Rolex Science: Spareparts (2)

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Rolex Science: Spareparts (2)

  1. 1. 09RolexCvrR3 9/3/09 8:57 AM Page 1
  2. 2. 09RolexCvrR3 9/3/09 8:57 AM Page 2 A message from General Manager MW Industries serves Ways to contact You can always rely on Rolex Spring... market leaders in Rolex Spring... Steven C. Krajewski industries such as… Mail Dear Rolex Spring Customer, Rolex Spring is a leading manufacturer Agricultural We at Rolex Spring are proud to introduce our 2009 Catalog, of disc springs with our first completely re-designed catalog in a very long time! It is an extensive Automotive just one of the many exciting changes we have made her e, all inventory and custom of which are intended to help us better serve you. manufacturing 8900 Kelso Drive capabilities. For forty Auto Racing Baltimore, MD 21221 We have relocated our production facility to our sister years Rolex Spring division, Maryland Precision Spring in Baltimore, Maryland, has been serving such industries as aviation/aer ospace, and have used this move as an opportunity to invest in new transportation, machining and construction and many mor e. Aviation PHONE production and heat treating equipment. Applying the Aerospace principles of Lean Manufacturing and Six Sigma, we have Rolex Spring provides: also streamlined and optimized our manufacturing pr ocesses across the board. s Large disc spring inventory Computers Since our founding in 1969, you can continue to r ely on Rolex s Custom manufacturing Spring for— Electrical 410-391-7400 s Exacting quality standards and certifications s Rolex Spring is just as committed to quality today as we s Metric and standard sizes were in 1996 when we were the first disc spring Energy manufacturer to achieve QS and ISO certifications. s ODs from 1/4" to 40" FAX s We offer design and engineering support – fr om drawing s Outstanding customer service and technical support Hand and Power board to installation – for your applications. Tools Rolex Spring is proud to be a part of Maryland Pr ecision s Our manufacturing expertise enables us to work in all Spring. Both businesses are members of the MW Industries grades and types of steel, in addition to specialty family of companies. Heavy Trucks metals. 410-687-9223 s We provide assembly and packaging services, including Transportation stacking, to meet your needs. WEB s We are not limited to the pr oducts you see in this catalog! We can custom manufacture to your Medical requirements and can match other manufactur ers’ standard designs as well. Terms: Maryland residents add 6% Off-Road We think you will be impr essed with our new catalog! You can or appropriate tax for your district. Machinery also visit us online at www.mw-ind.com/rolex. We are proud Prices are subject to change without mw-ind.com/rolex notice; FOB, Baltimore, M D. of our past, but equally excited about our futur e. Speaking for Outdoor Power all of us at Rolex Spring, we would like to thank you for your support and we look forward to serving you! All damage claims must be filed by Equipment EMAIL consignee within 30 days of receipt. Retail Products We accept: Display Fixtures Steve Krajewski Telecommunications rolexspring@mw-ind.com General Manager
  3. 3. 09RolexCatalogR3 9/4/09 11:30 AM Page 1 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex TABLE OF CONTENTS About Rolex Products & Services ...............2-3 NDS Series ..............................................21-22 Standard Springs ............................................3 AK Series Lookup Tables ..............................23 Spring Measurement & Function ....................4 AK Series (MM & KGF) ............................24-25 AM Series Tolerances .....................................5 AK Series (Inches & Pounds) ...................25-26 AM Series (MM & Newtons).........................6-9 Disc Spring Applications .........................27-28 AM Series (Inches & Pounds) ..................10-13 Design Info: Characteristics ..........................29 AI & AK Series Tolerances.............................14 Design Info: Load Calculations .....................30 AI Series...................................................15-16 Design Info: Loading & Fatigue ...............31-32 SP Series.......................................................17 Design Info: Stacks .......................................33 Contact Belleville Springs .............................18 Design Info: Disc Spring Properties..............34 Contact Belleville Springs - Military ..............19 Design Info: Tightening Torque .....................35 FL Series .......................................................20 Request For Quote........................................36 WARRANTY Maryland Precision Spring Division, the manufactur ers be liable for loss of use of a pur chaser’s equipment or of ROLEX Precision Disc Springs, sells these products facilities, or for loss of business, goodwill or pr ofits, or on the condition that the purchaser will make their own for costs of inspection, transportation, storage, or any determination as to the pr oducts’ suitability for their other incidental damages. Pur chaser must notify intended use. The pur chaser agr ees to this and Maryland Pr ecision Spring Division in writing of any accepts all r esponsibility for the use of ROLEX products considered defective within 30 days of r eceipt Precision Disc Springs. of products. Maryland Pr ecision Spring Division warrants that Maryland Pr ecision Spring disclaims any and all ROLEX Springs ar e fr ee fr om defects in material and expressed or implied warranties concer ning ROLEX workmanship. Our sole obligation for any br each of this Precision Disc Springs including, without limitation, warranty is the r epair or r eplacement of the pr oduct, at warranty of fitness for a specific purpose and warranty of our option. Maryland Precision Spring Division shall not merchantability, except the warranty set forth above. Note: Part numbers and dimensions throughout this ca talog are subject to manufacturer’s change without notice. Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 1
