S: part s4 44 440H 120-1OF2.prt 440H*120 REVISIONS SYM. DESCRIPTION DATE APPROVED C A RELEASED 11/02/07 T.L. B REVISED PER DCN 29177 T.L. 03/13/08 .474 MAX TYP .247 .329 .015 MIN TYP F .065/.025 4 TYP INTERFACE I.A.W MIL-C-38999 (TYP) B TYP SYM S STRAIGHT KNURL STYLE MFR OPTION - TYP 4 .094 DIA DRAIN HOLE(4 90) TYP A THREAD H D TYP G J TYP SYM W E SYM T 90 .010 45 MIN TYP .365 .008 MAX 4 F MIN SPLIT THRU TOOTH ROOT SYM TX, 45, .008 MAX SPLIT OPTION SPLIT THRU F TOOTH ROOT THIS COPYRIGHTED DOCUMENT IS THE PROPERTY OF GLENAIR, INC. AND IS FURNISHED ON THE CONDITION THAT IT IS NOT TO BE DISCLOSED, REPRODUCED IN WHOLE OR IN PART, OR USED TO SOLICIT QUOTATIONS FROM COMPETITIVE SOURCES, OR USED FOR MANUFACTURE BY ANYONE OTHER THAN GLENAIR, INC. WITHOUT SYM WX, 90, WRITTEN PERMISSION FROM GLENAIR, INC. THE INFORMATION HEREIN HAS BEEN DEVELOPED AT GLENAIR S EXPENSE AND MAY BE USED FOR ENGINEERING EVALUATION AND INCORPORATION INTO TECHNICAL SPECIFICATIONS AND OTHER DOCUMENTS WHICH SPECIFY PROCUREMENT OF PRODUCTS FROM GLENAIR, INC. SPLIT OPTION C DRAWN T. LE 04/21/03 CAD 2003 UNLESS OTHERWISE SPECIFIED CHECK R. PAINTER 04/21/03 DIMENSIONS ARE IN INCHES ENGR T. YOUNG 04/21/03 1211 AIR WAY - GLENDALE - CALIFORNIA 91201 TOLERANCES: ADAPTER, BANDING, RFI/EMI, + 1/16 FRACTIONS - BOEING ONLY APPROVED STRAIN RELIEF FOR MIL-DTL-38999 + .XX .03 - DECIMALS 5M2919, 5M2920, 5M2953 + .XXX .015 SERIES III & IV CONNECTORS - 2 + ANGLES 2 - APPROVED CODE IDENT. NO. REV. SIZE RELEASE DATE 11/02/07 DO NOT SCALE THIS DRAWING ORIGINAL 06324 440H*120 C B RELEASE DATE B/F 98-5746 P/C 44 NON REPARABLE COMMERCIAL ITEM SCALE N/A WEIGHT N/A SHEET 1 OF 2 1 of 1 S: part s4 44 440H 120-2OF2.prt 440H*120 TABLE I REVISIONS SYM. +.03 DESCRIPTION DATE APPROVED SHELL C MAX E MAX F CABLE DIA G H J A THREAD B D SEE SHEET 1 -.06 ISO METRIC DIM DIM MAX MAX MAX SIZE MAX MIN MAX DIM M12 X 1.0 - 6H .594 1.46 .66 1.02 .203 .094 .65 .470 1.02 09 M15 X 1.0 - 6H .718 1.46 .482 1.07 11 .69 1.07 .250 .141 .76 13 M18 X 1.0 - 6H .844 1.46 .75 1.13 .323 .172 .89 .494 1.13 M22 X 1.0 - 6H 1.000 1.46 .86 1.33 .203 1.04 .530 1.33 15 .422 1.188 .557 17 M25 X 1.0 - 6H 1.46 .94 1.40 .500 .234 1.14 1.40 M28 X 1.0 - 6H 1.218 1.46 1.00 1.46 .562 .265 1.28 .576 1.46 19 1.344 .600 21 M31 X 1.0 - 6H 1.54 1.07 1.61 .625 .297 1.40 1.61 M34 X 1.0 - 6H 1.469 1.54 