SAE International Datasheets for Standards and Technical Documents

Standards and technical documents includes standards, codes, regulation, handbooks, manuals, comprehensive guides and other formal publications. Standards, codes, and regulation establish uniform specifications, procedures or technical criteria.
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Product Name	Notes
Fuel Level Control Valves and Systems -- AIR1660C	A fuel level control valve/system controls the quantity of fuel in a tank being filled or emptied on the aircraft. This document provides a general familiarization with these mechanisms (e.g.,...
Fuel Level Control Valves/Systems -- AIR1660 Fuel Level Control Valves/Systems -- AIR1660B	A fuel level control valve/system controls the quantity of fuel in a tank being filled or emptied. This document provides a general familiarization with these mechanisms (e.g. forms they take,...
PERFORMANCE OF LOW PRESSURE RATIO EJECTORS FOR ENGINE NACELLE COOLING -- AIR1191 Performance of Low Pressure Ratio Ejectors for Engine Nacelle Cooling -- AIR1191A	A general method for the preliminary design of a single, straight-sided, low subsonic ejector is presented. The method is based on the information presented in References 1, 2, 3, and...
Spacecraft Life Support Systems -- AIR1168/14 Spacecraft Life Support Systems -- AIR1168/14A	A life support system (LSS) is usually defined as a system that provides elements necessary for maintaining human life and health in the state required for performing a prescribed mission.
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines -- AIR1419A	AIR1419 "Inlet Total Pressure Distortion Considerations for Gas Turbine Engines" documents engineering information for use as reference material and for guidance. Inlet total-pressure distortion and other forms of flow distortion...
Estimation of Total Error in Altimetry -- AIR1608A Estimation of Total Error in Altimetry -- AIR1608B	AIR1608 ESTIMATION OF TOTAL ERROR IN ALTIMETRY proposes a method of estimating overall error of altimetry in order to provide a basis for safe vertical separation of aircraft.
AIRBORNE INTERNAL INTERFACE STANDARDS FOR MODERATE BIT RATE* DIGITAL TIME DIVISION-MULTIPLEX SYSTEMS -- AIR1189 Airborne Internal Interface Standards for Moderate Bit Rate Digital Time Division-Multiplex Systems -- AIR1189A	All electrical and electronic signals within an aircraft are potential candidates for multiplexing, although the determination of whether or not they are multiplexed is a matter for individual system consideration.
METALLIC SEAL RINGS FOR HIGH TEMPERATURE RECIPROCATING HYDRAULIC SERVICE -- AIR1077 Metallic Seal Rings for High Temperature Reciprocating Hydraulic Service -- AIR1077A	An attempt has been made to consider all features of seal ring design including configuration, materials, hardness, dimensions, surface finishes, surface treatment, leak testing, and general quality. In addition to...
COMPARISON OF GROUND-RUNUP AND FLYOVER NOISE LEVELS -- AIR1216	Because of the special circumstances under which these tests were conducted, it is necessary to carefully define the limitations on the validity of the results. The measurements and the comparisons...
Crew Oxygen Requirements Up to a Maximum Altitude of 45,000 Ft. -- AIR1069A Crew Oxygen Requirements Up to a Maximum Altitude of 45,000 Ft. -- AIR1069B	Determine the required minimum oxygen concentration to be breathed prior to, during, and after a loss of cabin pressurization, and
Electromagnetic Interference on Aircraft from Jet Engine Charging -- AIR1147A Electromagnetic Interference on Aircraft from Jet Engine Charging -- AIR1147B	Engine charging of aircraft has been observed for many years. This SAE Aerospace Information Report (AIR) reviews the history of observations, physical characteristics, and possible techniques for minimizing the effects.
Groove Design - Metal Face Seal -- AIR1108 Groove Design - Metal Face Seal -- AIR1108A	Groove designs presented herein are applicable for use with machined or formed metal seals which are similar in configuration to those shown in figure 3 , which operate under internal...
Heat and Mass Transfer and Air-Water Mixtures -- AIR1168/2 Heat and Mass Transfer and Air-Water Mixtures -- AIR1168/2A	Heat transfer is the transport of thermal energy from one point to another. Heat is transferred only under the influence of a temperature gradient or temperature difference. The direction of...
