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Touchstone Systems & Services

1817 Porter Street SW, 49519, Wyoming, MI, United States

A2LA|560.01ISO/IEC 17025Register refreshed 2026-09-25
Certificates
1
Scope items
6
Locations
1

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Register record

A2LARefreshed
560.01Active

Certificates and scope

1
A2LA

ISO/IEC 17025

Active

560.01

The scope document we hold says it is valid until 2027-05-31.

View scope

Accredited scope, certificate 560.01

LineDisciplineMethodMatrixRange
1mechanicalRTCA/DO-160 C/D/E/F/G/H, Section 1-6; MIL-STD-202F; MIL-STD-810 C/D/E/F/G/H, Method 501, Method 502, Method 507; SAE J1211; IEC 68-2-2; IEC 60068-2-2; IEC 60068-2-38; IEC 61215; IEC 61646; GM9505P; GMW 14124; GM9132P; GMW 3217; GM2210M; DC-10611; PF9688; FORD 00.00EA-D11-1; FORD WSS-M15P34-D/E; NISSAN NES M 0007; MITSUBISHI ESX60210 4.3; NISSAN NES MO 131; DIN 75220; GM4465P; GM4350M; ASTM D1735, D2247, D4585; HES D2016-99A, HES D6501-03, HES D2021; FORD WSS-M15P34-D; ASTM D4587, G154; FLTM BI 104; ISO 4892-3; SAE J2412Textile-100 to 150 °C
2materialsASTM B117; ASTM B537; ASTM D610; ASTM D714; ASTM G85; GM4350M; GM4298P; GM4476P; GM9540P; RTCA/DO-160 C/D/E/F/G/H; MIL-STD-202F; MIL-STD-810 C/D/E/F/G/H; SAE J1211; PARKHAN P21- CPE-023 Rev.00; CHRYSLER LP-463-PB-10-01CHG.C; MS-PB-45-2 CHG.V; FORD FLTM BI 103-01; FRTLINER 49-00005 Rev.6; HES D2003-03B Rev.4; HES D2016-99A; HES D6501-03; HES D2021-99 C Rev.1; HES D6001-71; NISSAN 54400 NDS00; NISSAN NES M 0007; TSH6524G; Toyota TSH1552G; CEMS GT-7D; DIN 50021; Volvo STD 1027.14; ASTM B368; GM4372M; GM4476M; JIS H 8502-99; TSH6500G; HES D600-1-71; HES D2003-05B Rev.6; HES 2016-99A; HES D6501-03; TS430-1-4; GES 43226; WSB-MIP83-B1; WSB-MIP83-B2; WSB-MIP83-B3; WSB-MIP83-B4; DVM-0008RG Ver3; FRTLINER 49-00039 Rev A; FORD WSS-M1P83-C1/C2; RTCA/DO-160 C/D/E/F/G/H; MIL-STD-810 C/D/E/F/G/H; ISO 1183-1; ASTM D790; GMW 3235; SAE J1756; ISO 1172; SAE J400; MIL-STD-202F; GMW 3431; IEC 60529; SAE J575-to 70000 ft
3materialsASTM D870; ASTM D2248; IEC 60529; FLTM BI 104-01; GM4431M; HES D2016-99A; HES D6501-03; Toyota TSH1505G; RTCA/DO-160 C/D/E/F/G/H; MIL-STD-810 C/D/E/F/G/H; MIL-STD-202F; IEC 20653; SAE J994; WSS-M2P188-C1; ASTM D642; ASTM D3574; STRYKER ES-0668; STRYKER ES-0703; GM9502P; GM9150P; GM 4350M; ASTM D3363; HES D2016-99A; HES D6501-03 C Rev.2; NISSAN NES M 0007; GM9506P; GM9071P; GMW 14289; ASTM D3359; ASTM D1654; LP 63PB 15 01 CHG A; FLTM BI 104-01; FLTM BI 106-01; HES D2016-99; HES D 6501-03 C Rev. 2; DAIMLER DBL 7399; MIL-M-13231; ASTM D4060; SAE J365; SAE J948; RTCA/DO-160 C/D/E/F/G/H; MIL-STD-810 C/D/E/F/G/H; HES D6501-03 C Rev.2; HES D2016; FREIGHTLINER 49-00023; ASTM D1939; ASTM D1308; ASTM D5402; GM4350M; GM9500; GM9501; GM9517P; GM9900P; GMN 10033; GMW 14334; GMW 14444; NES M0007; SAE J1351; FLTM BN 112; FLTM BI 113-to 5000 lbs
4materialsGM9033P; HES D2016-99A; NISSAN NES M 0007; FLTM BN 107-1; JIS K 5400; ASTM D2794; ASTM D5276; ASTM D880; ASTM D4003; ASTM D617; DAIMLER VOA621-402; PACCAR CMT0033; ASTM D1654; CEM GT-7D; ASTM B487; ASTM D1005; ASTM D4138; ASTM D7091; HES D6501; ASTM D523; ASTM D522; ASTM D1737; GM9509P; GMW 15891; FLM BO 131; SAE J1351; IPC-A-610F; GMW3172-DRBTR; RTCA/DO-160 C/D/E/F/G/H; MIL-STD-810 C/D/E/F/G/H; MIL-STD-202F; SAE J1211; GM9110P; GM9123P; GMW 3172; PF9688; FORD 00.00EA-D11-1; DC-10611; ASTM D5487; IEC 68-2-27; IEC 68-2-29; MIL-STD-901--50 to 150 °C
5materialsCALIFORNIA TB117; CPAI-83; 16 CFR 1632; ISO 2685; 3795; JIS D1201; FMVSS 302 HES C206; DBL 5404; TSM0500G; BSDM0500; GMW3232; WSS-M15P4-1; ESE97B-1011014-AA; GB8410-2006; CMVSS 302; ISO 3795; DBL 5307.10; VCS5031; GM9070P (superseded 2011)2; SAE J369; FED TEST METHOD 5903.1; FED TEST METHOD 5906; FED STD 191A (VERT); FED STD 191 (HORIZ); FAA 25.853 APPENDIX F; PART 1(b)(5); POWER PLANT No. 3: AC 20-135; NFPA 260; NFPA 261; NFPA 101 (Sec 10.3); NFPA 701 UFAC TEST SERIES; ASTM E1537; E1353; RTCA/DO-160 F/G/H; Section 26; RTCA/DO-204-204; EN 1021-2; BS 5852; UL 94; BAC 5331; Boeing D6-81926 (except section 5.6.9 (Odor and Fungus)); Airbus L00716172Furniture Seating; Walls / Tops; Mattress; Foams; Films; PCB’s; Fabrics; Composites; Pneumatic / Servo PLC Driven Aircraft; Boot / Seal / Duct Lifecycle, in Combination with Extreme Temperature Internal and External with Pressure Cycling Screening (ESS), Vibration Profiles with Or Without Temperature and RH Using Customer QTP’s Engineering Design Requirements-
6mechanical---

Ranges are reproduced from the accredited scope document as published. An absent range means the register did not state one. Line numbers are ours, for cross-reference; they follow the order of the scope document.

Location

1817 Porter Street SW, Wyoming, MI, 49519, US

42.91326, -85.70570

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