Subject each sample group to one fluid only. The wired mated connectors shall be submerged in the fluids below at the temperatures listed. Each connector shall be submerged for five (5) minutes, then removed from the fluid to air dry for 24 hours. This cycle is to be completed a total of five (5) cycles. Motor Oil 30 weight: +60±3°C Brake Fluid (disc type 1): +60±3°C Gasoline: +25±3°C Diesel Fuel #2: +60±3°C 50/50 Antifreeze/Water Mixture: +60±3°C Transmission Oil 90 weight: +60±3°C C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. 3.5.8. Thermal Cycle A. Procedure : Not Applicable B. Method: Cycle mated connectors from –55 ± 3°C to +125 ±3°C at a rate of 3°C ± 1°C per minute. Connectors to remain at each temperature extreme for one (1) hour minimum. Mated connectors are to be cycled a total of 20 complete cycles. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test.
3.5.9. Water Immersion A. Procedure: Not Applicable B. Method: The wired mated connectors shall be placed in an oven at +125 ±3°C for two (2) hours minimum then immediately be placed in water with a 5% salt by weight content and 0.1 g/L wetting solution to a depth of 914mm for four (4) hours minimum. The free ends of the mated connectors must remain out of the water to prevent wicking of the water through the open wires. Water temperature to be +23 ±3°C. C. Requirement: Test samples must meet Insulation Resistance.
3.6 Appendix B. Test Requirements and Procedures Summary (Snap Cap Version) VISUAL 3.6.1. Examination of Product A. Procedure: SAE J2030_201506 B. Method: Conduct a visual examination for identification of product, torn seals, cracked plas tic, etc. C. Requirement: The connectors shall be correctly constructed, marked and show good qualit y and workmanship. Connector after conditioning shall not show signs of damage or any detectable los s of function. ELECTRICAL 3.6.2. Insulation Resistance A. Procedure: SAE J2030_201506 B. Method: Using a 1000 VDC megohmmeter check the insulation resistance between each contac t to each adjacent contact. C. Requirement: > 20 MΩ 3.6.3. Connection Resistance A. Procedure: SAE J2030_201506 B. Method: The resistance of a cable equal in length to that of the two measuring points shall be subtracted from the measured values. The cable used shall be from the same batch of cable as used for the connector wiring. C. Requirement: Measurements shall be taken after thermal equilibrium at 15A. Voltage drops shall not exceed 100mV. MECHANICAL 3.6.4. Mating Force A. Procedure: SAE J2030_201506 B. Method: The maximum required force to mate the plug and receptacle pair and engage the latc hing mechanism. C. Requirement: F ≤ 135N 3.6.5. Un-Mating Force A. Procedure: SAE J2030_201506 B. Method: The maximum force required to separate the plug and receptacle with the latch mechanism fully disengaged. C. Requirement: F ≤ 135N 3.6.6. Maintenance Aging A. Procedure: SAE J2030_201506 B. Method: Subject at least 10% of the cavities to 10 cycles of inserting and removing its respec tive contact. The 10th cycle shall include any disassembly required to remove the contacts. The connectors shall be mated and unmated during each cycle. C. Requirement: There shall be no visible change or damage to the contact cavity 3.6.7. Durability A. Procedure: SAE J2030_201506 B. Method: The connector shall be mated and unmated for a total of 50 complete cycles. C. Requirement: No evidence of damage to the contacts, contact plating, connector housing or seals which may be detrimental to reliable connector performance.
3.6.8. Terminal Retention in Connector A. Procedure: SAE J2030_201506 B. Method: The contacts shall be subjected to a direct pull of 110N for 1 minute. The pull is to be exerted on the conductor by means of a tension-testing machine or equivalent to prevent sudden or jerking force during test. The terminal shall maintain its original position in the connector throughout the test. The secondary-locking device is needed. C. Requirement: The contact shall remain in place. 3.6.9. Connector Retention A. Procedure: SAE J2030_201506 B. Method: Apply a pulling force to the wire bundle of the mated connector. The load shall be appl ied for 30 seconds. C. Requirement: a. 2pin: 222N b. 3pin: 300N 3.6.10. Vibration A. Procedure: SAE J2030_201506 B. Method: Sine Sweep: 10 to 2000 Hz Max Acceleration: 20G Time Per Axis : 8 hours Test Duration: 24 hours Test Current: 13A first 3 hours each axis C. Requirement: No defects, cracks and no discontinuity greater than 10Ω >1 μs during the last hour of each axis 3.6.11. Drop A. Procedure: SAE J2030_201506 B. Method: The free end of the cord or cable, which shall be 1500 mm, shall be fixed to a wall a t a height of 750 mm above a concrete floor. The specimen shall be held so that the cord or cable is horizontal and allowed to fall to a concrete floor eight times. Rotate the specimens through approximately 45° at it fixing each time. C. Requirement: There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Small chips and dents that do not adversely affect the connector shall be disregarded. ENVIRONMENTAL 3.6.12. Temperature Life A. Procedure: SAE J2030_201506 B. Method: +125ºC for 1000 hours C. Requirement: No evidence of cracking, chipping, or other damage detrimental to the normal operation of the connector. 3.6.13. Thermal Shock A. Procedure: SAE J2030_201506 B. Method: Test samples were subjected to 10 cycles. One cycle consisted of a soak time at -55°C, then transitioned within 2 minutes to an ambient temperature of +125°C with a soak time, and then transition back to -55°C within 2 minutes. The soak times were established as the time necessary to bring the internal connector temperature on test to within 5°C of each of the ambient temperatures. C. Requirement: No evidence of cracking, chipping, or other damage detrimental to the normal operation of the connector.
