ASTM_D_4054_-_09_rus.pdf

D 405409 STANDARD PRACTICE FOR QUALIFICATION AND APPROVAL OF NEW AVIATION TURBINE FUELS AND FUEL ADDITIVES 2013 ():1930-13/ASTM :15.04.2013 -,.9,-49,-1,119991.:(499)236-54-49,236-43-83:(499)230-13-72 E-mail:interstgost.ru Web:www.interstandart.ru (ASTM International)100 rr Harbor Drive,West Conshohocken,PA 19428,USA.ASTM International ,ASTM International.-,ASTM International ,.This translation is executed by FBU“CIC“Interstandard”of Federal Agency on Technical Regulating and Metrology under the license of American Society for Testing and Materials(ASTM International)100 rr Harbor Drive,West Conshohocken,PA 19428,USA.ASTM International does not approve and does not confirm these translations and in any cases only the English version published with a sign of ASTM International copyright can be considered as the original version.Reproduction of the specified translations by any Party,except for ASTM International or FBU“CIC“Interstandard”,is strictly forbidden according to the USA legislation and international copyright.ASTM D 4054-09 1 D 405409 1 D 4054;,.().1.*1.1 ,.(OEM-)ASTM International ,OEM-.,.,ASTM 1 ASTM D02 ,D02.J0.04 .01 2009.2010.1981.2003.D4054-93(2003).DOI:10.1520/D4054-09.ASTM D 4054-09 2International(D02.J0),OEM-.ASTM International OEM-/.1.2 OEM-,.OEM-,2016 Pratt&Whitney(P&W),D50TF2 General Electric Aviation(GE)Rolls-Royce(RR).OEM-,(ASTM),D 1655,91-91,MIL-DTL-83133 MIL-DTL-5624.,(FAA)(EASA).1.3 (),.1.4 ,.,ASTM D 4054-09 3 .2.2.1 ASTM:2 A 240/A240M ,B 36/B36M ,B 93/B93M ,D 56 D 86 D 257 D 395 D 412 D 445 ()D 471 D 790 /D 924 ()(2 ASTM,ASTM www.astm.org ASTM serviceastm.org.ASTM.Document Summary ASTM.ASTM D 4054-09 4)D 1002 (-)D 1319 D 1331 -3 D 1414 D 1655 D 2240 D 2386 D 2425 -D 2624 D 2717 D 2887 D 3241 D 3359 D 3363 D 3701 -D 3703 3.www.astm.org.ASTM D 4054-09 5,D 3828 D 3948 D 4052 ,API()D 4066 ,(PA)D 4629 ,D 5001 (BOCLE)D 5291 ,D 5304 -D 5363 (AN)D 5972 ()D 6304 ,D 6378 (VPX),-ASTM D 4054-09 6D 6379 D 6732 -D 6793 D 7111 -E 411 2,4-E 659 E 681 ()E 1269 2.2 :4 FED-STD-791 ,2.3 :4 DOD-L-85645 -MIL-A-8625 MIL-C-83019 4 ,700 Robbins Avenue,Building 4D,PA 1911-5094 -http:/assist.daps.dla.mil/quicksearch/ASTM D 4054-09 7MIL-DTL-5541 MIL-DTL-5624 JP-4 JP-5 MIL-DTL-24441 ,MIL-PRF-25017 ,/MIL-DTL-25988,-,MIL-DTL-26521 MIL-DTL-83054 MIL-DTL-83133 JP-8(NATO F-34),NATO F-35 JP-8+100(NATO F-37)MIL-H-4495 MIL-H-17902 MIL-HDBK-510-1 MIL-P-25732 275F(135C)MIL-PRF-370 MIL-PRF-6855 ,MIL-PRF-8516 ASTM D 4054-09 8 MIL-PRF-46010 ,NATO S-1738 