United States
Element Materials Technology – Jupiter
15814 Corporate Circle, 33478, Jupiter, FL, United States
A2LA|7039.01ISO/IEC 17025Register collected 2026-08-22
Certificates
1
Scope items
3
Locations
1
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- A2LACollected
- 7039.01Active
Certificates and scope
1A2LA
ISO/IEC 17025
Active7039.01
Accredited scope, certificate 7039.01
| Discipline | Method | Matrix | Range |
|---|---|---|---|
| mechanical | - | - | - |
| mechanical | MIL-STD-202, Method 212; MIL-STD-810, Method 513; MIL-E-5272, Rev. C, 22 Jan 71, Para. 4.16; RTCA/DO-160, Section 8; MIL-STD-202, Methods 201; MIL-STD-204; MIL-STD-214; MIL-STD-810, Methods 514; MIL-STD-810, Method 516; MIL-E 5272, Rev. C, 22 Jan 71, Para. 4.7; IEC 68-2-6; IEC 68-2-34; RTCA/DO-160, Section 7; MIL-STD-202, Methods 202; MIL-STD-205; MIL-STD-213; MIL-STD-810, Methods 514; MIL-STD-810, Method 516; IEC 68-2-27; MIL-STD-810, Method 516; SAE AS 2078, Sections 4.7; SAE AS 2078, Section 4.8; SAE ARP 1401; SAE ARP 603; SAE ARP 1383; SAE AS 2078 Section 4.9 | - | to 44000 lbf |
| mechanical | MIL-STD-810, Method 512; SAE AS 2078, Section 4.6; MIL-STD-810, Method 511; RTCA/DO-160, Section 9; SAE AS 4273; ISO 2685; SAE AS 1055; SAE AIR 1377A; DOT/FAA AC 20-135; RTCA/DO-160, Section 26; Rolls-Royce Spec. MTR00072; Rolls-Royce Spec. FVR08366; Rolls-Royce Spec. JES 314-1; ARP492 Continuous Flow; MIL-E-5007, Section 4.6.2.2.5; MIL-E-5007, Section 4.6.2.2.6; MIL-E-5007, Section 4.6.2.2.7; MIL-E-5007, Section 4.6.2.2.8; MIL-E-5007, Section 4.6.2.2.9 | Aerospace components; Military equipment; Nuclear equipment; Commercial and Automotive components | -100 to 8000 °F |
Ranges are reproduced from the accredited scope document as published. An absent range means the register did not state one.
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