Spacecraft Thermal Balance -- AIR1168/12 Spacecraft Thermal Balance -- AIR1168/12A	In the design of spacecraft, heat transfer becomes a criterion of operation to maintain structural and equipment integrity over long periods of time. The spacecraft thermal balance between cold space...
In-Flight Thrust Determination -- AIR1703A	In-Flight Thrust Determination, SAE AIR1703 reviews the major aspects of processes that may be used for the determination of in-flight thrust (IFT). It includes discussions of basic definitions, analytical and...
Aircraft Damage Caused by Ground Support Equipment -- AIR1589C	Incidents where a piece of ground support equipment or personnel damages an aircraft under the control of ground or maintenance operations that requires corrective action by aircraft maintenance personnel. Operations...
FINAL REPORT ON COLD STARTING OF RECIPROCATING AIRCRAFT ENGINES -- AIR13A	INTRODUCT ION Conventional internal conbustion a i r c r a f t engines require the same basic conditions for starting in cold weather as they do in warn weather.
FUEL GAGING SYSTEM ACCURACIES -- AIR1184	It is intended to provide capacitance gaging system "specifiers" with the necessary tools to make value judgements concerning the various errors typically encountered in systems of this type. Thus, in...
CONCURRENT DESIGN OF ENGINES AND SPECIFICATIONS OF STARTING SYSTEMS FOR HELICOPTERS -- AIR1296	It is recommended that all helicopter engine development programs include an evaluation of engine starting requirements. The evaluation should include starting requirement effects on helicopter weight, cost, and mission effectiveness.
Aerothermodynamic Test Instrumentation and Measurement -- AIR1168/5 Aerothermodynamic Test Instrumentation and Measurement -- AIR1168/5A	Like the technologies to which it contributes, the science of instrumentation seems to be expanding to unlimited proportions. In considering instrumentation techniques, primary emphasis was given in this section to...
AIRCRAFT CARGO DOOR OPENING/SILL DETAILS FOR GROUND SUPPORT EQUIPMENT INTERFACE -- AIR1673 Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface -- AIR1673A Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface -- AIR1673B	Manufacturers/design ers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and...
THE ADVANCED ENVIRONMENTAL CONTROL SYSTEM (AECS) COMPUTER PROGRAM FOR STEADY STATE ANALYSIS AND PRELIMINARY SYSTEM SIZING -- AIR1706A The Advanced Environmental Control System (AECS) Computer Program for Steady State Analysis and Preliminary System Sizing -- AIR1706B	Many different computer programs have been developed to determine performance capabilities of aircraft environmental control systems, and to calculate size and weight tradeoffs during preliminary design. Many of these computer...
HANDBOOK OF HYDRAULIC METRIC CALCULATIONS -- AIR1657A Handbook of Hydraulic Metric Calculations -- AIR1657B	Metric (SI and CGS) and English units related to aerospace hydraulics are summarized. Conversion of units is provided as required. Fundamental fluid properties and physical laws governing fluid motion, pressure...
Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems -- AIR1616B	MIL-STD-1290, 14 CFR 27.952, and 14 CFR 29.952 provide crash resistant fuel system design and test criteria that significantly minimize fuel leaks and occurrence of post-crash fire in survivable impacts.