  4. 4. 09RolexCatalogR3 9/4/09 11:30 AM Page 2 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex ABOUT ROLEX MPS/ROLEX SPRING Manufacturing precision disc springs since 1969. OUR PRODUCTS s MPS/Rolex Spring makes Belleville springs and disc s We have complete contr ol over all aspects of the springs fr om a variety of materials in sizes ranging manufacturing pr ocess. Our plant in Baltimor e, MD from 1/4" OD to 40" OD. includes tooling, stamping, machining, heat tr eating and finishing capabilities. s We stock a number of “catalog” parts or can make parts to your design specifications. s We have experience making parts fr om many specialty materials. s Our pr oducts ar e suitable for obtaining high spring loads in limited space. s We ar e well suited to supply custom engineer ed springs for all of your applications. s We make parts for use with pr etensioning bolted connections, for shock absorption, for vibration dampening, for friction devices, for live loading ball OUR SERVICES bearings, and many other design applications. s Complete design and engineering support. s Our parts are used in the Aerospace, Transportation, s Fast shipment of product from our extensive catalog Material Handling, Chemical Pr ocessing Equipment, part inventory. Mining and Oil Field Equipment, Machine T ool, s Complete manufacturing support for custom parts. Electrical Connector , V alve and many other industries. s Stocking programs for “just in time” deliveries. s Assembly and packaging services, including stacking. OUR QUALIFICATIONS s MPS/Rolex Spring is a leader in the design and s Quality control system support including certification, manufacture of disc springs. W e have a history material traceability, PPAP, etc. dating back to 1969. s We wer e the first disc spring manufactur er in the world to hold an ISO 9001 Quality System Certification. We currently maintain our registration to We are not limited to manufacturing springs listed in this ISO 9001:2000. catalog. W e have the knowledge, experience, and capability to produce springs to fit most any application. s We employee proprietary computer design programs Please contact our Sales Department for help with your to evaluate spring parameters to insur e acceptable custom applications. performance of our products in customer applications. Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 2
  5. 5. 09RolexCatalogR3 9/4/09 11:30 AM Page 3 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex ADDITIONAL SERVICES OFFERED BY MPS/ROLEX SPRING COMPLETE DISC SPRING ASSEMBLIES MADE PRE-STACKED PACKAGED DISC SPRINGS TO YOUR SPECIFICATIONS OR ASSEMBLED s Pre-stacked. pre-arranged assemblies TO COMPONENTS SUPPLIED BY YOU s Parallel and series combinations s Captive disc spring arrangements s Eliminate errors and labor caused s Guide rods, end restraints by manual stacking s Springs are stacked at our facility s Easy to handle, quick to install s Exact positioning and performance are factory tested on the pr emises Stack Spring Tension Device Typical Stack Assembly STANDARD SPRINGS Load Damping Spring Assembly Computer Spindle Drive Assembly Standard Springs s AM Series are precision springs geared to the metric s FL (inch) and MFL (metric) series flange springs ar e community and manufactured utilizing DIN 2092 and primarily designed for pipe flange applications. They DIN 2093 as guidelines. AM series springs ar e are intended to deflect and move with the bolted designed to meet high performance r equirements of joint in the event of thermal and/or mechanical dynamic spring applications. They ar e typically shock. Applications include piping construction, manufactured from High Carbon or Alloy steel; AISI compression joints, steam piping joints, valve and C1075 or 6150 material. pump connections, and other similar applications. The FL and MFL series ar e normally manufactur ed s AI Series springs ar e designed to maintain load from 17/7 PH stainless steel. tension in light bolted assemblies, wher e a constant load is r equired. Although this series is primarily s NDS Series flange springs ar e used to fill the designed for bolted applications, they may also be application needs similar to those described for the used in dynamic applications as long as the FL and MFL series springs. However , they ar e application does not exceed the designated str ess primarily designed to handle applications limits. Like the AM series the AI parts ar e typically demanding much higher load and/or temperatur e. manufactured from High Carbon or Alloy steel; AISI NDS parts ar e normally made fr om H11/H13 steel C1075 or 6150 material. and can pr oduce flat loads up to 310,000 pounds and, under most conditions, can withstand s SP Series are specifically designed for heavy bolted temperatures up of 1100° F (500° C). applications such as those r equired for bus bar and transformer applications. They ar e used wher ever s AK Series springs ar e specifically designed as there is a need to over come the ef fects of thermal preloading springs for use with radial ball bearings. expansion and contraction. The SP series ar e They ar e made fr om C1075 material and ar e normally manufactur ed fr om High Carbon or Alloy intended to maintain the positioning accuracy of the steel; AISI C1075 or 6150 material. bearing with no endplay and minimize vibration and shaft deflection. AK series springs ar e intended to meet both Metric and Inch standar d sizes. Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 3
