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2018-06-21 ...
  • June 21-22, 2018 (8:30 a.m. - 4:30 p.m.) - El Segundo, California
  • October 11-12, 2018 (8:30 a.m. - 4:30 p.m.) - Greenville, South Carolina
  • November 8-9, 2018 (8:30 a.m. - 4:30 p.m.) - London, United Kingdom
Training / Education Classroom Seminars
The avionics hardware industry world-wide is now commonly required to follow DO-254 Design Assurance Guidance for Airborne Electronic Hardware for literally all phases of development: Safety, Requirements, Design, Logic Implementation, V&V, Quality Assurance, etc. The DO-254 standard is a companion to the software DO-178B standard; however, there are many differences between hardware and software which must be understood. This basic course introduces the intent of the DO-254 standard for commercial avionics hardware development.
2018-06-21 ...
  • June 21, 2018 (8:30 a.m. - 4:30 p.m.) - Hamburg, Germany
Training / Education Classroom Seminars
The challenges associated with using composites as a replacement for aluminum reside primarily in the complex manufacturing processes and technologies for fabricating composite parts. The high cost of composites material and its manufacturing complexity have been inhibitors to the wide transfer of this technology to the non-aerospace market. The search for solutions to high manufacturing costs and efficient manufacturing processes have resulted in intense research by government, aerospace industry companies, and space agencies worldwide.
2018-03-21 ...
  • March 21-22, 2018 (8:30 a.m. - 4:30 p.m.) - Durham, North Carolina
  • May 23-24, 2018 (8:30 a.m. - 4:30 p.m.) - Warrendale, Pennsylvania
  • September 10-11, 2018 (8:30 a.m. - 4:30 p.m.) - Warrendale, Pennsylvania
Training / Education Classroom Seminars
The requirements of the AS9120, Rev. B, EN9120B and JIAQ9120B Standards have significantly changed and are based on the NEW ISO9001:2015 Standard. This two-day training program is designed to provide individuals with the knowledge necessary to understand and comprehend the NEW requirements described in AS9120 Rev. B, Quality Management Systems – Requirements for Aviation, Space, and Defense Distributors. The course includes classroom instruction combined with class exercises to further reinforce concepts and definitions now required by the standard.
2018-02-12 ...
  • February 12-13, 2018 (8:30 a.m. - 4:30 p.m.) - Cleveland, Ohio
  • July 9-10, 2018 (8:30 a.m. - 4:30 p.m.) - Warrendale, Pennsylvania
  • November 12-13, 2018 (8:30 a.m. - 4:30 p.m.) - El Segundo, California
Training / Education Classroom Seminars
Part 21 is the FAA regulation that provides the regulatory framework to conduct certification of products and parts. This includes the engineering, airworthiness, production and quality systems. The aerospace industry is hinged around compliance with Part 21; however, comprehension of Part 21 and its role in civil certification is challenging. This course is designed to provide participants with an understanding of the processes that encompass aircraft certification, including compliance with FARs, certification procedures and post certification responsibilities.
2017-12-12 ...
  • December 12-13, 2017 (8:30 a.m. - 4:30 p.m.) - Puyallup, Washington
  • March 5-6, 2018 (8:30 a.m. - 4:30 p.m.) - Durham, North Carolina
  • June 18-19, 2018 (8:30 a.m. - 4:30 p.m.) - Warrendale, Pennsylvania
Training / Education Classroom Seminars
Individuals responsible for quality management system, implementation, and transition to the AS9100:2016 series of standards for Aviation, Space, and Defense will require an understanding of the requirements for the preparation and execution of the audit process as defined in these revised standards. Management and implementers of AS9100:2016 Rev. D within these organizations must also be aware of what these changes may mean for their company.
2017-12-04 ...
  • December 4-5, 2017 (8:30 a.m. - 4:30 p.m.) - Puyallup, Washington
  • August 30-31, 2018 (8:30 a.m. - 4:30 p.m.) - Cleveland, Ohio
Training / Education Classroom Seminars
The requirements for producing an FAA approved replacement part can be daunting. Understanding the steps required in the FAA Parts Manufacturer Approval (PMA) process can greatly streamline the approval life-cycle and reduce unnecessary costs and delays, thereby shortening the time and cost to market. This course is designed for those organizations and individuals interested in designing and manufacturing replacement parts for civil aviation aircraft. This two-day course covers the crucial subjects and steps of the FAA-PMA approval process.
2017-11-17
WIP Standard
ARP1515B
To establish a recommended practice for the minimum protrusion of external threaded fasteners through one piece all metal self-locking nuts.
2017-11-17
WIP Standard
AS1177B
To establish the acceptance criteria of surface discontinuities of bolts and screws. This acceptance criteria establishes the location, number, size, depth, and type of surface discontinuities that are permitted on bolts and screws as revealed by visual, magnetic particle, or fluorescent penetrant inspection.
2017-11-17
WIP Standard
AS3568A
No scope available.
2017-11-17
WIP Standard
AS1349B
This SAE Aerospace Standard (AS) covers helical coil locking screw thread inserts made from formed wire in which the inner surface of the coil, after assembly, provides threads of standard Unified 60 degrees form as specified on the assembly drawing. This document also covers the performance requirements of the locking feature of the insert which will retain United ANSI B1.1 (UN Profile) or AS8879 (UNJ Profile) external threaded parts.

