Approvals
| Company name | Vendor code | Approval date | Approval expiry | Approval scope |
|---|---|---|---|---|
| NADCAP | 3619201088 | 2016-09-23 | 2023-08-31 | • Chemistry (Al, Co, Cu, Fe, Ni & Ti base) - XRF, OES, ICP, GFAA, Combustion, Fusion • Room Temperature Tensile • Elevated Temperature Tensie • Stress Rupture • Creep • Compression • Impact • High Cycle Fatigue • Low Cycle Fatigue • Fracture Toughness • Bend • Metallography (Micro & Macro) • Microhardness (Knoop & Vickers) • Hardness (Brinell & Rockwell) • Corossion (Stress Corrosion, Exfoliation, ASTM A 262 Practice A & E) • Mechanical Test Specimen Preparation • Heat Treating of Specimens |
| ISO/IEC 17025 | 1772 | 2017-03-17 | 2024-04-30 | • Room Temperature Tensile • Elevated Temperature Tensile • Notch Tensile • Compression • Hardness • Microhardness • Impact • Creep • Stress Rupture • Stress Corrosion • Metallurgical Analysis • Chemical Analysis |
| Airbus France | N/A | 2018-10-17 | None | • Tensile Test Room Temperature • Chemical Analysis • Micrography • Hardness Test • Chapy Impact at Room Temperature • Fracture Toughness • Stress Corrosion • Charpy Impact at -30°C • Electrical Conductivity • Macrography |
| Bell Helicopter | 400130 | None | None | • IH1 (Electrical Conductivity) • LA (Room Temp Tensile) • LB (Elevated Temp Tensile) • LC (Stress Rupture) • LD (Impact) • LE (Fatigue) • LF (Fracture Toughness) • LG (Metallography) • LH (Microhardness) • LJ (Intergranular Corrosion) • LK (Stress Corrosion) • LM (Spectroscopy) • LN (Hydrogen) • LO (Nitrogen) • LP (Oxygen) • LQ (Boron) |
| Boeing | 560942 | None | None | • Determination of Hydrogen in Titanium • Mechanical Testing • Metallurgical Testing • Temper Inspection of Aluminium Alloys (only applies to BAC 5602) • Fracture Toughness Testing |
| Cessna | 280311 | None | None | • Etch Inspection of Ground or Machined Steel Parts • Electrical Conductivity Testing of Aluminium Alloys • Nital Etch Inspection-Steel Parts • Hardness Testing of Metals • Decarburization and Carburization - Determination Procedure |
| General Electric | T2981 | 2021-08-13 | 2024-07-31 | • A - Room Temperature Tensile • B - Elevated Temperature Tensile • C - Stress Rupture • XH - Cyclic Rupture • XA - Creep • P - Fracture Toughness • M - Hardness • D - Gravimetric Chemical Analysis • F - Instrumental Quantitative Analysis • G - Carbon Determination • H - Sulfur (Sulphur) Determination • I - Hydrogen Analysis • J - Nitrogen Analysis • K - Oxygen Analysis • XD - Trace Element Anaysis • L - Metallography • XF - Inclusion Content • XZ - E50TF133 Grain Size • Q - Corrosion and Stress Corrosion • Z - Low Stress Grinding • XG - Heat Treatment of Specimens |
| Goodrich Corporation | GMBSQA-306-01 | None | None | • Chemical • Mechanical • Metallographic Testing |
| Gulfstream | 2018-01-11 | 2025-06-27 | • 5.02 Material Test, Chemical • 5.03 Material Test, Metallographic • 5.04 Material Test, Physical • 5.05 Material Test, Spectrographic • 5.11 Material Test, Salt Spray ASTM B 117 | |
| Honeywell Engines & Systems | 04160 | None | None | • Chemical Analysis • Heat Treat of Specimens • Macrohardness • Mechanical Testing • Mechanical Test Specimen Preparation • Metallography • Corrosion and Oxidation |
| IHI Corporation | - | - | 2023-10-14 | • Room Temperature Tensile • Elevated Temperature Tensile • Metallography • Hydrogen (Combustion or Fusion) |
| Kawasaki Heavy Industry (KHI) | KHI 4952 | 2022-11-03 | 2024-11-03 | • J-ISAJT-F005 • Code A Room Temperature Tensile • Code B Elevated Temperature Tensile • Code O High Cycle Fatigue • Code Y Low Cycle Fatigue • Code F3 OES • Code G2 Hydrogen • Code L Porosity • Code L8 Alpha Case • Code L13 Grain Size • Code M1 Brinell Hardness • Code Z X-Ray • Limitation: PW1100GJM Parts only |
| Kaman Aerospace Corporation | 044756-00 | None | None | • Inspection-Chemical • Inspection-Mechanical • Inspection-Metallurgical • Inspection System Requirements |
| Lockheed Martin | PQA272 | None | None | Fracture Toughness Testing |
| MD Helicopters Inc | N/A | None | None | • MDP1-1 – Heat Treat of Steels (Approved/Test Samples Only) • MDP1-2 – Heat Treat of Aluminum Alloys (Approved/Test Samples Only)• MDP6-16 – Control and Inspection of Aluminum Alloy Forgings (Approved/None)• MDP6-25 – Procedures for Determining the Mechanical and Chemical Properties of Metallic Materials (Approved/None) |
| Messier-Bugatti-Dowty | N/A | None | None | Laboratory Testing |
| MTU | 50000054 | 2018-05-02 | 2023-05-31 | • Low Stress Grinding and Polishing • Metallogragraphic Evaluation (micros) MTV1127 • RT tensile Testing ASTM E8, EN2002-1 • ET Tensile Testing ASTM E21, EN2002-2 • HCF Testing ASTM E466 • Stress Rupture Testing ASTM E139 • Creep Testing ASTM E139 • Headness Testing (HB2, HRC, HV) • Machine of Standard Specimen • Creep Testing ASTM E139 |
| Northrop Grumman | N/A | None | None | • Process Specification IT-49 • Process Specification IT-72 |
| Pratt and Whitney | N/A | None | None | • Tensile, Room Temperature • Tensile, Elevated Temperature • Stress Rupture • Creep Rupture • Hardness • Impact • Metallographic Examination • Wet Chemical Analysis • OES Quantitative Spectographic Analysis |
| Rolls Royce Plc | 87680 | None | None | • Manufacture of Test Pieces • Mechanical Testing as specified in CME 5021 and in accordance with MSRR 9922 • Chemical analysis in accordance with MSRR 9920 • MSRR 9969-Brinell and Rockwell • Metallography, Corrosion Testing, RPS 953 |
| Sikorsky | SP859 | None | None | • Lab 1 (ASTM E8) Incl. Sub-Size • Lab 3 (ASTM E882, E 743, E 851, E 548) • Lab 5 (ASTM E3) Incl. Titaninum • Lab 7 (ASTM E10, E18, E384) |
| Safran | 001 | 2017-01-26 | None | • (A) Room Temperature Tensile • (B) Elevated Temperature Tensile • (C) Stress Rupture • (F1) X-Ray Fluorescence • (F2) ICP Analysis • (F3) Optical Emission • (F5) Furnace Graphite Atomic Absorption (Trace Elements) • (G) Carbon Content • (H) Sulfur Content • (I) Hydrogen Analysis • (J) Nitrogen Content • (N) Impact Test • (XG) Heat Treatment of Test Pieces |