AGS883 4 B.A. Studs -- AGS883-5 AGS884 2 B.A. Studs -- AGS884-5 AGS885 1/4" B.S.F. Studs -- AGS885-5 AGS886 5/16" B.S.F. Studs -- AGS886-5 AGS887 3/8" B.F.S. Studs -- AGS887-5 AGS888 Drain Cock -- AGS888-5 AGS889 Drainage Hole Eyelets, (Marine Type) -- AGS889-4 AGS893 Standard Countersunk Head Woodscrews -- AGS893-3 AGS894 Standard Round-Head Woodscrews -- AGS894-3 AGS895 Clip for Spearing Tubes -- AGS895-4 AGS897 Ferrules, Steel Wire for Elastic Cord -- AGS897-4 AGS899 Collars (Mild Steel) -- AGS899-5 AGS900 Metal Couplings (Aluminium Alloy) 5/16 Light Type for Automatic Controls Only -- AGS900-20 AGS904 Pipe Couplings (Aluminium Alloy) Outer Sleeve -- AGS904-27 AGS905 Pipe Coupling Aluminium Alloy Inner Sleeve -- AGS905-25 AGS908 Reducing Union Body. (Light Alloy) -- AGS908-9 AGS910 Lubrication Nipple -- AGS910-7 AGS920 Ferrules. (Non-Corrodible.) for Screwed Rod -- AGS920-3 AGS921 Screwed Rod. (Non-Corrodible) -- AGS921-3 AGS934 Ferrules (Plated) for Screwed Rod -- AGS934-4 AGS935 Screwed Rod. (5.2, 5.11. Or D.T.D. 153) (Plated) -- AGS935-5 AGS937 R.A.E. Petrol Filters, Shallow Sump Type -- AGS937-12 AGS939 R.A.E. Petrol Filters -- AGS939-15 AGS946 Bright Washers. (Steel, Non-Corrodible) -- AGS946-4 AGS947 Special Bright Washers, (Steel, Non-Corrodible) -- AGS947-4 AGS948 Plugs Flanged (Aluminium Alloy) -- AGS948-16 AGS949 Double Ended Union Body (Steel) -- AGS949-17 AGS950 Metal Couplings Reducing Union Body (Steel) -- AGS950-16 AGS952 Pipe Couplings Collar -- AGS952-18 AGS954 Metal Couplings. (Steel). Outer Sleeve -- AGS954-17 AGS955 Metal Couplings (Steel) Inner Sleeve -- AGS955-19 AGS957 Union Lock Nuts (Light Alloy) -- AGS957-6 AGS958 Female Flanges (Light Alloy) -- AGS958-11 AGS959 Special Female Flanges (Light Alloy) -- AGS959-11 AGS963 Oil Thermometer Pocket, 7/8" B.S. Pipe -- AGS963-9 AGS964 Oil Thermometer Pocket. 1 1/4" B.S. Pipe -- AGS964-9 AGS965 Oil Thermometer Pocket. 1 1/2" B.S. Pipe -- AGS965-8 AGS966 Cock. (No. 2 Size) with Diffuser -- AGS966-7 AGS970 Washers. (Aluminium Alloy) -- AGS970-7 AGS974 Oil Thermometer Pocket. 3/8" B.S. Pipe -- AGS974-8 AGS977 Male Flanges (Bolted) (Aluminium Alloy) -- AGS977-10 AGS978 Male Flanges (Bolted) (Steel) -- AGS978-9 AGS980 Female Flanges (Bolted) (Aluminium Alloy) -- AGS980-6 AGS981 Female Flanges. (Bolted.) (Steel) -- AGS981-5 AGS986 Female Flanges (Bolted) with Spigot (Aluminium Alloy) -- AGS986-6 AGS987 Female Flanges (Bolted.) with Spigot (Steel) -- AGS987-6 AGS995 Studs 2 B.A. High Duty -- AGS995-2 AGS996 Studs 1/4" B.S.F. High Duty -- AGS996-3 AGS997 Studs 3/16 " B.S.F. High Duty -- AGS997-2 AGS998 Studs 3/8" B.S.F. High Duty -- AGS998-2	No scope available.
Aircraft Damage Caused by Ground Support Equipment -- AIR1589A Aircraft Damage Caused by Ground Support Equipment -- AIR1589B	Only those incidents where a piece of ground support equipment directly associated with the "turnaround" servicing of an aircraft was involved are reviewed. Specifically excluded are those incidents that occurred...
AGS912 BOW, D-SHAPED (FOR CHAIN SHACKLE) -- AGS912-8	Scope is unavailable.
Recommended Part Numbering Guidelines for Fluid System Components Inch System of Measurements -- AIR1590A	Scope Unavailable
HANDBOOK OF HYDRAULIC METRIC CALCULATIONS -- AIR1657	SI and other metric units related to aerospace hydraulics are summarized. Conversion of English units is provided as required. Fundamental fluid properties and physical laws governing fluid motion and pressure...
Environmental Degradation of Textiles -- AIR1490C	Since cargo restraint devices made with textiles should have a predictable service life, there should be data available so that predictions can be made. This document compiles available information on...
