ABOUT COMPANY
Authorization
ISO/JIS Q 14001 / Environmental Management Systems
ISO/IEC 17025 (Testing Laboratory) / General requirements for the competence of testing and calibration laboratories
ISO/IEC 17025(Calibration Laboratory) / General requirements for the competence of testing and calibration laboratories
Nadcap(National Aerospace and Defense Contractors Accreditation Program )
Materials Testing (MTL)
Non Metallic Materials Testing (NMMT)
IHI Corporation
| Scope of Approval | Material Testing (J-ISAJT-F005), Metallic Materials Testing (ISAJT-F005) |
|---|---|
| Approval for | Management System |
| Initial App. Date | October 13, 2010 |
| App. Date | May 17, 2022 (*March 12, 2022) |
| Exp. Date | March 11, 2025 |
| Test Code & Test Item | A: Room Temperature Tensile |
| B: Elevated Temperature Tensile | |
| C: Stress Rupture | |
| L: Metallography (General) | |
| La: Grain Size | |
| L2: Alloy Depletion* | |
| L4: Casting (Mold) Reaction* | |
| L7: IGA/IGO* | |
| L8: Alpha Cace_Wrought | |
| L9: Alpha Cace_Casting | |
| L13: Other* | |
| O: Load Control (High Cycle) Fatigue | |
| P: Fracture Toughness | |
| XA: Creep | |
| XE: Crack Propagation | |
| Y: Strain Control (Low Cycle) Fatigue | |
| Z: Mechanical Testing Specimen Preparation (Low Stress Grinding and Polishing) |
|
| * Applies to ISAJT-F005 ONLY. | |
| Scope of Approval | CMC Materials Testing (ISAJT-F009) |
|---|---|
| Approval for | Management System |
| Initial App. Date | May 10, 2016 |
| App. Date | July 6, 2023 |
| Exp. Date | March 11, 2025 |
| Test Code & Test Item | |
| 1A: In-plane Tensile Test (Room Temperature) | |
| 1B: In-plane Tensile Test (Elevated Temperature) | |
| 1C: In-plane Compressive Test (Room Temperature) | |
| 1Ca: In-plane Compressive Test (Elevated Temperature) | |
| 1D: In-plane Shear Test (Room Temperature) | |
| 1E: Interlaminar Shear Test (Room Temperature) | |
| 1Ea: Interlaminar Shear Test (Elevated Temperature) | |
| 1F: Out-of-plane Compressive Test (Room Temperature) | |
| 1Fa: Out-of-plane Compressive Test (Elevated Temperature) | |
| 1G: Out-of-plane Tensile Test (Room Temperature) | |
| 1J: In-plane Tension - Tension Cyclic Fatigue Test | |
| 1N: In-plane Tensile Creep and Creep Rapture Test | |
| 1U: In-plane Shear Test (Elevated Temperature) | |
| 1T: Out-of-plane Tensile Test (Elevated Temperature) | |
| 1V: Out-of-plane Shear Test (Room Temperature) | |
| 1Va: Out-of-plane Shear Test (Elevated Temperature) |
Mitsubishi Heavy Industries, Ltd. Nagoya Aerospace Systems Works
| Specification | MSJ4000 |
|---|---|
| Certification Required | AS/EN/JIS Q 9100:2016 |
| Initial App. Date | November 15, 2012 |
| App. Date | November 15, 2021 |
| Exp. Date | November 14, 2024 |
| Scope | Activities related to test piece preparation, jig machining, examination services, inspection services, and testing services |
| Item excluded | 8.3 Design and Development of Products and Services |
Mitsubishi Heavy Industries, Ltd. Nagoya Guidance & Propulsion Systems Works
| Specification | MS84001 Session B |
|---|---|
| Initial App. Date | April 28, 2015 |
| App. Date | April 28, 2015 |
| Exp. Date | - |
| Scope | Manufacturing |
| Applicable to | Machined products for Aerospace and Defense |
| Limited to | Specimen preparation, testing, examination, and creation of report only |
Kawasaki Heavy Industries, Ltd. Aerospace Systems Co.
| Specification | J-ISAJT-F005 |
|---|---|
| Process | Metallic Materials Testing Laboratories |
| Initial App. Date | July 17, 2013 |
| App. Date | October 13, 2023 |
| Exp. Date | October 12, 2025 |
| Test Code & Test Item | A: Room Temperature Tensile |
| B: Elevated Temperature Tensile | |
| C: Stress Rupture | |
| XA: Creep Rupture | |
| O: Force Controlled Fatigue | |
| Y: Strain Controlled Fatigue | |
| L: Metallography | |
| La: Grain Size | |
| L13: Other | |
| Z : Low Stress Grinding of Test Specimens | |
| Other: Shear NASM1312-13 |
| Specification | KQ-7204 |
|---|---|
| Process | Metallic Materials Testing Laboratories |
| Initial App. Date | June 15, 2020 |
| App. Date | October 13, 2023 |
| Exp. Date | October 12, 2025 |
| Test Code & Test Item | 1: Room Temperature Tensile |
| 2: Elevated Temperature Tensile | |
| 3: Stress Rupture | |
| 4: Creep, Creep Rupture | |
| 5: Fatigue-Load Controlled | |
| 6: Fatigue-Strain Controlled | |
| 21: Rockwell | |
| 30: General Microstructure | |
| 30-a: Grain Size | |
| 31: Macrostructure | |
| 35*1: Surface Contamination | |
| 55: Other Mechanical Testing | |
| 70*2: Specimen Heat Treatment | |
| 71: Specimen Machining | |
| 72: Specimen Low-stress Machining |
*1: Applies to Ni, Co, and Fe.