1.15 1.66 .703 .328 1.51 .627 1.66 23 M37 X 1.0 - 6H 1.594 1.54 1.21 1.72 .359 .653 1.72 25 .765 1.63 TABLE II SYM FINISH DESCRIPTION B CADMIUM PLATE/OLIVE DRAB PART NUMBER DEVELOPMENT GOLD IRIDITE OVER CADMIUM J PLATE OVER NICKEL EXAMPLE: 440 H S 120 NF 21 M ELECTROLESS NICKEL CADMIUM PLATE/OLIVE DRAB N OVER NICKEL PRODUCT SERIES CAD/O. D. OVER ELECTROLESS NF NICKEL (500 HOUR SALT SPRAY) CONNECTOR DESIGNATOR, CADMIUM PLATE/BRIGHT DIP T H = MIL-DTL-38999 OVER NICKEL SER, III & IV 300 SERIES STAINLESS STEEL, Z1 PASSIVATE, QQ-P-35 ANGULAR FUNCTION, XM ELECTROLESS NICKEL S = STRAIGHT W = 90 T = 45 WX = 90, SPLIT OPTION TX = 45, SPLIT OPTION BASIC NO FINISH SYM, TABLE II SHELL SIZE, TABLE I BOEING ONLY 5M2919, 5M2920, 5M2953 NOTES: 1. ASSEMBLY IDENTIFIED WITH MANUFACTURER S NAME AND P/N, SPACE PERMITTING. THIS COPYRIGHTED DOCUMENT IS THE PROPERTY OF GLENAIR, INC. AND IS FURNISHED ON THE CONDITION THAT IT IS NOT TO BE DISCLOSED, REPRODUCED IN WHOLE OR IN PART, OR USED TO SOLICIT QUOTATIONS FROM COMPETITIVE SOURCES, OR USED FOR MANUFACTURE BY ANYONE OTHER THAN GLENAIR, INC. WITHOUT WRITTEN PERMISSION FROM GLENAIR, INC. THE INFORMATION HEREIN HAS BEEN DEVELOPED AT GLENAIR S EXPENSE AND MAY BE USED FOR ENGINEERING 2. FOR EFFECTIVE GROUNDING, CONNECTOR WITH CONDUCTIVE FINISH EVALUATION AND INCORPORATION INTO TECHNICAL SPECIFICATIONS AND OTHER DOCUMENTS WHICH SPECIFY PROCUREMENT OF PRODUCTS FROM GLENAIR, INC. C SHOULD BE USED. DRAWN T. LE 04/21/03 CAD 2003 UNLESS OTHERWISE SPECIFIED CHECK R. PAINTER 04/21/03 3. GLENAIR 600 SERIES BACKSHELL ASSEMBLY TOOLS ARE RECOMMENDED DIMENSIONS ARE IN INCHES ENGR T. YOUNG 04/21/03 1211 AIR WAY - GLENDALE - CALIFORNIA 91201 FOR ASSEMBLY AND INSTALLATION. TOLERANCES: ADAPTER, BANDING, RFI/EMI, 4 ACCOMMODATES 600-083 MICRO BAND. + 1/16 FRACTIONS - APPROVED STRAIN RELIEF FOR MIL-DTL-38999 + .XX .03 - DECIMALS 5. MATERIAL/FINISH: + SERIES III & IV CONNECTORS .XXX .015 - 2 COUPLING NUT - AL ALLOY, QQ-A-225/B ASTMB221 OR STAINLESS STEEL, + ANGLES 2 - APPROVED CODE IDENT. NO. SIZE REV. QQ-S-763/ASTMB484 OR COMPOSITE/SEE TABLE II. RELEASE DATE 11/02/07 STRAIN RELIEF - THERMOPLASTIC, PPS (RADEL-R5100, COLOR BLACK) DO NOT SCALE THIS DRAWING ORIGINAL 06324 440H*120 C B RELEASE DATE B/F 98-5746 P/C 44 NON REPARABLE COMMERCIAL ITEM SCALE N/A WEIGHT N/A SHEET 2 OF 2 1 of 1