Environmental Degradation of Textiles -- AIR1490B	Since the ULD device containing textiles should have a predictable service life, there should be data available so that predictions can be made. This document compiles available information on textiles...
ENVIRONMENTAL DEGRADATION OF TEXTILES -- AIR1490A	Since the ULD device containing textiles should have a predictable service life, there should be data available so that predictions can be made. This technical report compiles available information on...
Chemical Oxygen Supplies -- AIR1133A Chemical Oxygen Supplies -- AIR1133B	Solid chemical oxygen supplies of interest to aircraft operations are "chlorate candles" and potassium superoxide (KO 2 ). Chlorate candles are used in passenger oxygen supply units and other emergency...
ANTI-BLOW-BY DESIGN PRACTICE FOR CAP STRIP SEALS -- AIR1243	Suggestions for piston Cap Strip Seal side-wall notch design and other anti-blow-by design details are described.
ANTI BLOWBY DESIGN PRACTICE FOR CAP-STRIP SEALS -- AIR1243A	Suggestions for piston cap-strip seal side wall notch design and other anti blowby design details are described.
1992 Bibliography on Fuel Handling and Contamination in Aircraft Systems -- AIR1196 1992 Report on Flip Chip and Beam Lead Bonding for Electronic Circuits -- AIR1141 1992 Space Technology Available for Transfer to Civil Environmental Protection and Pollution Control -- AIR1246 A Method of Ground Resonance Testing for Helicopters -- AIR12 ACOUSTIC EFFECTS PRODUCED BY A REFLECTING PLANE -- AIR1327 AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY -- AIR1489 AIRCRAFT ACCESSORY DRAG TORQUE DURING ENGINE STARTS -- AIR1087 AIRCRAFT ACCESSORY DRAG TORQUE DURING ENGINE STARTS -- AIR1087A AIRCRAFT ENGINE AND ACCESSORY DRIVES AND FLANGE STANDARDS -- AIR1160A AIRCRAFT ENGINE AND ACCESSORY DRIVES AND FLANGE STANDARDS -- AIR1160B AIRCRAFT NOISE RESEARCH NEEDS -- AIR1079 AIRLINE TOW TRACTOR - BAGGAGE/CARGO FACTORS FOR DESIGN CONSIDERATION -- AIR1316 Acoustic Effects Produced by a Reflecting Plane -- AIR1327A Airborne Monitoring of Commercial Transport Aircraft, Fluid System and Equipment Performance -- AIR1155 BIBLIOGRAPHY OF REFERENCES PERTAINING TO THE EFFECTS OF OXYGEN ON IGNITION AND COMBUSTION OF MATERIALS -- AIR1169 BIBLIOGRAPHY OF REFERENCES PERTAINING TO THE EFFECTS OF OXYGEN ON IGNITION AND COMBUSTION OF MATERIALS -- AIR1169A BRAKE DYNAMICS -- AIR1064 BRAKE DYNAMICS -- AIR1064A BRAKE DYNAMICS -- AIR1064B Bibliography - Lightning and Precipitation Static -- AIR1208 CABLING GUIDELINES FOR ELECTROMAGNETIC COMPATIBILITY -- AIR1394 CHEMICAL OXYGEN GENERAL INFORMATION -- AIR1133 CLAMP MATERIAL, INJECTION MOLDED -- AIR1397 CREW OXYGEN REQUIREMENTS UP TO A MAXIMUM ALTITUDE OF 45, 000 FT. -- AIR1069 DESIGNING WITH ELASTOMERS FOR USE AT LOW TEMPERATURES -- AIR1387 DESIGNING WITH ELASTOMERS FOR USE AT LOW TEMPERATURES -- AIR1387A DESIGNING WITH ELASTOMERS FOR USE AT LOW TEMPERATURES, NEAR OR BELOW GLASS TRANSITION -- AIR1387B DESIRABLE CHARACTERISTICS FOR HELICOPTER