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  Datasheet File OCR Text:
 Strain Reliefs
AS85049/52, MS3417, and M83723/15S Strain Reliefs
Glenair Connector Designator A MIL-DTL-5015 Series 3400, MIL-DTL-26482 Series 2, AS81703 Series 3, MIL-DTL-83723 Series I & III, 40M39569, DEF 5326-3, EN 2997, EN 3646, ESC 10, ESC 11, LN 29504, NFC93422 Series HE302, PAN 6432-1, PAN 6432-2, PATT 602
M85049/52 S 10 W Basic Part No. S = Self-Locking -1- = Non-Self-Locking Dash No. Material and Finish Designator A = Aluminum, Black Anodize N = Aluminum, Electroless Nickel W = Aluminum, 1,000 Hour Cadmium Olive Drab Over Electroless Nickel
MS3417-10 A Basic Part No. (Non-Self-Locking Only) Dash No.
SUPERCEDED SPEC.
Material and Finish Designator A = Aluminum, 1,000 Hour Cad. Olive Drab Over Electroless Nickel C = Aluminum, Cadmium Olive Drab G = Aluminum, Black Anodize N = Aluminum, Electroless Nickel
M83723/15S-10 A Basic Part No. (Non-Self-Locking Only) Dash No.
SUPERCEDED SPEC.
Finish Designator A = Non-Conductive, Black Anodize R = Conductive, Electroless Nickel
A Thread
F Self Locking Only
Cable Entry
E Dia Self Locking Only
G
(c) 2005 Glenair, Inc.
CAGE Code 06324
Printed in U.S.A.
GLENAIR, INC. * 1211 AIR WAY * GLENDALE, CA 91201-2497 * 818-247-6000 * FAX 818-500-9912 www.glenair.com E-Mail: sales@glenair.com 62-22
AS85049/52, MS3417, and M83723/15S Strain Reliefs
TABLE I
A Thread E Dia Max Dash Class 2B Self-Locking No. .562 - 24 UNEF n/a 3*+ .500 - 20 UNF .885 (22.5) 8 .625 - 24 UNEF 1.010 (25.7) 10 .750 - 20 UNEF 1.135 (28.8) 12 .875 - 20 UNEF 1.260 (32.0) 14 1.000 - 20 UNEF 1.385 (35.2) 16 1.062 - 18 UNEF 1.510 (38.4) 18 1.188 - 18 UNEF 1.635 (41.5) 20 1.313 - 18 UNEF 1.760 (44.7) 22 1.438 - 18 UNEF 1.885 (47.9) 24 2.135 (54.2) 28+ 1.750 - 18 UNS 2.395 (60.8) 32+ 2.000 - 18 UNS 2.635 (66.9) 36+ 2.250 - 16 UN 2.885 (73.3) 40+ 2.500 - 16 UN 3.135 (79.6) 44+ 2.750 - 16 UN 3.385 (86.0) 48+ 3.000 - 16 UN n/a 61*+ 1.500 - 18 UNEF * Not Available in Self Locking + Not Available under M83723/15S F Max Self-Locking n/a .73 (18.5) .85 (21.6) .98 (24.9) .98 (24.9) 1.10 (27.9) 1.35 (34.3) 1.48 (37.6) 1.60 (40.6) 1.73 (43.9) 1.88 (47.8) 2.13 (54.1) 2.44 (62.0) 2.63 (66.8) 3.00 (76.2) 3.40 (86.4) n/a G .020 (.5) .732 (18.6) .732 (18.6) .812 (20.6) .968 (24.6) 1.026 (26.1) 1.299 (33.0) 1.431 (36.3) 1.537 (39.0) 1.633 (41.5) 1.755 (44.6) 2.000 (50.8) 2.366 (60.1) 2.476 (62.9) 2.546 (64.7) 2.840 (72.1) 3.324 (84.4) 1.755 (44.6) Cable Entry Max Min .204 (5.2) .125 (3.2) .204 (5.2) .125 (3.2) .286 (7.3) .187 (4.7) .416 (10.6) .291 (7.4) .476 (12.1) .351 (8.9) .626 (15.9) .501 (12.7) .706 (17.9) .518 (13.2) .831 (21.1) .581 (14.8) .956 (24.3) .644 (16.4) 1.081 (27.5) .706 (17.9) 1.187 (30.1) .750 (19.1) 1.250 (31.8) .875 (22.2) 1.375 (34.9) .938 (23.8) 1.500 (38.1) .938 (23.8) 1.750 (44.5) 1.188 (30.2) 1.875 (47.6) 1.312 (33.3) 1.081 (27.5) .706 (17.9)
1. For complete dimensions see applicable Military Specification. 2. Metric dimensions (mm) are indicated in parentheses. 3. Cable Entry is defined as the accomodation entry for the wire bundle or cable. Dimensions are not intended for inspection criteria.
(c) 2005 Glenair, Inc.
CAGE Code 06324
Printed in U.S.A.
GLENAIR, INC. * 1211 AIR WAY * GLENDALE, CA 91201-2497 * 818-247-6000 * FAX 818-500-9912 www.glenair.com E-Mail: sales@glenair.com 62-23
Strain Reliefs


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