*2: Applies to industrial gas turbine work ONLY as the internal procedures of furnace reference JIS B6901.
GE Aviation
| Scope of Approval | Mechanical Testing, Mechanical Test Specimen Preparation |
|---|---|
| Approval for | S-400 |
| Initial App. Date | October 22, 2014 |
| App. Date | October 27, 2023 |
| Exp. Date | March 31, 2025 |
| Test Code & Test Item | AI0A: Room Temperature Tensile |
| AI0B: Elevated Temperature Tensile | |
| AI0C: Stress Rupture | |
| AI3L: Alpha Case of Wrought Ti Alloys | |
| AI8L: Grain Size | |
| AI9L: Inclusion Content / Other Metallographic Evaluations | |
| AI1M: Rockwell Hardness | |
| AI2M: Brinell Hardness | |
| AI3M: Vickers Hardness | |
| AI0O: High Cycle Fatigue Testing | |
| AI0N: Charpy Testing | |
| AI0P: Fracture Toughness Determination | |
| AI0X: Low Stress Grinding | |
| AI0Y: Low Cycle Fatigue Testing | |
| AI0Z: Low Stress Grinding and Polishing | |
| AIXE: Crack Propagation Measurement | |
| AIXA: Creep | |
| AIXL: Macro Metallography | |
| AIXR: Residual Life | |
| AIXZ: E50TF133 Grain Size Evaluation |
Rolls-Royce
| Scope of Approval |
・Test Piece Machining ・Mechanical testing as specified in CME 5021 and in accordance with MSRR 9922 ・MSRR 9968 |
|---|---|
| Initial App. Date | October 07, 2015 |
| App. Date | May 26, 2016 |
| Exp. Date | Unlimited |
| Test Item | Tensile (Room Temp. and Elevated Temp.) |
| Stress Rupture | |
| Creep Strain | |
| Low Cycle Fatigue (Load Control / Strain Control) | |
| High Cycle Fatigue (Axial) | |
| Fracture Toughness | |
| Crack Propagation (Compact Tension) | |
| Charpy Impact |
MTU Aero Engines
| Vendor Code | 50000268 |
|---|---|
| Initial App. Date | August 29, 2016 |
| App. Date | July 19, 2024 |
| Exp. Date | July 31, 2027 |
| Test Item | Machining of specimen (Low stress grinding and polishing ) |
| Evaluation of microstructure | |
| RTT-Testing | |
| ETT-Testing | |
| SR Testing | |
| Creep Testing | |
| LCF-Testing | |
| Fracture Toughness | |
| Machining of specimen (Machining of standard specimen ) | |
| Hardness Testing (HBW/HRC/HV) |
Safran Aircraft Engines
| Initial App. Date | June 24, 2014 |
|---|---|
| App. Date | June 12, 2024 |
| Exp. Date | Not limited |
| Test Code & Test Item | Z1: Machining test pieces for metallic fatigue test pieces |
| Z2: Machining test pieces other than metallic fatigue test pieces (such as for tensile and charpy impact tests) |
|
| A: Metals ― Room Temp. Tensile Test | |
| B: Metals ― Elevated Temp. Tensile Test | |
| Y: Metals ― Low Cycle Fatigue Test | |
| O: Metals ― High Cycle Fatigue Test | |
| N: Metals ― Impact Test | |
| M3: Metals ― Rockwell Hardness | |
| L1a: Metals ― Grain Size | |
| L1b: Metals ― Inclusion Content (Except Maraging 250 and ML340) |
|
| L1e: Metals ― Contamination on Ti Alloy (Alpha Case) | |
| XL3: Metals ― Macrographic Examinations | |
| L2a: Metals ― SEM: Fracture Surface Analysis |
Pratt & Whitney
| Scope of Approval | MCL Commercial Lab |
|---|---|
| Initial App. Date | April 9, 2018 |
| App. Date | - |
| Exp. Date | - |
| Test Code & Test Item | 1: Tensile (Room Temp.) |
| 2: Tensile (Elevated Temp.) | |
| 3: Stress Rupture | |
| 4: Creep Strain | |
| 5: Hardness （Brinell and Rockwell） | |
| 7: Metallographic Examination | |
| 7a: Microstructure/Grainsize | |
| 7h: Heat Treat （Only test for heat-treated specimens） |