  6. 6. 09RolexCatalogR3 9/4/09 11:30 AM Page 4 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex BASIC INFORMATION FOR MEASUREMENT AND FUNCTION OF A DISC SPRING CONICAL SPRING NOMENCLATURE OF A CONICAL SPRING OD = Outside Diameter ID = Inside Diameter t or TH = Thickness OH = Overall Height h or d = Cone or Dish Height 3 SPRINGS IN PARALLEL PARALLEL SPRING STACK Springs in parallel incr ease the potential for ce by the number of springs being used. 3 springs in parallel = 3 x the for ce of one If one spring can develop 100 pounds of clamping force, degree of accuracy because friction will cause risers in 3 in parallel can develop 300 pounds of clamping for ce. loads during the compr ession phase and dips in loads during the r eleasing phase. These ar e caused by a The potential to develop a high coef ficient of friction surface friction grabbing ef fect that pr events the exists in a parallel stack due to the friction that is cr ated e surfaces moving smoothly acr oss each other. The effect on the surface contacts. Stacks larger than three tend to tends to be pr esent in both the compr ession and develop a high, unpr edictable, coef ficient of friction. A releasing cycles. stack lar ger then thr ee can not be pr edicted with any 6 SPRINGS IN SERIES If one spring can develop 100 pounds of clamping for ce at 75% of its travel height, then 6 (or mor e) springs will produce the same 100 pounds for ce at 75% of the total travel distance of the stack. If a single spring, at .020" travel, is 75% deflection and develops 100 pounds of for ce, then a series stack of 6 will need to travel 6 times the deflection distance or .120", 75% of the stack travel height, to pr oduce the same 100 pounds of force. The formula is: Stack height = Single spring height x the number of springs in the stack. SPRING INFO Unlike the parallel stack, the coef ficient of friction plays less a roll in a series stack. However, larger series stacks made of numbers gr eater than ten, tend to develop an SERIES SPRING STACK unpredictable coef ficient of friction ar ound the contact Springs stacked in series increase the travel of the spring edges that make it dif ficult to pr edict the accuracy of by the number of springs in the stack while r etaining the load points. These tend to be identified as sticking points potential force of only one across the span of the stack. and can pr oduce a gripping or popping sound as the Example: 6 springs in series will allow the springs to stack moves through the compression cycle. Numerous travel 6 times the distance of a single spring while preventive measures such as lubricants, a lar ger radius retaining the potential force of only one. or bearing flats may be specified to aid in r educing these effects. Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 4
  7. 7. 09RolexCatalogR3 9/4/09 11:30 AM Page 5 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex AM/SAM SERIES PRECISION SPRING TOLERANCES The tolerances on this page are for the AM (AISI 1075 or AISI 6150 carbon steel) and SAM (17/7 PH stainless steel) series parts. THICKNESS (t) TOLERANCE TOLERANCES Refer to the “SAM” columns for dimensional and/or tolerance differences Carbon Steel AISI C1075 or AISI 6150 required for ALL 17/7 PH stainless steel parts. AM Series (MM) AM Series (Inches) Range Tolerance Range Tolerance ALL stainless steel ma terials will utilize these SAM specifica tions with the exception of materials not a vailable in the standard tolerance range. In those < 0.70 - 0.025 < 0.0276 ± 0.001 cases, the closest material tolerance will be used. > = 0.70 > = 0.0276 ± 0.051 ± 0.002 < 2.25 < 0.088 When requesting parts made of stainless steel, add the letter “S” in front of the > = 2.25 > = 0.088 existing part number . For example, carbon steel part number AM-502520 ± 0.076 ± 0.003 < 3.00 < 0.118 becomes SAM-502520 for stainless steel. > = 3.00 > = 0.118 ± 0.102 ± 0.004 < 4.00 < 0.157 For a vailability of other ma terial types and achievable tolerances, please call > = 4.00 ± 0.127 > = 0.157 ± 0.005 Rolex Sales or Engineering for assistance. Design Note : stainless steel ma terial thickness is different than steel and is subject to commercial availability. The overall height will be used to compensate for the difference in load due to the difference in thickness. THICKNESS (t) TOLERANCE 17/7 PH Stainless Steel OUTSIDE & INSIDE DIAMETER TOLERANCE SAM Series (MM) SAM Series (Inches) Range Tolerance Range Tolerance AM Series (MM) SAM (MM) AM SERIES (Inches) SAM (Inches) Carbon Steel Stainless Carbon Steel Stainless < = 0.51 ± 0.05 < = 0.020 ± 0.002 > 0.51 > 0.020 Range Tolerance Tolerance Range Tolerance Tolerance ± 0.08 ± 0.003 < = 1.27 < = 0.050 ID + 0.102 ID + 0.13 ID + 0.004 ID + 0.005 > 1.27 > 0.050 < = 3.0 < = 0.118 ± 0.10 ± 0.004 OD - 0.102 OD - 0.13 OD - 0.004 OD - 0.005 < = 2.34 < = 0.092 > 3.0 ID + 0.127 ID + 0.15 > 0.118 ID + 0.005 ID + 0.006 > 2.34 > 0.092 ± 0.13 ± 0.005 < = 6.0 OD - 