| NADCAP |
3619214052 |
9/23/2016 |
11/30/2026 |
- 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 |
3/17/2017 |
4/30/2026 |
- Room Temperature Tensile
- Elevated Temperature Tensile
- Notch Tensile
- Compression
- Hardness
- Microhardness
- Impact
- Creep
- Stress Rupture
- Stress Corrosion
- Metallurgical Analysis
- Chemical Analysis
|
| Airbus France |
276093 |
11/30/2022 |
N/A |
- 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 |
N/A |
N/A |
- 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)
|
| BÖHLER - voestalpine BÖHLER Aerospace GmbH & Co KG |
300359/2023 |
8/29/2023 |
8/28/2026 |
Material Testing |
| Boeing |
560942 |
N/A |
N/A |
- Determination of Hydrogen in Titanium
- Mechanical Testing
- Metallurgical Testing, Temper Inspection of Aluminium Alloys (only applies to BAC 5602)
- Fracture Toughness Testing
|
| Cessna |
280311 |
1/26/2009 |
N/A |
- 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 |
7/31/2024 |
4/30/2026 |
- 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 Corp. |
GMBSQA-306-01 |
N/A |
N/A |
- Chemical
- Mechanical
- Metallographic Testing
|
| Gulfstream |
N/A |
1/11/2018 |
6/27/2025 |
- 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 |
N/A |
N/A |
- Chemical Analysis
- Heat Treat of Specimens
- Macrohardness
- Mechanical Testing
- Mechanical Test Specimen Preparation
- Metallography, Corrosion and Oxidation
|
| IHI Corp. Aero-Engine & Space Operations |
IHI-F0070 |
12/26/2023 |
1/14/2027 |
- Room Temperature Tensile
- Elevated Temperature Tensile
- Metallography
- Hydrogen (Combustion or Fusion)
|
| Kawasaki Heavy Industry (KHI) |
KHI 4952 |
11/3/2022 |
11/3/2024 |
- 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 Corp. |
044756-00 |
N/A |
N/A |
- Inspection-Chemical
- Inspection-Mechanical
- Inspection-Metallurgical
- Inspection System Requirements
|
| Lockheed Martin |
PQA272 |
N/A |
N/A |
Fracture Toughness Testing |
| MD Helicopters Inc |
8700 |
1/28/2021 |
 |
- 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/N/A)
- MDP6-25 – Procedures for Determining the Mechanical and Chemical Properties of Metallic Materials (Approved/N/A)
|
| Messier-Bugatti-Dowty |
N/A |
N/A |
N/A |
Laboratory Testing |
| MTU Aero Engines |
50000054 |
7/28/2023 |
3/31/2026 |
- 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 - Aerospace
Northrop Grumman - Space - SSSD |
90049888 |
2/12/2020 |
 |
- Process Specification IT-49
- Process Specification IT-72
|
| Parker Aerospace |
N/A |
8/22/2019 |
N/A |
|
| Pratt and Whitney |
 |
6/8/2020 |
Ongoing via MCL |
- Tensile, Room Temperature
- Tensile, Elevated Temperature
- Stress Rupture
- Creep Rupture, Hardness
- Impact, Metallographic Examination
- Wet Chemical Analysis
- OES Quantitative Spectographic Analysis
|
| Robinson Helicopter Company |
149702 |
4/17/2023 |
4/17/2025 |
Physical/Chemical Testing Analysis |
| Rolls Royce Plc |
200723 |
8/4/2014 |
N/A |
- 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
|
| Safran |
MDM502857 |
4/15/2019 |
N/A |
- (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
- (K) Oxygen Content
- (L1) Optical Micrography
- (L1a) Grain Size Determination
- (M1) Brinell Hardness
- (M3) Rockwell Hardness
- (N) Impact Test
- (P) Determination of KIC
- (XA) Creep Elongation Tests
- (XL2) Macrographic Inspection
- (XG) Heat Treatment of Test Pieces
- (Z2) Sample Machining except Fatigue
|
| Siemens |
N/A |
7/19/2022 |
N/A |
|
| Sikorsky |
SP859 |
10/2/2018 |
N/A |
- 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)
|
