ABS5441

REQUEST QUOTE ABS5441 is an Airbus Specification for Nickel 718 Plate similar to AMS 5596   Nickel 718 (UNS N07718) is an austenitic nickel-based superalloy. Nickel / Inconel 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. Nickel 718 is used in applications that requireContinue reading “ABS5441”

ABS5440

REQUEST QUOTE ABS5440 is an Airbus Specification for Nickel 718 Plate similar to AMS 5596 Nickel 718 (UNS N07718) is an austenitic nickel-based superalloy. Nickel / Inconel 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. Nickel 718 is used in applications that require highContinue reading “ABS5440”

BMS7-415

REQUEST QUOTE BMS 7-415 is a NICKEL 718 Boeing Material Specification for “NICKEL ALLOY 718 PLATE” under AMS 5596 Nickel 718 is an austenitic nickel-based superalloy. Alloy 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. Alloy 718 is used in applications that require highContinue reading “BMS7-415”

BMS7-240

REQUEST QUOTE LIVE STOCK LIST BMS 7-240 is a 15-5 PH Boeing Material Specification for “15-5PH (UNS S15500) SHEET, PLATE, AND STRIP”  15-5 PH per AMS 5862 stainless steel is a martensitic precipitation-hardening stainless steel with approximately 15% Chromium and 5% Nickel. It has high strength, high hardness, and excellent corrosion resistance. Strength can beContinue reading “BMS7-240”

AMS 4905

REQUEST QUOTE AMS 4905 specification for “Titanium Alloy, Damage-Tolerant Grade Plate, 6Al – 4V, Beta Annealed” The AMS 4905 specification covers 6Al-4V titanium alloy plate in the beta-annealed condition. Beta annealing is done at temperatures above the β transus of the alloy being annealed. To prevent excessive grain growth, the temperature for β annealing shouldContinue reading “AMS 4905”

BAC 5616

BAC 5616 is a Boeing Specification regarding the “HEAT TREATMENT OF NICKEL-BASE AND COBALT-BASE ALLOYS”   With regards to D1-4426 Quality Process Lists, Fighter Jet Metals can help you to ensure that you procure and source the correct material that has been heat treated to BAC 5616. Please visit our Request For Quote page and let usContinue reading “BAC 5616”

AMS 5537

REQUEST QUOTE L605 per AMS 5537 Cobalt Alloy, Corrosion and Heat-Resistant, Sheet, Strip, Foil, and Plate 52Co – 20Cr – 10Ni – 15W Solution Heat Treated The AMS 5537 specification covers L605 corrosion and heat-resistant cobalt alloy in the form of sheet, strip, foil, and plate.

AMS 5536

REQUEST QUOTE Technical Information for Hastelloy X per AMS 5536 Hastelloy X per AMS 5536 is a nickel-chromium-iron-molybdenum alloy with outstanding strength and oxidation resistance at temperatures to 2200°F (1200°C). Matrix stiffening provided by the molybdenum content results in high strength in a solid-solution alloy having good fabrication characteristics. Used in gas turbines, industrial furnaces,Continue reading “AMS 5536”

AMS 5597

REQUEST QUOTE Technical Information on Nickel 718 per AMS 5597 Nickel 718 per AMS 5597, Also known as Inconel 718, is a precipitation-hardenable nickel-chromium alloy also containing significant amounts of iron, niobium and molybdenum along with lesser amounts of aluminum and titanium. It combines corrosion resistance and high strength with outstanding weldability, including resistance toContinue reading “AMS 5597”