0.127 OD - 0.15 < = 0.236 OD - 0.005 OD - 0.006 < = 3.18 < = 0.125 > 6.0 ID + 0.152 ID + 0.18 > 0.236 ID + 0.006 ID + 0.007 > 3.18 > 0.125 ± 0.20 ± 0.008 < = 10.0 OD - 0.152 OD - 0.18 < = 0.394 OD - 0.006 OD - 0.007 < = 4.95 < = 0.195 > 10.0 ID + 0.178 ID + 0.20 > 0.394 ID + 0.007 ID + 0.008 > 4.95 ± 0.25 > 0.195 ± 0.010 < = 18.0 OD - 0.178 OD - 0.20 < = 0.709 OD - 0.007 OD - 0.008 > 18.0 ID + 0.203 ID + 0.23 > 0.709 ID + 0.008 ID + 0.009 < = 30.0 OD - 0.203 OD - 0.23 < = 1.180 OD - 0.008 OD - 0.009 > 30.0 ID + 0.254 ID + 0.28 > 1.180 ID + 0.010 ID + 0.011 < = 50.0 OD - 0.254 OD - 0.28 < = 1.970 OD - 0.010 OD - 0.011 OPERATION LOAD TOLERANCE > 50.0 ID + 0.305 ID + 0.33 > 1.970 ID + 0.012 ID + 0.013 < = 80.0 OD - 0.305 OD - 0.33 < = 3.150 OD - 0.012 OD - 0.013 Thickness Range AM SAM > 80.0 ID + 0.356 ID + 0.38 > 3.150 ID + 0.014 ID + 0.015 MM Inches Series Series < = 120 OD - 0.356 OD - 0.38 < = 4.720 OD - 0.014 OD - 0.015 + 25.0% > 120 ID + 0.406 ID + 0.43 > 4.720 ID + 0.016 ID + 0.017 < = 1.25 < = .049 ± 20% - 7.5% < = 180 OD - 0.406 OD - 0.43 < = 7.090 OD - 0.016 OD - 0.017 > 1.25 > .049 + 15.0% ID + 0.457 ID + 0.48 ID + 0.018 ID + 0.019 ± 20% > 180 > 7.090 < = 3.00 < = .118 - 7.5% OD - 0.457 OD - 0.48 OD - 0.018 OD - 0.019 > 3.00 > .118 + 10.0% ± 20% < = 6.00 < = .236 - 5.0% + 5.0% OVERALL HEIGHT TOLERANCE > 6.00 > .236 ± 20% - 5.0% AM Series (MM) SAM (MM) AM Series (Inches) SAM (Inches) by part thickness Stainless by part thickness Stainless t Range OH Tol. OH Tol. t Range OH Tol. OH Tol. + 0.10 + 0.11 + .004 + 0.0045 < = 1.25 < = .049 HARDNESS TOLERANCE - 0.05 - 0.06 - .002 - 0.0025 > 1.25 + 0.15 + 0.17 > .049 + .006 + 0.0065 AM Series Tolerance SAM <= 2.00 - 0.08 - 0.09 < = .078 - .003 - 0.0035 Thickness Range Rockwell Stainless > 2.00 + 0.30 + 0.32 > .078 + .012 + 0.0125 MM Inches HRc HRc <= 3.00 - 0.10 - 0.11 < = .118 - .004 - 0.0045 > 3.00 + 0.30 + 0.32 > .118 + .012 + 0.0125 < 1.00 < 0.039 46 - 51 Minimum 38 <= 6.00 - 0.15 - 0.17 < = .236 - .006 - 0.0065 > = 1.00 > = 0.039 44 - 49 Minimum 38 + 0.30 + 0.32 + .012 + 0.0125 < 4.25 < 0.157 > 6.00 > .236 > = 4.25 > = 0.157 42 - 48 Minimum 38 - 0.30 - 0.32 - .012 - 0.0125 5
  8. 8. 09RolexCatalogR3 9/4/09 11:30 AM Page 6 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex AM/SAM SERIES in MM and NEWTONS RECOMMENDED OPERATIONAL LOAD LIMITS ROLEX PART DIMENSIONS (MM) MINIMUM MAXIMUM NUMBER Load Deflection Load Deflection OD ID t h OH h/t (Newtons) (f) % (Newtons) (f) % AM-63203 6.000 3.200 0.300 0.200 0.400 0.667 89 0.076 50% 129 0.114 75% AM-83202 8.001 3.200 0.201 0.198 0.399 0.987 21 0.099 50% 31 0.198 100% AM-83203 8.001 3.200 0.300 0.251 0.549 0.838 85 0.124 50% 125 0.226 90% AM-83204 8.001 3.200 0.399 0.203 0.599 0.510 102 0.071 35% 187 0.127 63% AM-84202 8.001 4.191 0.201 0.251 0.450 1.252 36 0.124 50% 44 0.251 100% AM-84203 8.001 4.191 0.300 0.251 0.549 0.839 95 0.127 51% 120 0.175 70% AM-84204 8.001 4.191 0.399 0.203 0.599 0.510 159 0.102 50% 227 0.152 75% AM-103203 10.008 3.200 0.300 0.353 0.650 1.178 87 0.175 50% 115 0.353 100% AM-103204 10.008 3.200 0.399 0.305 0.701 0.764 144 0.152 50% 202 0.244 80% AM-103205 10.008 3.200 0.500 0.251 0.749 0.502 173 0.102 40% 265 0.163 65% AM-104204 10.008 4.191 0.399 0.305 0.701 0.764 151 0.152 50% 230 0.274 90% AM-104205 10.008 4.191 0.500 0.251 0.749 0.502 221 0.124 50% 315 0.188 75% AM-105225 10.008 5.207 0.249 0.305 0.551 1.224 51 0.152 50% 65 0.305 100% AM-105204 10.008 5.207 0.399 0.305 0.701 0.764 168 0.152 50% 215 0.213 70% AM-105205 10.008 5.207 0.500 0.251 0.749 0.503 246 0.127 51% 350 0.188 75% AM-124204 11.989 4.191 0.399 0.404 0.800 1.013 151 0.201 50% 219 0.404 100% AM-124205 11.989 4.191 0.500 0.353 0.851 0.706 225 0.175 50% 321 0.282 80% AM-124206 11.989 4.191 0.599 0.404 1.001 0.674 369 0.163 40% 513 0.244 60% AM-125205 11.989 5.207 0.500 0.401 0.899 0.802 283 0.201 50% 359 0.282 70% AM-125206 11.989 5.207 0.599 0.353 0.950 0.589 394 0.178 50% 520 0.249 71% AM-126205 11.989 6.198 0.500 0.356 0.851 0.711 259 0.178 50% 353 0.267 75% AM-126206 11.989 6.198 0.599 0.356 0.950 0.593 356 0.142 40% 502 0.213 60% AM-135205 12.497 5.207 0.500 0.353 0.851 0.706 214 0.175 50% 334 0.318 90% AM-136235 12.497 6.198 0.351 0.452 0.800 1.290 138 0.226 50% 161 0.340 75% AM SERIES AM-136205 12.497 6.198 0.500 0.353 0.851 0.706 231 0.178 50% 360 0.318 90% AM-136207 12.497 6.198 0.701 0.302 1.001 0.431 454 0.137 45% 637 0.198 66% mm & newtons AM-147235 13.995 7.188 0.351 0.452 0.800 1.290 112 0.226 50% 137 0.452 100% AM-147205 13.995 7.188 0.500 0.401 0.899 0.802 223 0.201 50% 334 0.363 91% AM-147208 13.995 7.188 0.800 0.302 1.100 0.378 594 0.152 50% 811 0.213 71% AM-155204 15.011 5.207 0.399 0.554 0.950 1.389 164 0.277 50% 190 0.554 100% AM-155205 15.011 5.207 0.500 0.503 1.001 1.005 236 0.251 50% 342 0.503 100% AM-155206 15.011 5.207 0.599 0.452 1.049 0.754 325 0.226 50% 476 0.384 85% AM-155207 15.011 5.207 0.701 0.401 1.100 0.572 427 0.201 50% 569 0.282 70% AM-156205 15.011 6.198 0.500 0.503 1.001 1.005 245 0.251 50% 347 0.478 95% AM-156206 15.011 6.198 0.599 0.452 1.049 0.754 334 0.226 50% 512 0.406 90% AM-156207 15.011 6.198 0.701 0.401 1.100 0.572 445 0.201 50% 623 0.302 75% AM-158207 15.011 8.204 0.701 0.404 1.100 0.576 516 0.203 50% 681 0.282 70% AM-158208 15.011 8.204 0.800 0.404 1.199 0.505 685 0.183 45% 943 0.264 65% AM-168204 16.002 8.204 0.399 0.503 0.899 1.261 138 0.251 50% 173 0.503 100% AM-168206 16.002 8.204 0.599 0.455 1.049 0.758 325 0.226 50% 498 0.409 90% AM-168207 16.002 8.204 0.701 0.455 1.151 0.649 503 0.229 50% 689 0.340 75% AM-168208 