ENGINES -- AIR16 DESIRED CHARACTERISTICS FOR HELICOPTER WHEELS, TIRES AND BRAKES -- AIR15 Desired Characteristics for Helicopter Wheels, Tires and Brakes -- AIR15A ELECTROMAGNETIC INTERFERENCE ON AIRCRAFT FROM JET ENGINE CHARGING -- AIR1147 ENVIRONMENTAL DEGRADATION OF TEXTILES USED IN AIR CARGO RESTRAINT EQUIPMENT -- AIR1490 ESTIMATION OF TOTAL ERROR IN ALTIMETRY -- AIR1608 EVALUATION OF HEADPHONES FOR DEMONSTRATION OF AIRCRAFT NOISE -- AIR1115 EVALUATION OF HELICOPTER TURBINE ENGINE LINEAR VIBRATION ENVIRONMENT -- AIR1289 FAA REGULATIONS COVERING THE USE OF OXYGEN IN AIRCRAFT -- AIR1389 FINAL REPORT ON COLD STARTING OF AIRCRAFT ENGINES -- AIR13 FLUID SYSTEM COMPONENT SPECIFICATION CRITERIA -- AIR1082 FUEL LEVEL CONTROL VALVES/SYSTEMS -- AIR1660A Flight Compartment Glare -- AIR1151 GAS ENERGY LIMITED STARTING SYSTEMS -- AIR1467 GAS ENERGY LIMITED STARTING SYSTEMS -- AIR1467A HELICOPTER AND V/STOL AIRCRAFT NOISE MEASUREMENT PROBLEMS -- AIR1286 HIGH TENSION EXCITER OUTPUT VOLTAGE MEASUREMENT USING CATHODE-RAY OSCILLOSCOPE -- AIR1092 HOSE ASSEMBLY IDENTIFICATION PRACTICES -- AIR1698 HYDRAULIC ENERGY LIMITED ENGINE STARTING SYSTEMS -- AIR1466 HYDRAULIC SYSTEM SURVIVABILITY -- AIR1083 House Noise-Reduction Measurements for Use in Studies of Aircraft Flyover Noise -- AIR1081 House Noise-Reduction Measurements for Use in Studies of Aircraft Flyover Noise -- AIR1081A IDENTIFICATION AND CODING OF FLUID AND ELECTRICAL PIPING SYSTEM FUNCTIONS -- AIR1273 INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES -- AIR1419 INSTALLATION OF LIQUID OXYGEN SYSTEMS IN CIVIL AIRCRAFT -- AIR1223 In-Flight Thrust Determination -- AIR1703 Installation and Use of Equilateral Triangle Cross-Section Hydraulic O-Ring Seal Backup Rings (Dyna-Baks) -- AIR1186 Installation and Use of Equilateral Triangle Cross-Section Hydraulic O-Ring Seal Backup Rings (Dyna-Baks) -- AIR1186A Installation of Liquid Oxygen Systems in Civil Aircraft -- AIR1223A Installation of Liquid Oxygen Systems in Civil Aircraft -- AIR1223B Interior Contours, Main Deck Cargo Compartments, Jet Powered Cargo Airplanes -- AIR1044 Introduction to Pressure Suite Assemblies -- AIR1103 Lightning Protection and Static Electrification -- AIR1406 MATERIALS FOR FLUID SYSTEMS COMPONENTS AND THEIR INTERNATIONAL EQUIVALENTS -- AIR1564 METHODS OF ACHIEVING ELECTROMAGNETIC COMPATIBILITY OF GAS TURBINE ENGINE ACCESSORIES, FOR SELF-PROPELLED VEHICLES -- AIR1425 MINIMIZATION OF ELECTROSTATIC HAZARDS IN AIRCRAFT FUEL SYSTEMS -- AIR1662 MINIMUM SAFETY REQUIREMENTS FOR SPECIAL PURPOSE AIRLINE GROUND SUPPORT EQUIPMENT -- AIR1375 MINIMUM SAFETY REQUIREMENTS FOR SPECIAL PURPOSE AIRLINE GROUND SUPPORT EQUIPMENT -- AIR1375A MOLDED RIGID PLASTIC PARTS -- AIR1269A Methods for Determining Turbine Engine Nozzle Area -- AIR1627 NUMERAL, LETTER AND SYMBOL DIMENSIONS FOR AIRCRAFT INSTRUMENT DISPLAYS -- AIR1093 OXYGEN SYSTEM MAINTENANCE GUIDE -- AIR1392 PHOSPHATE ESTER AIRCRAFT HYDRAULIC FLUID CONTAMINATION WITH CHLORINE CONTAINING COMPOUNDS -- AIR1416 