3.6.14. Water Immersion A. Procedure: SAE J2030_201506 B. Method: The wired mated connectors shall be placed in an oven at +125°C for 1 hour then immediately be placed in water with a 5% salt in weight content and 0.1 g/L wetting agent, to a depth of 1 meter for 4 hours. Water temperature is to be 23°C. The ends of the cable are to be sealed during this test. C. Requirement: Must meet Insulation Resistance and visually inspect for moisture inside the connector. 3.6.15. Fluid Immersion A. Procedure: SAE J2030_201506 B. Method: Subject each connector to one fluid only in the cabled and mated condition. Submerge the mated connector in fluid per table below at the specified temperature ±3 °C for 5 minutes, then remove and allow to air dry for 24 h. This completes one cycle. Each connector is to be subjected to a total of five cycles. Inspect for damage after the test. C. Requirement: No evidence of cracking, distortion or detrimental damage to the connector.
3.7 Product Qualification and Requalification Test Sequence (Snap Cap Version)
TEST GROUP (a) 1 2 3 TEST SEQUENCE (b) Examination of Product 1,12 1,11 1,8 Insulation Resistance 2,10 2 Connection Resistance 3,6,8 3,10 Mating Forces 5 3 Un-mating Forces 6 4 Maintenance Aging 2 Durability 7 5 Terminal Retention in Connector 6 Connector Retention 7 Thermal Shock 4 8 Temperature Life 4 Vibration 5 Drop 7 9 Water Immersion 9 Fluid Immersion 11 NOTE a) Specimens shall be prepared in accordance with applicable Application Specificat ion and shall be selected at random from current production. b) Groups 1-3. Specimens shall consist of 2 and 3-position snap cap connectors with DEUTS CH stamped and formed terminal system size 16 nickel plated pin and socket contacts with 16 GXL wire. c) Numbers indicate sequence in which tests are performed.
3.8 Appendix C. Test Procedure Comparison Chart Test MIL-STD-1344 Method EIA-364 Dash No. Similar to SAE J2030 Paragraph Similar to ISO 8092-2 Paragraph Examination of product - 18 6.1 4.2 Insulation Resistance 3003.1 21 6.3 4.12 Dielectric Withstanding Voltage 3001.1 20 - 4.13 Low Level Contact Resistance 3002.1 23 6.2 4.8 Contact Resistance 3004.1 06 6.4 4.8 Maintenance Aging 2002.1 24 6.6 - Contact Retention 2007.1 29 6.18 4.7 Durability 2016 09 6.11 4.3 Vibration 2005.1 28 6.15 - Shock 2004.1 27 6.16 - Impact - 42 6.17 4.20 Connector Retention - - 6.20 - Temperature Life 1005.1 17 6.7 4.18 Salt Spray 1001.1 26 6.12 4.16 Fluid Immersion 1016 10 6.14 4.23 Thermal Cycle - - - - Thermal Shock 1003.1 32 6.13 4.22 Moisture - - - - Water Immersion - - 6.19 4.9
- REVISION HISTORY Rev Ltr Brief Description of Change Date Dwn Apvd A Initial Release 02-Mar-2015 RM DM B Fixed Section 3.3 19-Mar-2015 RM DM B1 Removed INLINE from part number table 09-Jun-2015 RM DM B2 Add new part numbers 24-Jul-2015 RM DM B3 Fix typo 30-Jul-2015 RM DM B4 Add dust cap part number table on sheet 1 for the plugs 28-Jun-2017 JA DM B5 Add Production Drawing table for DTF13 and 15 on sheet 2. 11-May-2018 JA DM C Revised and rewritten Added snap cap version 17-Apr-2020 DM DM D Page 1. Corrected hyperlinks Page 1, Sec 2.1. Added 114-151001, 114-151004, 502-151009 Page 3, Sec 3.2. Added (Inline) to Ingress Protection, Added Ingress Protection (Header) Page 3, Sec 3.2. Added (Inline) to Flammability, Added Flammability (Header) 11-May-2020 DM DM