16.002 8.204 0.800 0.404 1.199 0.505 623 0.201 50% 890 0.302 75% AM-168209 16.002 8.204 0.899 0.356 1.250 0.395 756 0.178 50% 1032 0.249 70% AM-186204 18.009 6.198 0.399 0.605 1.001 1.516 133 0.302 50% 147 0.483 80% AM-186205 18.009 6.198 0.500 0.602 1.100 1.203 218 0.302 50% 285 0.602 100% AM-186206 18.009 6.198 0.599 0.602 1.199 1.004 338 0.302 50% 489 0.602 100% AM-186207 18.009 6.198 0.701 0.551 1.250 0.786 445 0.277 50% 649 0.470 85% AM-186208 18.009 6.198 0.800 0.503 1.300 0.629 560 0.251 50% 783 0.378 75% AM-188205 18.009 8.204 0.500 0.605 1.100 1.208 236 0.302 50% 302 0.605 100% AM-188207 18.009 8.204 0.701 0.554 1.250 0.790 480 0.277 50% 698 0.470 85% AM-188208 18.009 8.204 0.800 0.505 1.300 0.632 605 0.251 50% 885 0.404 80% AM-188210 18.009 8.204 1.001 0.401 1.400 0.401 885 0.201 50% 1205 0.282 70% AM-189245 18.009 9.195 0.450 0.605 1.049 1.345 196 0.302 50% 231 0.574 95% AM-189207 18.009 9.195 0.701 0.503 1.199 0.717 445 0.251 50% 694 0.452 90% AM-189210 18.009 9.195 1.001 0.404 1.400 0.404 939 0.201 50% 1281 0.282 70% AM-208206 19.990 8.204 0.599 0.706 1.300 1.178 365 0.353 50% 471 0.671 95% AM-208207 19.990 8.204 0.701 0.653 1.349 0.931 476 0.325 50% 694 0.620 95% AM-208208 19.990 8.204 0.800 0.605 1.400 0.756 596 0.302 50% 916 0.544 90% AM-208209 19.990 8.204 0.899 0.556 1.450 0.619 738 0.277 50% 1081 0.445 80% AM-208210 19.990 8.204 1.001 0.554 1.549 0.553 996 0.277 50% 1330 0.389 70% Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 6
  9. 9. 09RolexCatalogR3 9/4/09 11:30 AM Page 7 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex AM/SAM SERIES in MM and NEWTONS ROLEX RECOMMENDED OPERATIONAL LOAD LIMITS PART DIMENSIONS (MM) MINIMUM MAXIMUM NUMBER Load Deflection Load Deflection OD ID t h OH h/t (Newtons) (f) % (Newtons) (f) % AM-201005 19.990 10.211 0.500 0.655 1.151 1.310 231 0.328 50% 285 0.655 100% AM-201008 19.990 10.211 0.800 0.554 1.349 0.692 587 0.277 50% 881 0.470 85% AM-201009 19.990 10.211 0.899 0.556 1.450 0.619 818 0.279 50% 1134 0.419 75% AM-201010 19.990 10.211 1.001 0.556 1.549 0.556 1103 0.277 50% 1468 0.389 70% AM-201011 19.990 10.211 1.100 0.455 1.549 0.413 1139 0.229 50% 1552 0.318 70% AM-201013 19.990 10.211 1.250 0.508 1.750 0.407 1352 0.178 35% 2059 0.279 55% AM-201015 19.990 10.211 1.501 0.302 1.801 0.201 1868 0.152 50% 2598 0.211 70% AM-221106 22.504 11.201 0.599 0.805 1.400 1.343 391 0.404 50% 454 0.645 80% AM-221108 22.504 11.201 0.800 0.655 1.450 0.819 569 0.328 50% 881 0.622 95% AM-221113 22.504 11.201 1.250 0.505 1.750 0.404 1441 0.254 50% 2010 0.353 70% AM-238207 23.012 8.204 0.701 0.805 1.501 1.149 480 0.401 50% 641 0.805 100% AM-238208 23.012 8.204 0.800 0.754 1.549 0.943 596 0.376 50% 872 0.716 95% AM-238209 23.012 8.204 0.899 0.706 1.600 0.785 738 0.353 50% 1072 0.599 85% AM-238210 23.012 8.204 1.001 0.704 1.699 0.703 983 0.351 50% 1339 0.528 75% AM-231009 23.012 10.211 0.899 0.759 1.651 0.845 863 0.378 50% 1134 0.569 75% AM-231010 23.012 10.211 1.001 0.706 1.699 0.706 1041 0.353 50% 1490 0.564 80% AM-231013 23.012 10.211 1.250 0.658 1.900 0.526 1615 0.295 45% 2224 0.427 65% AM-231210 23.012 12.192 1.001 0.607 1.600 0.607 939 0.302 50% 1450 0.516 85% AM-231213 23.012 12.192 1.250 0.607 1.849 0.486 1615 0.274 45% 2237 0.396 65% AM-231215 23.012 12.192 1.501 0.505 1.999 0.337 1997 0.203 40% 2936 0.302 60% AM-251010 24.994 10.211 1.001 0.754 1.750 0.754 939 0.378 50% 1379 0.643 85% AM-251207 24.994 12.192 0.701 0.907 1.600 1.293 552 0.452 50% 641 0.681 75% AM-251209 24.994 12.192 0.899 0.706 1.600 0.785 689 0.353 50% 1116 0.706 100% AM-251210 24.994 12.192 1.001 0.808 1.801 0.807 1108 0.404 50% 1401 0.566 70% AM SERIES AM-251213 24.994 12.192 1.250 0.709 1.951 0.567 1712 0.356 50% 2273 0.495 70% AM-251215 24.994 12.192 1.501 0.554 2.050 0.369 1984 0.249 45% 2798 0.361 65% mm & newtons AM-281008 27.940 10.211 0.800 0.955 1.750 1.194 592 0.478 50% 770 0.955 100% AM-281010 27.940 10.211 1.001 0.904 1.900 0.904 939 0.452 50% 1397 0.859 95% AM-281013 27.940 10.211 1.250 0.805 2.050 0.644 1450 0.404 50% 2006 0.605 75% AM-281015 27.940 10.211 1.501 0.704 2.250 0.469 2055 0.318 45% 2647 0.452 64% AM-281210 27.940 12.192 1.001 0.958 1.951 0.957 1072 0.480 50% 1419 0.767 80% AM-281213 27.940 12.192 1.250 0.859 2.101 0.687 1650 0.429 50% 2371 0.686 80% AM-281215 27.940 12.192 1.501 0.757 2.250 0.504 2153 0.340 45% 2976 0.493 65% AM-281408 27.940 14.199 0.800 1.011 1.801 1.263 729 0.505 50% 841 0.706 70% AM-281410 27.940 14.199 1.001 0.808 1.801 0.807 898 0.404 50% 1343 0.726 90% AM-281413 27.940 14.199 1.250 0.861 2.101 0.689 1637 0.389 45% 2188 0.559 65% AM-281415 27.940 14.199 1.501 0.655 2.149 0.437 2148 0.328 50% 2913 0.460 70% AM-321210 31.496 12.192 1.001 1.107 2.101 1.107 1019 0.554 50% 1370 1.052 95% AM-321213 31.496 12.192 1.250 0.958 2.200 0.766 1441 0.478 50% 2108 0.813 85% AM-321215 31.496 12.192 1.501 0.853 2.350 0.569 2068 0.427 50% 2905 0.640 75% AM-321608 31.496 16.307 0.800 1.057 1.849 1.321 627 0.528 50% 747 0.953 90% AM-321613 31.496 16.307 1.250 0.909 2.149 0.728 1512 0.455 50% 2144 0.726 80% AM-321615 31.496 16.307 1.501 0.912 2.400 0.607 2304 0.409 45% 3131 0.592 65% AM-321618 31.496 16.307 1.753 0.706 2.451 0.403 2913 0.353 50% 3968 0.495 70% AM-321620 31.496 16.307 1.999 0.762 2.751 0.381 3799 0.305 40% 5547 0.457 60% AM-341210 34.036 12.192 1.001 1.257 2.250 1.256 1063 0.627 50% 1321 1.194 95% AM-341213 34.036 12.192 1.250 1.107 2.350 0.886 1490 0.554 50% 2162 0.996 90% AM-341215 34.036 12.192 1.501 1.006 2.499 0.670 2131 0.503 50% 2927 0.754 75% AM-341413 34.036 14.300 1.250 