To establish the performance requirements of helical coil locking screw thread inserts for use in fastening systems utilizing a lubricant which induces a low coefficient of friction between insert and fastener.

2017-11-17
WIP Standard
AS1229D
This SAE Aerospace Standard (AS) covers helical coil stud locking screw thread inserts made from formed wire in which the inner surface of the coil, after assembly provides threads of standard Unified 60° form as specified on the assembly drawing. This standard also covers the performance requirements of the locking feature of the insert which will retain Unified ANSI B1.1 (UN Profile) or AS8879 (UNJ Profile) external threaded parts.

To establish the performance requirements of helical coil stud locking screw thread inserts.

2017-11-17
WIP Standard
AS4959A
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering Systems as UNS S66286. The following specification designations and their properties are covered: AS4959 140 ksi minimum ultimate tensile strength at room temperature 70 ksi stress-rupture strength at 1200 degrees F; AS4959-1 140 ksi minimum ultimate tensile strength at room temperature 84 ksi minimum ultimate shear strength at room temperature.
2017-11-17
WIP Standard
AS82C
This SAE Aerospace Standard (AS) defines an external thread with a rounded root radius based on a minimum root radius of .108 x Pitch.
2017-11-17
WIP Standard
AS919A
To establish external dimensions for shafts requiring shallow grooves and internal dimensions for mating locking devices when used with parts dimensionally equivalent to Bearing Retaining Spanner Nuts, MS172236 thru MS172270.
2017-11-17
WIP Standard
MA3378D
This specification covers metric bolts and screws made from a corrosion and heat resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS NO7001. The following specification designations and their properties are covered: MA3378 - 1210 MPa minimum ultimate tensile strength at room temperature MA3378 - 520 MPa stress-rupture strength at 730 °C MA3378-1 - 1210 MPa minimum ultimate tensile strength at room temperature MA3378-1 - 726 MPa minimum ultimate shear strength at room temperature
2017-11-17
WIP Standard
MA1937A
This procurement specification covers alloy steel and corrosion and heat resistant steel free running metric nuts of the following types, styles and classes: (a) Types: Hex nut plain, standard height; Hex nut plain, shear height; Hex nut slotted, standard height; Hex nut slotted, shear height; (b) Styles: Washer face; Double chamfered; Castellated; (c) Classes: 516 MPa axial strength, min (shear height nuts); 600 MPa axial strength, min (shear height nuts) 860 MPa axial strength, min; 1000 MPa axial strength, min.
Viewing 1 to 30 of 21733

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