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The video systems include a camera, display, and lights. Video is the recording, reproducing, or broadcasting of moving visual images as illustrated in Figure 1. A camera video imaging system is a system composed of a camera and a monitor, as well as other components, in which the monitor provides a real-time or near real-time visual image of the scene captured by the camera. Such systems are capable of providing remote views to the pilot and can therefore be used to provide improved visibility (for example, coverage of blind spots). In general, camera video systems may be used in the pilot’s work position for purposes of improving airplane and corresponding environmental visibility. Examples of aircraft video system applications include: Ground maneuver or taxi camera system Flight deck entry video surveillance system Cargo loading and unloading Cargo compartment livestock monitoring Monitoring systems that are used to track the external, internal, and security functions of an
A-20B Exterior Lighting Committee
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
This specification covers cored and uncored open cell latex foam rubber sheets, molded and hand- built shapes having good shock-absorbing, vibration-damping, and comfort cushioning characteristics (see 6.1).
AMS P Polymeric Materials Committee
This specification covers discontinuously reinforced aluminum alloy (DRA) metal matrix composites (MMC) made by mechanical alloying of the 2124A powder and SiC particulate, which is then consolidated by hot isostatic pressing (HIP) into shapes less than 62 square inches (0.04 m2) in cross-sectional area (see 8.12).
AMS D Nonferrous Alloys Committee
This specification covers the requirements for surface bonded laminated shim stock.
AMS D Nonferrous Alloys Committee
This specification covers the requirements for glass fabric base plastic honeycomb core materials for aircraft structural applications, including aircraft exterior parts, such as radio and radar antenna housings, and other parts.
AMS P17 Polymer Matrix Composites Committee
This specification presents the requirements for one type of a heat-sensitive recording paper, in roll form, that furnishes permanent marking or tracing on one side.
AMS P Polymeric Materials Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification establishes requirements for three types of corrosion-preventative coatings for protection of aircraft integral fuel tanks.
AMS G8 Aerospace Organic Coatings Committee
This SAE Standard encompasses connectors between two cables or between a cable and an electrical component and focuses on the connectors external to the electrical component. This document provides environmental test requirements and acceptance criteria for the application of connectors for direct current electrical systems of 60 V or less in the majority of heavy-duty applications typically used in off-highway machinery. Severe applications can require higher test levels or field-testing on the intended application.
CTTC C2, Electrical Components and Systems
This SAE Recommended Practice defines the minimum performance specifications for sensors used within anthropomorphic test devices (ATDs) when performing impact tests per SAE J211. It is intended that any agency proposing to conduct tests in accordance with SAE J211 shall be able to demonstrate that the transducers they use would meet the performance requirements specified in this document.
Safety Test Instrumentation Standards Committee
This specification establishes the engineering requirements for producing an anodic coating on titanium and titanium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a low expansion iron alloy in the form of sheet or strip 0.250 inch (6.35 mm) and under in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Information Report applies to structural integrity, performance, drivability, and serviceability of personally licensed vehicles not exceeding 10000 pounds GVWR such as sedans, crossovers, SUVs, MPVs, light trucks, and van-type vehicles that are powered by gas and alternative fuel such as electric, plug-in hybrid, or hybrid technologies. It provides engineering direction to vehicle modifiers in a manner that does not limit innovation, and it specifies procedures for preparing vehicles to enhance safety during vehicle modifications. It further provides guidance and recommendations for the minimum acceptable design requirements and performance criteria on general and specific structural modifications, thereby allowing consumers and third-party payers the ability to obtain and purchase equipment that meets or exceeds the performance and safety of the OEM production vehicle.