1.161 2.400 0.929 1655 0.579 50% 2206 0.927 80% AM-341415 34.036 14.300 1.501 1.059 2.550 0.706 2366 0.528 50% 3380 0.846 80% AM-341615 34.036 16.307 1.501 1.059 2.550 0.706 2500 0.531 50% 3234 0.742 70% AM-341620 34.036 16.307 1.999 0.861 2.850 0.431 3558 0.345 40% 5155 0.516 60% AM-361809 35.560 18.288 0.899 1.158 2.050 1.288 747 0.579 50% 921 1.158 100% AM-361813 35.560 18.288 1.250 1.011 2.250 0.809 1357 0.505 50% 2104 0.960 95% AM-361820 35.560 18.288 1.999 0.810 2.799 0.405 3870 0.404 50% 5266 0.566 70% AM-401413 39.878 14.300 1.250 1.407 2.649 1.126 1566 0.704 50% 2122 1.407 100% AM-401415 39.878 14.300 1.501 1.257 2.751 0.838 2091 0.627 50% 3091 1.130 90% AM-401420 39.878 14.300 1.999 1.059 3.051 0.530 3345 0.478 45% 4604 0.688 65% AM-401615 39.878 21.387 1.501 1.308 2.799 0.871 2415 0.592 45% 3105 0.853 65% AM-401620 39.878 16.307 1.999 1.110 3.099 0.555 3994 0.554 50% 5315 0.777 70% Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 7
  10. 10. 09RolexCatalogR3 9/4/09 11:30 AM Page 8 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex AM/SAM SERIES in MM and NEWTONS RECOMMENDED OPERATIONAL LOAD LIMITS ROLEX PART DIMENSIONS (MM) MINIMUM MAXIMUM NUMBER Load Deflection Load Deflection OD ID t h OH h/t (Newtons) (f) % (Newtons) (f) % AM-401820 39.878 18.288 1.999 1.163 3.150 0.582 4408 0.582 50% 5840 0.815 70% AM-402010 39.878 20.396 1.001 1.311 2.301 1.310 934 0.655 50% 1139 1.311 100% AM-402015 39.878 20.396 1.501 1.158 2.649 0.772 2108 0.579 50% 3082 0.986 85% AM-402020 39.878 20.396 1.999 1.115 3.099 0.558 4426 0.556 50% 5885 0.780 70% AM-402023 39.878 20.396 2.250 0.909 3.150 0.404 4919 0.455 50% 6699 0.638 70% AM-402025 39.878 20.396 2.499 0.963 3.449 0.385 5800 0.386 40% 8460 0.579 60% AM-452213 44.958 22.403 1.250 1.613 2.850 1.291 1726 0.808 50% 2010 1.209 75% AM-452218 44.958 22.403 1.750 1.313 3.051 0.750 2905 0.655 50% 4270 1.115 85% AM-452225 44.958 22.403 2.499 1.011 3.500 0.404 5787 0.505 50% 7877 0.709 70% AM-501813 50.038 18.390 1.250 1.608 2.850 1.287 1241 0.803 50% 1530 1.608 100% AM-501815 50.038 18.390 1.501 1.808 3.299 1.205 2326 0.904 50% 3011 1.808 100% AM-501820 50.038 18.390 1.999 1.511 3.500 0.756 3634 0.754 50% 5342 1.285 85% AM-501825 50.038 18.390 2.499 1.613 4.100 0.645 6708 0.726 45% 9038 1.049 65% AM-501830 50.038 18.390 3.000 1.412 4.399 0.471 6565 0.424 30% 10471 0.706 50% AM-502020 50.038 20.396 1.999 1.511 3.500 0.756 3723 0.757 50% 5693 1.361 90% AM-502025 50.038 20.396 2.499 1.361 3.851 0.545 6054 0.681 50% 8069 0.955 70% AM-502220 50.038 22.403 1.999 1.615 3.599 0.808 4208 0.808 50% 5836 1.293 80% AM-502225 50.038 22.403 2.499 1.412 3.899 0.565 6534 0.706 50% 8678 0.991 70% AM-502513 50.038 25.400 1.250 1.610 2.850 1.289 1397 0.805 50% 1721 1.610 100% AM-502515 50.038 25.400 1.501 1.610 3.099 1.073 2153 0.805 50% 2807 1.369 85% AM-502520 50.038 25.400 1.999 1.415 3.401 0.708 3741 0.709 50% 5582 1.204 85% AM-502525 50.038 25.400 2.499 1.417 3.899 0.567 6979 0.709 50% 9270 0.993 70% AM-502530 50.038 25.400 3.000 1.113 4.100 0.371 8118 0.500 45% 11436 0.724 65% AM-562915 55.880 28.499 1.501 1.963 3.449 1.308 2415 0.983 50% 2833 1.572 80% AM SERIES AM-562920 55.880 28.499 1.999 1.615 3.599 0.808 3576 0.808 50% 5360 1.453 90% AM-562930 55.880 28.499 3.000 1.316 4.300 0.439 8634 0.658 50% 11694 0.998 76% mm & newtons AM-602120 59.944 20.498 1.999 2.113 4.100 1.057 4079 1.057 50% 5622 2.007 95% AM-602125 59.944 20.498 2.499 1.811 4.300 0.725 5805 0.907 50% 8247 1.450 80% AM-602130 59.944 20.498 3.000 1.712 4.699 0.571 8189 0.770 45% 11187 1.113 65% AM-602625 59.944 25.502 2.499 1.915 4.399 0.766 6561 0.958 50% 9207 1.534 80% AM-602630 59.944 25.502 3.000 1.666 4.651 0.555 9087 0.833 50% 12090 1.166 70% AM-603125 59.944 30.505 2.499 1.821 4.300 0.729 6645 0.912 50% 8558 1.275 70% AM-603130 59.944 30.505 3.000 1.722 4.699 0.574 9385 0.775 45% 12815 1.120 65% AM-603135 59.944 30.505 3.500 1.521 5.001 0.435 11276 0.610 40% 16329 0.912 60% AM-633118 62.992 30.988 1.801 2.370 4.150 1.316 3905 1.186 50% 4435 1.659 70% AM-633125 62.992 30.988 2.499 1.765 4.249 0.706 5640 0.884 50% 8789 1.590 90% AM-633130 62.992 30.988 3.000 1.821 4.801 0.607 9754 0.912 50% 12859 1.275 70% AM-633135 62.992 30.988 3.500 1.415 4.900 0.404 11249 0.706 50% 15314 1.062 75% AM-702620 70.104 25.502 1.999 2.515 4.501 1.258 3999 1.257 50% 5022 2.515 100% AM-703125 70.104 30.505 2.499 2.421 4.900 0.968 6721 1.209 50% 8852 1.935 80% AM-703130 70.104 30.505 3.000 2.118 5.100 0.706 8998 1.059 50% 12859 1.694 80% AM-703630 70.104 35.509 3.000 2.123 5.100 0.708 9706 1.062 50% 12552 1.488 70% AM-703640 70.104 35.509 4.001 1.821 5.799 0.455 16484 0.820 45% 22947 1.184 65% AM-704140 70.104 40.513 4.001 1.628 5.601 0.407 15968 0.732 45% 22391 1.057 65% AM-704150 70.104 40.513 4.999 1.219 6.200 0.244 22596 0.549 45% 32279 0.792 65% AM-713620 71.120 36.068 1.999 2.624 4.600 1.313 4706 1.313 50% 5346 1.836 70% AM-713625 71.120 36.068 2.499 2.019 4.501 0.808 4079 0.706 35% 8340 1.133 56% AM-713640 71.120 36.068 4.001 1.618 5.601 0.404 15359 0.810 50% 20906 1.143 71% AM-803125 80.010 30.988 2.499 2.819 5.301 1.128 6325 1.410 50% 8407 2.677 95% AM-803130 80.010 30.988 3.000 2.515 5.499 0.838 8407 1.257 50% 12437 2.263 90% AM-803140 80.010 30.988 4.001 2.116 6.101 0.529 14807 1.059 50% 19789 1.481 70% AM-803630 80.010 36.068 3.000 2.723 5.700 0.908 9892 1.361 50% 12792 2.042 75% AM-803640 80.010 36.068 4.001 2.223 6.200 0.556 16462 1.110 50% 21898 1.554 70% AM-804123 80.010 40.894 2.250 2.977 5.199 1.323 5769 1.339 45% 6748 1.935 65% AM-804130 80.010 40.894 3.000 2.324 5.301 0.775 8384 1.161 50% 12236 1.976 85% AM-804140 80.010 40.894 4.001 2.228 6.200 0.557 17605 1.113 50% 23419 1.560 70% AM-804150 80.010 40.894 5.050 1.722 6.701 0.341 20203 0.686 40% 31999 1.087 63% AM-904625 89.916 45.974 2.499 3.228 5.700 1.292 7019 1.615 50% 8162 2.421 75% AM-904635 89.916 45.974 3.500 2.525 6.050 0.721 11498 1.288 51% 17005 2.189 87% AM-904650 89.916 45.974 4.999 2.024 7.000 0.405 23561 1.013 50% 32070 1.417 70% AM-1004140 100.076 40.894 4.001 3.226 7.201 0.806 16333 1.613 50% 23579 2.741 85% Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 8
