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This document provides background information, rationale, and data (both physical testing and computer simulations) used in defining the component test methods and similarity criteria described in SAE Aerospace Recommended Practice (ARP) 6330. ARP6330 defines multiple test methods used to assess the effect of seat back mounted IFE monitor changes on blunt trauma to the head and post-impact sharp edge generation. The data generated is based on seat and IFE components installed on type A-T (transport airplane) certified aircraft. While not within the scope of ARP6330, generated test data for the possible future development of surrogate target evaluation methods is also included
Aircraft Seat Committee
This SAE Aerospace Recommended Practice (ARP) provides recommendations for: The audit process in general A list of specific areas of attention to be audited Maintaining the test facility in such a manner that it meets audit requirements
EG-1E Gas Turbine Test Facilities and Equipment
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry
Engine Power Test Code Committee
This specification covers tungsten in the form of forgings produced from billets processed by isostatically cold pressing, utilizing hydrogen reduced tungsten powder, and high-temperature sintering
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
This specification covers tantalum in the form of sheet, strip, plate, and foil up through 0.1875 inch (4.75 mm), inclusive
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of forgings, 6.000 inches (152.40 mm) and under in cross-sectional thickness and forging stock of any size
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars up through 6.000 inches (152.40 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 6.000 inches (152.40 mm), inclusive and stock for forging of any size
AMS G Titanium and Refractory Metals Committee
This specification covers aircraft quality, commercially pure titanium and alpha, alpha-beta and beta titanium alloy rolled or forged bar and reforging stock products
AMS G Titanium and Refractory Metals Committee
This list of terms, with accompanying photomicrographs where appropriate, is intended as a guide for use in the preparation of material specifications
AMS G Titanium and Refractory Metals Committee
This specification covers tungsten in the form of pressed, sintered, and wrought sheet, strip, plate, and foil
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet and strip up to 0.143 inches (3.63 mm), inclusive, in nominal thickness
AMS G Titanium and Refractory Metals Committee
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer
AMS G Titanium and Refractory Metals Committee
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of blocks, blanks or shapes
AMS G Titanium and Refractory Metals Committee
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm), inclusive
AMS G Titanium and Refractory Metals Committee
This specification covers anethylene propylene (EPM) rubber in the form of molded rings
AMS CE Elastomers Committee
This specification covers a titanium alloy in the form of wire for welding filler metal
AMS G Titanium and Refractory Metals Committee
This specification covers vacuum-arc-cast molybdenum in the form of wrought round bars
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of forgings up to 4.000 inches (101.60 mm) inclusive and forging stock
AMS G Titanium and Refractory Metals Committee
This specification covers aircraft quality titanium and titanium alloy metal sheet, strip and plate products
AMS G Titanium and Refractory Metals Committee
This test method provides procedures for exposing specimens of elastomer material (slab form) representative to those used in gas turbine engines to aviation lubricants under extended duration and engine relevant thermal conditions. For AS5780 requirements the time is at least 1800 hours and temperatures are 100 °C to 160 °C. Positive volume change is an indication of specimen swell and subsequent negative volume change is an indication of specimen deterioration, both properties are important in the evaluation of the compatibility of the lubricant with elastomers used in the construction of the gas turbine
E-34 Propulsion Lubricants Committee
An oil sample is placed into an open top glass vial which is then inserted into a stainless steel pressure vessel. The vessel is then sealed, pressurized, and placed into a heated aluminum block bath for 18 hours. At the end of the 18 hour time period, the vessel is removed from the heat source and allowed to cool to room temperature at which time the contents of the vial are filtered and the total sediment is reported as milligrams of sediment per 20 mL of oil
E-34 Propulsion Lubricants Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4 inches (101.6 mm
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes from vacuum hot pressed powder
AMS G Titanium and Refractory Metals Committee
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of seamless tubing
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars and forgings up through 10.000 inches (254.00. mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 79.0 in2 (506.45 cm2) and forging stock of any size (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification defines basic physical, chemical, and performance limits for 5 cSt grades of gas turbine engine lubricating oils used in aero and aero-derived marine and industrial applications, along with standard test methods and requirements for laboratories performing them. It also defines the quality control requirements to assure batch conformance and materials traceability, and the procedures to manage and communicate changes in oil formulation and brand. This specification invokes the Performance Review Institute (PRI) product qualification process. Requests for submittal information may be made to the PRI at the address in Appendix D Section D.2, referencing this specification. Products qualified to this specification are listed on a Qualified Products List (QPL) managed by the PRI. Additional tests and evaluations may be required by individual equipment builders before an oil is approved for use in their equipment. Approval and/or certification for use of a specific gas
E-34 Propulsion Lubricants Committee
This specification covers a titanium alloy in the form of sheet 0.020 to 0.1874 inch (0.51 to 4.760 mm), inclusive, in nominal thickness. (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products
AMS G Titanium and Refractory Metals Committee
Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder
AMS G Titanium and Refractory Metals Committee
This specification covers a tantalum alloy in the form of sheet, strip, and plate from 0.010 through 0.250 inch (0.25 through 6.35 mm), inclusive
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides and stock of any size for forging or flash welded rings
AMS G Titanium and Refractory Metals Committee
This specification covers a columbium (niobium) alloy in the form of sheet, strip, and plate
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.7
AMS G Titanium and Refractory Metals Committee
This specification covers the heat treatment of titanium and titanium alloy mill products (raw material), including wrought and cast products, by material producers. This specification also covers furnace equipment requirements, test procedures, and general information for heat treating procedures, heat treating temperatures, and material test procedures for the heat treatment of titanium and titanium alloys. It also describes procedures that, when followed, have produced the desired properties within the limitations of the respective alloys
AMS G Titanium and Refractory Metals Committee
This SAE Recommended Practice specifies graphic symbols for operator controls, gauges, tell-tales, indicators, instructions, and warning against risks in small craft and for engines and other equipment intended to be used in small craft
Marine Technical Steering Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.6 mm) nominal thickness
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal cross-sectional thickness and of stock for forging of any size
AMS G Titanium and Refractory Metals Committee
This specification covers flash welded rings made of titanium and titanium alloys
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of welding wire
AMS G Titanium and Refractory Metals Committee
This SAE Aerospace Information Report (AIR) establishes guidance for the specification of formulated lubricant properties which contribute to the lubricating function in bearings, gears, clutches, and seals of aviation propulsion and drive systems
E-34 Propulsion Lubricants Committee
This specification covers a titanium alloy in the form of prealloyed powder
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by cold isostatic pressing (CIP) and sintering
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet and strip 0.125 inch (3.18 mm) and under in nominal thickness
AMS G Titanium and Refractory Metals Committee
This specification covers a titanium alloy in the form of seamless tubing
AMS G Titanium and Refractory Metals Committee
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