Aircraft-grade nickel superalloys for jet engines, turbines, and aerospace structures. AMS certified materials with AS9100 quality systems.
✈️ AS9100 Certified • 🔬 AMS Specifications • 📋 FAA-PMA Available • 🚛 Expedited Shipping
Complete range of AMS-certified nickel superalloys for aircraft applications
| Alloy | AMS Specifications | Service Temperature | Primary Applications | Key Properties | Availability |
|---|---|---|---|---|---|
| Inconel 718 | AMS 5662, 5663, 5664 | Up to 1300°F (704°C) |
| High strength, age-hardenable, excellent fatigue resistance | Stock & Custom |
| Hastelloy X | AMS 5536, 5754, 5798 | Up to 2200°F (1204°C) |
| Oxidation resistance, thermal stability, fabricability | Stock & Custom |
| Inconel 625 | AMS 5666, 5837, 5581 | Up to 2000°F (1093°C) |
| Corrosion resistance, weldability, thermal fatigue resistance | Stock & Custom |
| Inconel 617 | AMS 5887, 5888 | Up to 2100°F (1149°C) |
| Creep resistance, oxidation resistance, metallurgical stability | Custom Order |
| Hastelloy C-276 | AMS 5750, 5751 | Up to 1900°F (1038°C) |
| Chemical resistance, low carbon content, versatile | Stock & Custom |
| Waspaloy | AMS 5708, 5709, 5710 | Up to 1500°F (816°C) |
| High strength, creep resistance, thermal stability | Custom Order |
Selecting the right alloy for your operating temperature range
Ambient to low temperature
Recommended Alloys:
Most nickel alloys suitable
Moderate temperature service
Recommended Alloys:
Inconel 625, 718, Hastelloy C-276
Intermediate temperature
Recommended Alloys:
Inconel 718, 625, Hastelloy X
High temperature service
Recommended Alloys:
Hastelloy X, Inconel 617, Waspaloy
Extreme temperature
Recommended Alloys:
Hastelloy X, Inconel 617 (specialized)
Real-world applications and material solutions for aircraft components
High temperature, centrifugal stress, thermal cycling
Creep-resistant superalloys with excellent high-temperature strength
Inconel 718, Waspaloy, Hastelloy X
1200-2200°F
Thermal shock, oxidation, vibration fatigue
Oxidation-resistant alloys with thermal fatigue resistance
Inconel 625, Hastelloy X, Inconel 617
1400-2000°F
Fuel compatibility, stress corrosion cracking, weight
Corrosion-resistant alloys with excellent fabricability
Hastelloy C-276, Inconel 625, Inconel 718
400-1000°F
Fatigue loading, environmental exposure, weight optimization
High-strength alloys with fatigue resistance and durability
Inconel 718, Inconel 625, Hastelloy C-276
200-800°F
Meeting the highest standards for aerospace material supply
Aerospace Quality Management System
Scope: Complete quality system for aerospace manufacturing
Importance: Required for all aerospace suppliers
National Aerospace and Defense Contractors Accreditation Program
Scope: Special process certifications (heat treat, NDT, chemical processing)
Importance: Ensures consistent special process quality
Federal Aviation Administration Parts Manufacturer Approval
Scope: Authorization to manufacture aircraft parts
Importance: Required for aircraft component manufacturing
Aerospace Material Specifications
Scope: Material composition, properties, and testing requirements
Importance: Defines aerospace material standards
Download comprehensive guides and specifications for aerospace nickel alloys
Comprehensive guide for selecting the right nickel alloy for aerospace applications
Quick reference chart for common AMS specifications and their applications
Detailed mechanical and physical properties at elevated temperatures
Side-by-side comparison of key aerospace nickel alloys
Meeting the demanding requirements of aerospace manufacturing
Full aerospace quality management system compliance
Complete compliance with aerospace material specifications
AOG support and critical delivery capabilities
Complete material certifications and mill test reports
Get competitive pricing on aerospace-grade nickel superalloys with complete documentation and certification packages.