  11. 11. 09RolexCatalogR3 9/4/09 11:30 AM Page 9 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex AM/SAM SERIES in MM and NEWTONS RECOMMENDED OPERATIONAL LOAD LIMITS ROLEX PART DIMENSIONS (MM) MINIMUM MAXIMUM NUMBER Load Deflection Load Deflection OD ID t h OH h/t (Newtons) (f) % (Newtons) (f) % AM-1004150 100.076 40.894 4.999 2.774 7.750 0.555 24802 1.387 50% 32995 1.943 70% AM-1005127 100.076 51.054 2.700 3.528 6.200 1.307 7864 1.765 50% 9238 2.824 80% AM-1005135 100.076 51.054 3.500 2.824 6.299 0.807 10453 1.412 50% 16240 2.682 95% AM-1005140 100.076 51.054 4.001 3.033 7.000 0.758 16493 1.516 50% 22178 2.273 75% AM-1005150 100.076 51.054 4.999 2.837 7.800 0.568 28080 1.420 50% 37274 1.986 70% AM-1005160 100.076 51.054 5.999 2.228 8.199 0.371 32546 1.003 45% 45850 1.448 65% AM-1125730 112.014 56.896 3.000 3.932 6.901 1.311 9585 1.966 50% 11249 3.147 80% AM-1125740 112.014 56.896 4.001 3.228 7.201 0.807 14229 1.615 50% 21319 2.906 90% AM-1125760 112.014 56.896 5.999 2.527 8.499 0.421 32684 1.262 50% 47242 1.895 75% AM-1254140 124.968 40.894 4.001 4.219 8.199 1.055 14905 2.111 50% 21035 4.219 100% AM-1255140 124.968 51.054 4.001 4.529 8.499 1.132 17387 2.266 50% 22169 3.851 85% AM-1255150 124.968 51.054 4.999 3.932 8.900 0.787 24673 1.966 50% 35860 3.343 85% AM-1255160 124.968 51.054 5.999 3.429 9.401 0.572 34094 1.715 50% 47887 2.570 75% AM-1256150 124.968 60.960 4.999 4.044 8.999 0.809 27520 2.022 50% 34881 2.830 70% AM-1256160 124.968 60.960 5.999 3.642 9.601 0.607 39467 1.821 50% 52028 2.550 70% AM-1256180 124.968 60.960 7.493 3.508 10.899 0.468 45156 1.036 30% 78583 1.902 54% AM-1256435 124.968 64.008 3.500 4.542 8.001 1.298 14109 2.271 50% 16084 3.180 70% AM-1256450 124.968 64.008 4.999 3.536 8.499 0.707 23548 1.768 50% 35161 3.005 85% AM-1256480 124.968 64.008 7.493 3.152 10.599 0.421 54288 1.262 40% 78774 1.892 60% AM-1257160 124.968 71.120 5.999 3.350 9.299 0.558 36149 1.509 45% 49488 2.177 65% AM-1257180 124.968 71.120 7.399 3.056 10.399 0.413 53078 1.222 40% 77111 1.831 60% AM-1257110 124.968 71.120 9.200 2.654 11.801 0.289 67312 0.798 30% 110221 1.328 50% AM-1407240 139.954 72.136 3.988 4.470 8.382 1.121 14585 2.215 50% 19558 4.209 94% AM-1407250 139.954 72.136 5.050 3.988 8.999 0.790 27093 1.994 50% 34174 3.589 90% AM SERIES AM-1407280 139.954 72.136 7.493 3.759 11.199 0.502 59127 1.692 45% 81719 2.443 65% AM-1506150 150.114 60.960 4.994 5.339 10.300 1.069 26684 2.672 50% 34872 4.542 85% mm & newtons AM-1506160 150.114 60.960 5.999 4.839 10.800 0.807 36665 2.418 50% 52922 4.112 85% AM-1507160 150.114 71.120 5.999 4.849 10.800 0.808 38929 2.423 50% 51695 3.637 75% AM-1507180 150.114 71.120 7.493 4.562 11.999 0.609 62134 2.052 45% 84294 2.967 65% AM-1508180 150.114 81.026 7.493 4.272 11.699 0.570 55831 1.709 40% 79037 2.563 60% AM-1508110 150.114 81.026 9.299 3.764 13.000 0.405 78356 1.318 35% 119238 2.073 55% AM-1608243 160.020 82.042 4.300 5.646 9.901 1.313 20007 2.824 50% 23459 4.519 80% AM-1608260 160.020 82.042 5.999 4.544 10.500 0.757 32555 2.273 50% 49751 4.089 90% AM-1608210 160.020 82.042 9.398 4.163 13.500 0.443 87052 1.666 40% 125892 2.499 60% AM-1809248 180.086 91.948 4.801 6.251 11.001 1.302 24095 3.124 50% 28360 5.001 80% AM-1809260 180.086 91.948 5.999 5.144 11.100 0.857 30318 2.570 50% 47536 5.144 100% AM-1809210 180.086 91.948 9.398 4.663 14.000 0.496 95014 2.332 50% 127622 3.264 70% AM-2008280 199.898 82.042 7.600 6.652 14.201 0.875 61631 3.327 50% 83636 5.324 80% AM-2008210 199.898 82.042 9.601 5.951 15.499 0.620 99724 2.977 50% 131172 4.166 70% AM-2008212 199.898 82.042 11.501 5.151 16.599 0.448 114443 2.060 40% 165386 3.089 60% AM-2009210 199.898 91.948 9.500 6.170 15.601 0.649 96806 2.776 45% 130326 4.011 65% AM-2009212 199.898 91.948 11.400 5.464 16.800 0.479 125051 2.187 40% 179802 3.279 60% AM-2009214 199.898 91.948 13.106 5.060 18.100 0.386 210724 2.530 50% 387434 3.795 75% AM-20010260 199.898 102.108 5.994 6.502 12.497 1.085 35499 3.279 50% 45952 5.575 86% AM-20010280 199.898 102.108 7.493 6.172 13.599 0.824 58594 3.086 50% 77484 4.630 75% AM-20010210 199.898 102.108 9.398 6.292 15.601 0.669 92483 2.517 40% 128489 3.774 60% AM-20010212 199.898 102.108 11.252 5.009 16.193 0.445 127564 2.253 45% 177862 3.256 65% AM-20010214 199.898 102.108 13.106 5.179 18.199 0.395 141749 1.554 30% 228818 2.591 50% AM-20011212 199.898 112.014 11.100 5.189 16.200 0.468 123121 2.078 40% 177368 3.114 60% AM-20011214 199.898 112.014 12.901 4.686 17.501 0.363 149222 1.641 35% 228418 2.578 55% AM-20011216 199.898 112.014 14.801 4.074 18.801 0.275 165096 1.224 30% 270763 2.040 50% AM-22511285 225.044 112.014 6.200 7.463 13.599 1.204 36834 3.729 50% 46410 6.711 90% AM-22511280 225.552 112.014 7.493 7.071 14.501 0.944 55195 3.536 50% 73272 5.659 80% AM-22511212 225.044 112.014 11.252 5.814 17.000 0.517 128845 2.908 50% 183004 4.361 75% AM-25010210 249.936 102.108 9.601 8.468 18.001 0.882 101450 4.234 50% 132128 6.353 75% AM-25010212 249.936 102.108 11.501 7.564 18.999 0.658 141068 3.782 50% 184258 5.296 70% AM-25012770 249.936 127.000 6.701 8.164 14.801 1.218 42091 4.082 50% 53389 7.752 95% AM-25012710 249.936 127.000 9.398 7.684 17.000 0.818 91509 3.843 50% 121208 5.763 75% AM-25012712 249.936 127.000 11.252 8.158 19.299 0.725 120954 2.855 35% 173699 4.488 55% AM-25012714 249.936 127.000 13.106 6.581 19.601 0.502 188746 3.292 50% 253291 4.608 70% AM-25012716 249.936 127.000 15.011 6.899 21.801 0.460 213993 2.416 35% 322871 3.795 55% Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 9
