Stainless Steel s
Stainless Steel s Nuts Nuts for use with alloy steel s New S SH Nut Code Old S SH escription AN365 self-locking, cadmium-plated steel with non-metallic insert AN363 self-locking high-temperature, cadmium-plated, steelplated nut ecommended Use For applications up to +250 F (+121 C) For applications up to +550 F (+287 C) s Eaton s Aeroquip straps are made for use on many tie-down and equipment holding applications. imum radius is that recommended to be used at the corners of objects. The latch should be located about the curvature when possible rather than on the flat. Ample wrench clearance should be provided at the nut end of the latch. oop end types are designed for use with clevis pins or bolts; the slotted loop ends are for use with eye bolts and pins. olts Nuts for use with stainless steel s New M Nut Code Old ST NONE escription MS103C plain hex; silver plated stainless steel with lockwire hole ESNA Z1200J self-locking high temperature silver plated stainless steel special ecommended Use For applications up to +800 F (+426 C) For applications up to +1200 F (+648 C) All bolts have UNJF-3A Threads Important rawing Note: s are shipped either on the trunnion or side of the latch depending on the latch assembly; therefore, care must be taken to pair even (or odd) series numbers so the complete unit will contain a. Strength ata and Material MI-S-5059 Comp 301 ½-Hard Steel and Yield Strength, lbs. in Hundredths Inches 62 75 88 100 112 125 138 150 1364 1650 1936 2200 2062 2420 2750 3090 3438 3795 4125 olt Material: A286 CES per AMS 5732/5737 olt Strength: Yield = 3200 lbs. ¼ 28 Yield = 5824 lbs. AN Pin-Flat Head (Clevis) in ouble Shear 3/16 = 4140 lbs. ¼ = 7360 lbs. 3 /8 = 16575 lbs. AN Eye olt Yield Strength: AN42 ( olt 3 /16 Pin) = 800 lbs. AN43 ( olt 3 /16 Pin) = 1800 lbs. AN44 ( 5 /16-24 olt ¼ Pin) = 3000 lbs. AN46 ( 3 /8-24 olt 3 /8 Pin) = 5375 lbs. 2 EATON Aerospace Group TF100-27 April 2013
Stainless Steel Engineering ata oop End/ atch Spotwelds Nut (Type). Pin oop ia *All dimensions in inches. 2330 2334 2338 2332 2336 2340 2430 2434 2438 2432 2436 2440 oop ia. olt 1 2 1 2 2 2 1 1 3 3 3 3 oop End/ Coupler atch Coupler Spotwelds Nut (Type) Pin oop ia. Coupler *All dimensions in inches. 2331 2335 2333 2337 2431 2435 2433 2437 oop ia. 2339 2341 2439 2441 olt 1 2 1 2 2 2 1.313 1.688 1.313 1.688 1 2.563 1 2.563.188.188 3 3 3 3 oop End Slotted/ atch Nut. Spotwelds (Type) 3 Pin oop ia *All dimensions in inches. 2360 2364 2368 2362 2366 2370 2460 2464 2468 2462 2466 2470 oop ia. olt 1 2 1 2 2 2 1 1 EATON Aerospace Group TF100-27 April 2013 3
Stainless Steel Engineering ata oop End Slotted/ Coupler atch Coupler Spotwelds Nut (Type). 3 Coupler Pin oop ia *All dimensions in inches. 2361 2365 2363 2367 2461 2465 2463 2467 oop ia. 2369 2371 2469 2471 1 2 1 2 2 2 1 1 Plain End/ atch Spotwelds (Type) Nut. All dimensions in Inches 2300 2302 2304 2400 2402 2404 olt 1 2 2 1.282 Plain End/ Coupler atch All dimensions in Inches Nut Coupler. Spotwelds (Type) Coupler 2301 2303 2401 2403 olt 2305 2405 1 2 2 1.313 1.688 1 2.563.188 4 EATON Aerospace Group TF100-27 April 2013
Ordering Information *Part Number Example: 2302-62 - 550 S Notes: Code: A,C, or = A286 bolt (In hundredth inches: 100=1.00 inch) Pad: = No Pad P =.060 Thick Cork-ubber Pad Per AMS-6841 (Example: 2303-62P55OS) 1. Specify all widths in one of the following available sizes: 2300 series/52,62, 75, 88, 100, 112, 138, 150, 162, 175, 188, 200, 212, 225. 2400 Series/75, 88, 100, 112, 125, 138, 150, 162, 175, 188, 200, 212, 225, 238, 250. 2. Specify all lengths in even.06 inch increments. For minimum lengths, see charts for specific part number. 3. When pad is specified, pad width will be same as strap width. * Order one of each assembly to make to make a complete strap unit or see ordering note on cover. (In hundredth inches: 100= 1.00 inch) Nut (See cover for coding) EATON Aerospace Group TF100-27 April 2013 5
Weight ata Weight in Pounds.150.100.050 2300 Series Weight Graph Add weight factor from table below to values from chart 1 7/8 3/4 5/8 and Inches Weight in Pounds.300.200.100 2400 Series Weight Graph Add weight factor from table below to values from chart 1-1/2 1-3/8 1-1/4 1-1/8 1 7/8 3/4 and Inches 1.88 5 10 15 20 in in Inches Inches 2 5 10 15 20 in Inches in Inches Series 2300 +.000 Weight Factor ue to Component Hardware bs. Series 2400 +.024 Weight Factor ue to Component Hardware bs. 2301 2401.075 2302.017 2402.053 2303.029 2403.088 2304.021 2404.064 2305.003 2405.000 2330; 32.010 2430; 32.047 2331; 33.028 2431; 33.098 2334; 36.027 2434; 36.076 2335; 37.032 2435; 37.111 2338; 40.031 2438; 40.087 2339; 41.012 2439; 41.023 2360.009 2460.045 2361.034 2461.096 2362.008 2462.041 2363.033 2463.092 2364.026 2464.075 2365.038 2465.109 2366 2466.070 2367.037 2467.105 2368.030 2468.086 2369.011 2469.022 2370.029 2470.081 2371.010 2471.017 All weights are figured less pad. For weight assembly with pads, consult Eaton. 6 EATON Aerospace Group TF100-27 April 2013
Eaton Aerospace Group Fluid & Electrical istribution ivision 90 Clary Connector Eastanollee, Georgia 30538 Phone: (706) 779 3351 Fax: (706) 779 2638 Eaton Aerospace Group 9650 Jeronimo oad Irvine, California 92618 Phone: (949) 452 9500 Fax: (949) 452 9555 www.eaton.com/aerospace Copyright 2013 Eaton All ights eserved Copying or Editing is Forbidden Form No. TF100-27A (Supersedes AA33) April 2013