MIL-PRF-81733-MIL-PRF-87260 MIL-R-46082 MIL-S-85334 MIL-DTL-5578 MMM-A-132 QPL-25017 ,MIL-PRF-25017(,/)2.4 SAE International:5 SAE-AMS-2410-SAE-AMS-2427 ,-SAE-AMS-3215 -(NBR)65-75 SAE-AMS-3265-(T)5 SAE International,400 Commonwealth Dr.,Warrendale,15096,http:/www.sae.org/servlets/index ASTM D 4054-09 9 360 F(182 C)SAE-AMS-3276 360 F(182 C),SAE-AMS-3277 400 F(204C),SAE-AMS-3278 (PUR),/,SAE-AMS-3279 350F(177C)/SAE-AMS-3281 (T)360 F(182C)/SAE-AMS-3283-SAE-AMS-3361 ,150 400 (15 40 a)SAE-AMS-3375 /,SAE-AMS-3376-ASTM D 4054-09 10SAE-AMS-4017 2.5Mg-0.25Cr(5052-H34),SAE-AMS-4027 1.0Mg-0.60Si-0.28Cu-0.20Cr(6061;-T6,-T651),SAE-AMS-4029 4.5Cu-0.85SI-0.80Mn-0.50Mg(2014;-T6,-T651),SAE-AMS-4037 4.4Cu-1.5Mg-0.60Mn(2024;-T3,-T351),SAE-AMS-4107 (7050-T74),SAE-AMS-4260 7.0Si-0.32Mg(356.0-T6),SAE-AMS-4750-45Sn-55Pb SAE-AMS-4751-63Sn-37Pb SAE-AMS-4901,70.0 .(485 Ma)SAE-AMS-4915,8Al-1V-IMo SAE-AMS-5330 0.80Cr-1.8Ni-0.35Mo(0.38-0.46C)(SAE 4340.)SAE-AMS-5338 0.95Cr-0.20Mo(0.35-0.45C)(SAE 4140 Mod),ASTM D 4054-09 11 SAE-AMS-5504,-12.5Cr(SAE 51410)SAE-AMS-5525,-15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V 1800 F(982 C),SAE-AMS-5604,-16.5Cr-4.0Ni-4.0Cu-0.30,SAE-AMS-5613,-12.5Cr(SAE 51410)SAE-AMS-5643,-16Cr-4.0Ni-0.30Cb-4.0Cu,SAE-AMS-5688 -18Cr-9.0Ni(SAE 30302),SAE-AMS-5737,-15Cr-25.5Ni-1.2Mo-2.1Ti-0.006B-0.30V,1650 F(899 C)SAE-AMS-6277,0.50Cr-0.55Ni-0.20Mo(0.18-0.23C)(SAE 8620),SAE-AMS-6345,-0.95Cr-0.20Mo(0.28-0.33C)(SAE 4130),SAE-AMS-6415,0.80Cr-1.8Ni-0.25Mo(0.38-0.43C)(SAE 4340)SAE-AMS-6444,1.45Cr ASTM D 4054-09 12(0.93-1.05C)(SAE 52100),SAE-AMS-6470,1.6Cr-0.35Mo-1.13Al(0.38-0.43C)SAE AMS 6472 1.6Cr-0.35Mo-1.1Al(0.38-0.43C),112 .(772 Ma)SAE-AMS-7257 ,(FFKM)70 80 SAE-AMS-7271 -(NBR),60 70 SAE-AMS-7276 -(FKM),70 80 SAE-AMS-7902 ,98Be SAE-AMS-C-27725 250 F(121 C)SAE AMS-I-7444 SAE-AMS-DTL-23053/5 -SAE-AMS-P-5315-(NBR)60 70 SAE-AMS-P-83461 ,275 F(135 C)SAE-AMS-QQ-A-250/12 7075 SAE-AMS-QQ-P-416 ASTM D 4054-09 13SAE-AMS-R-25988,-/SAE-AMS-R-83485-/SAE-AMS-S-4383 -N SAE-AMS-S-8802 /SAE AS5127/1 -2.5 (AWS):6 AWS C3.4 AWS C3.5 AWS C3.6 AWS C3.7 2.6 IPC:7 J-STD-004 J-STD-005 J-STD-006 ,2.7 Boeing(BMS):8 BMS 5-267 BMS 10-20-BMS 10-39-6 ,550 N.W.LeJeune Road,33126;http:/www.aws.org/7 IPC,3000 Lakeside Drive,Suite 309S,Bannockburn,60015;http:/www.ipc.org 8 Boeing.ASTM D 4054-09 142.8 (ISO):9 ISO 20823.,2.9 (UK MOD):10 91-91 ,Jet A-1,NATO:F-35 :AVTUR 2.10 (EPA):11 8015 8260 /-(GC/MS)8270 /-(GC/MS)2.11 (API)12 API 1581 /(5-)3.3.1 /,.9 ISO,1,ch.de la Voie-Creuse,CP 56,CH-1211 20,;http:/www.iso.org/10 ,Kentigern House,65