  12. 12. 09RolexCatalogR3 9/4/09 11:30 AM Page 10 410-391-7400 Fax 410-687-9223 www.mw-ind.com/rolex AM/SAM SERIES in INCHES and POUNDS RECOMMENDED OPERATIONAL LOAD LIMITS ROLEX PART DIMENSIONS (Inches) MINIMUM MAXIMUM NUMBER Load Deflection Load Deflection OD ID t h OH h/t (Pounds) (f) % (Pounds) (f) % AM-63203 0.236 0.126 0.012 0.008 0.016 0.667 20 0.003 38% 29 0.005 75% AM-83202 0.315 0.126 0.008 0.008 0.016 0.987 5 0.004 50% 7 0.008 100% AM-83203 0.315 0.126 0.012 0.010 0.022 0.838 19 0.005 50% 28 0.009 90% AM-83204 0.315 0.126 0.016 0.008 0.024 0.510 23 0.003 35% 42 0.005 63% AM-84202 0.315 0.165 0.008 0.010 0.018 1.252 8 0.005 50% 10 0.010 100% AM-84203 0.315 0.165 0.012 0.010 0.022 0.839 21 0.005 51% 27 0.007 70% AM-84204 0.315 0.165 0.016 0.008 0.024 0.510 36 0.004 50% 51 0.006 75% AM-103203 0.394 0.126 0.012 0.014 0.026 1.178 20 0.007 50% 26 0.014 100% AM-103204 0.394 0.126 0.016 0.012 0.028 0.764 32 0.006 50% 46 0.010 80% AM-103205 0.394 0.126 0.020 0.010 0.030 0.502 39 0.004 40% 60 0.006 65% AM-104204 0.394 0.165 0.016 0.012 0.028 0.764 34 0.006 50% 52 0.011 90% AM-104205 0.394 0.165 0.020 0.010 0.030 0.502 50 0.005 50% 71 0.007 75% AM-105225 0.394 0.205 0.010 0.012 0.022 1.224 12 0.006 50% 15 0.012 100% AM-105204 0.394 0.205 0.016 0.012 0.028 0.764 38 0.006 50% 48 0.008 70% AM-105205 0.394 0.205 0.020 0.010 0.030 0.503 55 0.005 51% 79 0.007 75% AM-124204 0.472 0.165 0.016 0.016 0.032 1.013 34 0.008 50% 49 0.016 100% AM-124205 0.472 0.165 0.020 0.014 0.034 0.706 51 0.007 50% 72 0.011 80% AM-124206 0.472 0.165 0.024 0.016 0.039 0.674 83 0.006 40% 115 0.010 60% AM-125205 0.472 0.205 0.020 0.016 0.035 0.802 64 0.008 50% 81 0.011 70% AM-125206 0.472 0.205 0.024 0.014 0.037 0.589 89 0.007 50% 117 0.010 71% AM-126205 0.472 0.244 0.020 0.014 0.034 0.711 58 0.007 50% 79 0.011 75% AM-126206 0.472 0.244 0.024 0.014 0.037 0.593 80 0.006 40% 113 0.008 60% AM-135205 0.492 0.205 0.020 0.014 0.034 0.706 48 0.007 50% 75 0.013 90% AM-136235 0.492 0.244 0.014 0.018 0.032 1.290 31 0.009 50% 36 0.013 75% AM SERIES AM-136205 0.492 0.244 0.020 0.014 0.034 0.706 52 0.007 50% 81 0.013 90% inches & pounds AM-136207 0.492 0.244 0.028 0.012 0.039 0.431 102 0.005 45% 143 0.008 66% AM-147235 0.551 0.283 0.014 0.018 0.032 1.290 25 0.009 50% 31 0.018 100% AM-147205 0.551 0.283 0.020 0.016 0.035 0.802 50 0.008 50% 75 0.014 91% AM-147208 0.551 0.283 0.032 0.012 0.043 0.378 134 0.006 50% 182 0.008 71% AM-155204 0.591 0.205 0.016 0.022 0.037 1.389 37 0.011 50% 43 0.022 100% AM-155205 0.591 0.205 0.020 0.020 0.039 1.005 53 0.010 50% 77 0.020 100% AM-155206 0.591 0.205 0.024 0.018 0.041 0.754 73 0.009 50% 107 0.015 85% AM-155207 0.591 0.205 0.028 0.016 0.043 0.572 96 0.008 50% 128 0.011 70% AM-156205 0.591 0.244 0.020 0.020 0.039 1.005 55 0.010 50% 78 0.019 95% AM-156206 0.591 0.244 0.024 0.018 0.041 0.754 75 0.009 50% 115 0.016 90% AM-156207 0.591 0.244 0.028 0.016 0.043 0.572 100 0.008 50% 140 0.012 75% AM-158207 0.591 0.323 0.028 0.016 0.043 0.576 116 0.008 50% 153 0.011 70% AM-158208 0.591 0.323 0.032 0.016 0.047 0.505 154 0.007 45% 212 0.010 65% AM-168204 0.630 0.323 0.016 0.020 0.035 1.261 31 0.010 50% 39 0.020 100% AM-168206 0.630 0.323 0.024 0.018 0.041 0.758 73 0.009 50% 112 0.016 90% AM-168207 0.630 0.323 0.028 0.018 0.045 0.649 113 0.009 50% 155 0.013 75% AM-168208 0.630 0.323 0.032 0.016 0.047 0.505 140 0.008 50% 200 0.012 75% AM-168209 0.630 0.323 0.035 0.014 0.049 0.395 170 0.007 50% 232 0.010 70% AM-186204 0.709 0.244 0.016 0.024 0.039 1.516 30 0.012 50% 33 0.019 80% AM-186205 0.709 0.244 0.020 0.024 0.043 1.203 49 0.012 50% 64 0.024 100% AM-186206 0.709 0.244 0.024 0.024 0.047 1.004 76 0.012 50% 110 0.024 100% AM-186207 0.709 0.244 0.028 0.022 0.049 0.786 100 0.011 50% 146 0.019 85% AM-186208 0.709 0.244 0.032 0.020 0.051 0.629 126 0.010 50% 176 0.015 75% AM-188205 0.709 0.323 0.020 0.024 0.043 1.208 53 0.012 50% 68 0.024 100% AM-188207 0.709 0.323 0.028 0.022 0.049 0.790 108 0.011 50% 157 0.019 85% AM-188208 0.709 0.323 0.032 0.020 0.051 0.632 136 0.010 50% 199 0.016 80% AM-188210 0.709 0.323 0.039 0.016 0.055 0.401 199 0.008 50% 271 0.011 70% AM-189245 0.709 0.362 0.018 0.024 0.041 1.345 44 0.012 50% 52 0.023 95% AM-189207 0.709 0.362 0.028 0.020 0.047 0.717 100 0.010 50% 156 0.018 90% AM-189210 0.709 0.362 0.039 0.016 0.055 0.404 211 0.008 50% 288 0.011 70% AM-208206 0.787 0.323 0.024 0.028 0.051 1.178 82 0.014 50% 106 0.026 95% AM-208207 0.787 0.323 0.028 0.026 0.053 0.931 107 0.013 50% 156 0.024 95% AM-208208 0.787 0.323 0.032 0.024 0.055 0.756 134 0.012 50% 206 0.021 90% AM-208209 0.787 0.323 0.035 0.022 0.057 0.619 166 0.011 50% 243 0.018 80% AM-208210 0.787 0.323 0.039 0.022 0.061 0.553 224 0.011 50% 299 0.015 70% AM-201005 0.787 0.402 0.020 0.026 0.045 1.310 52 0.013 50% 64 0.026 100% Can’t find the part required for your application? No problem! Call Rolex Spring at 410-391-7400 and speak to a Sales Associate regarding our custom manufacturing capabilities. 10

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