Adaptive Devices Standards Committee
This SAE Standard covers normalized electric-resistance welded flash-controlled single-wall, low-carbon steel pressure tubing intended for use as pressure lines and in other applications requiring tubing of a quality suitable for bending, double flaring, beading, forming, and brazing. Material produced to this specification is not intended to be used for single flare applications, due to the potential leak path caused by the Inside Diameter (ID) weld bead or scarfed region. Assumption of risks when using this material for single flare applications shall be defined by agreement between the producer and purchaser. This specification also covers SAE J356 Type-A tubing. The mechanical properties and performance requirements of SAE J356 and SAE J356 Type-A are the same. The SAE J356 or SAE J356 Type-A designation define unique manufacturing differences between coiled and straight material. Nominal reference working pressures for this tubing are listed in ISO 10763 for metric tubing, and SAE
Metallic Tubing Committee
This specification covers electric furnace steel bars and reforging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 microns) and that no powder (0.0 wt.%) greater than 40 mesh (425 microns) is allowed.
AMS AM Additive Manufacturing Metals
This specification establishes the requirements for a waterborne, corrosion-inhibiting, chemical- and solvent-resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 °F (93 to 99 °C).
AMS G8 Aerospace Organic Coatings Committee
This specification covers grease for use on aircraft wheel bearings. It also defines the quality control requirements to assure batch conformance and materials traceability and the procedures to manage and communicate changes in the grease 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 2.2, 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 a grease is approved for use in their equipment. Approval and/or certification for use of a specific grease in aero and aero-derived marine and industrial applications is the responsibility of the individual equipment builder and/or governmental authorities and is not implied by compliance with or qualification to this
AMS M Aerospace Greases Committee
This specification covers the requirements for procurement of one grade of powdered molybendum disulfide to be used in lubricants and greases for surfaces where boundary conditions exist.
AMS B Finishes Processes and Fluids Committee
This specification covers treated aluminum core material for structural sandwich construction.
AMS P17 Polymer Matrix Composites Committee
This specification covers steel forgings suitable for use in the construction of aircraft/aerospace equipment, special ordnance, and related accessories.
AMS E Carbon and Low Alloy Steels Committee
This specification covers the requirements for electroless (autocatalytic chemical reduction) deposition of nickel-phosphorous alloy coatings on metal and composite surfaces.
AMS B Finishes Processes and Fluids Committee
This specification covers pasted-mica electrical insulation for molded armature slot bases, commutator insulation, shells, heating elements, and other similar insulating purposes.
AMS P Polymeric Materials Committee
This specification covers class L, low dielectric constant (12 or under), ceramic, electrical, insulating compounds, for use in electronic, communications, and allied electrical equipments, and the grading thereof (see 6.1).
AMS P Polymeric Materials Committee
This SAE Recommended Practice is intended as the definition of a standard test, but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No. 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutches with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. The specific purpose of this document is to define a 3600 rpm Stepped Power Test for the evaluation of wet friction system performance variation as a function of power level. This procedure uses an initial engagement speed of 3600 rpm and is intended as a standard procedure for common use by both suppliers and end users. The only variables selected by the supplier or user of the friction system are: a Friction Material b Fluid c Reaction Plates These three variables must be clearly identified when reporting the results of using this
Automatic Transmission and Transaxle Committee
This SAE Standard specifies requirements for a foaming liquid cleaning compound which, when diluted with water 1:9 v/v, is suitable for cleaning the soiled exterior of Service aircraft. The cleaning compound may be applied by spraying, either as foam or liquid, by brushing or by swabbing. The surfaces to be cleaned may be unpainted metal or surfaces painted with glossy or matt schemes, including strippable acrylic paint complying with DTD 5599. This Standard includes tests to limit specific forms of corrosion that affect aircraft structural materials.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This standard specifies a method for testing and measuring the deflection of friction materials assemblies and compressibility of friction materials. This standard applies to disc brake pad assemblies and its coupons or segments, brake shoe lining and its coupons or segments, and brake blocks segments used in road vehicles. This SAE test method is consistent in intent with the ISO 6310 and the JIS 4413.
Brake Linings Standards Committee
This specification covers a solvent cleaning compound in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a water-base cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers upholstery fabrics woven from nylon and treated for fire retardation.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers a general purpose disinfectant in the form of a concentrated liquid to be used diluted in accordance with label instructions.
AMS J Aircraft Maintenance Chemicals and Materials Committee
This specification covers two types of aircraft glass window cleaners in the form of a ready-to-use liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
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