Approvals
| Company name | Vendor code | Approval date | Approval expiry | Approval scope |
|---|---|---|---|---|
| A2LA | 1772 | 2010-02-19 | 2012-04-30 | • Room Temperature Tensile • Elevated Temperature Tensile • Notch Tensile • Compression • Hardness • Microhardness • Impact • Creep • Stress Rupture • Stress Corrosion • Salt Spray • Metallurgical Analysis • Chemical Analysis • Hydrogen Embrittlement |
| Airbus France | N/A | 2009-03-17 | 2010-12-31 | • 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 | 001149 | 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 |
| Goodrich Corporation | GMBSQA-306-01 | None | None | • Chemical • Mechanical • Metallographic Testing |
| Honeywell Engines & Systems | 04160 | None | None | • Chemical Analysis • Heat Treat of Specimens • Macrohardness • Mechanical Testing • Mechanical Test Specimen Preparation • Metallography • Corrosion and Oxidation |
| Kaman Aerospace Corporation | 044756-00 | None | None | • Inspection-Chemical • Inspection-Mechanical • Inspection-Metallurgical • Inspection System Requirements |
| Lockheed Martin | PQA272 | None | None | Fracture Toughness Testing |
| Messier-Dowty Inc. | N/A | None | None | Laboratory Testing |
| Northrop Grumman | N/A | None | None | • Process Specification IT-49 • Process Specification IT-72 |
| NADCAP | 128426 | 2009-08-10 | 2011-10-31 | • Chemical Laboratory • Mechanical Laboratory • Metallography and Microhardness • Hardness Testing • Corossion • Mechanical Test Specimen Preparation • Heat Treating of Specimens |
| 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) • Lab 7 (ASTM E10, E18, E92, E384) • Lab 5 (ASTM E3) |
| SNECMA Moteurs | 001 | 2009-11-18 | 2012-12-31 | • (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 |