NSN 5340-01-259-4151

Part Details | LOOP CLAMP

5340-01-259-4151 A clamp designed to surround other item(s) such as cable(s), conduit(s), pipe(s), hose(s), or tube(s), and to fasten together or to another object or structure. Includes straight flexible items. For items specifically designed to clamp a hose to a connection to prevent leakage, see CLAMP, HOSE. See also HANGER, PIPE and CLIP, SPRING TENSION. For retaining straps with a bridge, see STRAP, RETAINING. Excludes CLAMP, ELECTRICAL; BAND, RETAINING; CLAMP (1), C; BRACKET PIPE.

Alternate Parts: 674938705, 6749387-05, 6494121040, 649-412-104-0, J1220G06, J1220G06, J1220G06, J1220G06, J1220G06, J1220G06, 5340-01-259-4151, 01-259-4151, 5340012594151, 012594151

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53JUL 17, 198701-259-415117532 ( CLAMP, LOOP )
REFERENCE DRAWINGS & PICTURES

OFFSET MOUNT

Cross Reference | NSN 5340-01-259-4151
Part Number Cage Code Manufacturer
6749387-0573342ALLISON TRANSMISSION, INC.
649-412-104-058828CFM INTERNATIONAL, INC.
J1220G0658828CFM INTERNATIONAL, INC.
J1220G0607482GENERAL ELECTRIC COMPANYDBA GE
J1220G0622175J & M PRODUCTS, INC.
J1220G063G1W3KLX AEROSPACE SOLUTIONS DEFENSE LLCDBA KLX AEROSPACE SOLUTIONS DEFENSE
J1220G0683930TRANSDIGM INCDBA ADEL WIGGINS GROUP-COMMERCIAL
J1220G0618076UMPCO, INC.
Technical Data | NSN 5340-01-259-4151
Characteristic Specifications
STYLE DESIGNATOR OFFSET MOUNT
OVERALL WIDTH12.32 MILLIMETERS MINIMUM AND 13.08 MILLIMETERS MAXIMUM
MATERIAL THICKNESS0.69 MILLIMETERS MINIMUM AND 0.94 MILLIMETERS MAXIMUM
CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE14.6 MILLIMETERS MINIMUM AND 15.9 MILLIMETERS MAXIMUM
DISTANCE FROM LOOP CENTER TO TONGUE END19.88 MILLIMETERS MINIMUM AND 21.69 MILLIMETERS MAXIMUM
LOOP INSIDE DIAMETER12.06 MILLIMETERS NOMINAL
TONGUE HOLE TYPE ROUND, UNTHREADED
DIAMETER5.05 MILLIMETERS MINIMUM AND 5.30 MILLIMETERS MAXIMUM
ENVIRONMENTAL ATTRIBUTE CODE ASBESTOS ALTERNATIVE PRODUCTS
END ITEM IDENTIFICATIONW/S: AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT, TF34-GE-100(A-10); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-1235H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT, GALAXY C-5; ENGINE, AIRCRAFT, GE T-700 (UH-60A); AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); ENGINE, AIRCRAFT, F-108 (CFM-56, KC-135A)