PRACTICAL METHODS TO OBTAIN FREE-FIELD SOUND PRESSURE LEVELS FROM ACOUSTICAL MEASUREMENTS OVER GROUND SURFACES -- AIR1672 PRACTICAL METHODS TO OBTAIN FREE-FIELD SOUND PRESSURE LEVELS FROM ACOUSTICAL MEASUREMENTS OVER GROUND SURFACES -- AIR1672A PREDICTION METHOD FOR LATERAL ATTENUATION OF AIRPLANE NOISE DURING TAKEOFF AND LANDING -- AIR1751 PREDICTION PROCEDURE FOR NEAR-FIELD AND FAR-FIELD PROPELLER NOISE -- AIR1407 PROCEDURE FOR THE CALCULATION OF BASIC EMISSION PARAMETERS FOR AIRCRAFT TURBINE ENGINES -- AIR1533 Practical Methods to Obtain Free-Field Sound Pressure Levels from Acoustical Measurements Over Ground Surfaces -- AIR1672B Practical Methods to Obtain Free-Field Sound Pressure Levels from Acoustical Measurements Over Ground Surfaces -- AIR1672C Prediction Method for Lateral Attenuation of Airplane Noise During Takeoff and Landing -- AIR1751A Prediction Procedure for Near-Field and Far-Field Propeller Noise -- AIR1407A RADIOISOTOPE POWER SYSTEMS -- AIR1213 RAMP DE-ICING -- AIR1335 RECOMMENDED PRACTICE FOR MEASUREMENT OF STATIC MECHANICAL STIFFNESS PROPERTIES OF AIRCRAFT TIRES -- AIR1380 REPORT ON AIRCRAFT ENGINE CONTAINMENT -- AIR1537 Radioisotope Power Systems -- AIR1213A SAFETY CRITERIA FOR PNEUMATIC STARTING SYSTEMS -- AIR1639 SOME FACTORS AFFECTING VISIBILITY OF AIRCRAFT NAVIGATION LIGHTS -- AIR1106 Structural Characteristics of Aircraft Tubing -- AIR17 THE MEASUREMENT OF TRAINEE PERFORMANCE IN SIMULATORS AND PART-TASK TRAINERS -- AIR1054 THE MEASUREMENT OF TRAINEE PERFORMANCE IN SIMULATORS AND PART-TASK TRAINERS -- AIR1054A THESAURUS FOR FUEL SYSTEM COMPONENTS -- AIR1615 TRANSFILLING & MAINTENANCE OF OXYGEN CYLINDERS -- AIR1059 TRANSFILLING & MAINTENANCE OF OXYGEN CYLINDERS -- AIR1059A TRANSPARENT AREA WASHING SYSTEMS FOR AIRCRAFT -- AIR1102 UNCERTAINTY OF IN-FLIGHT THRUST DETERMINATION -- AIR1678 UPPER FREQUENCY MEASUREMENT BOUNDARY FOR EVALUATION OF SHIELDING EFFECTIVENESS IN CYLINDRICAL SYSTEMS -- AIR1700 VERIFICATION OF LANDING GEAR DESIGN STRENGTH -- AIR1494	Technical Standard
FLUID SYSTEM COMPONENT SPECIFICATION PREPARATION CRITERIA -- AIR1082A	The "Scope" section may be a very brief statement describing the coverage of the specification for a simple device, or it may require a long description of limiting parameters for...
AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER -- AIR1326 Aircraft Fuel System Vapor-Liquid Ratio Parameter -- AIR1326A	The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system...
FOUR WHEEL DRIVE AIRCRAFT TOW TRACTORS - FACTORS FOR DESIGN CONSIDERATION -- AIR1363	The AIR is presented in two parts. The first part is simply a summarization of design factors that must be considered in establishing performance requirements. The second part consists of...
Braking System Dynamics -- AIR1064D	The aircraft landing gear is a complex multi-degree of freedom dynamic system, and may encounter vibration or dynamic response problems induced by braking action. The vibratory modes can be induced...
ANIMAL ENVIRONMENT IN CARGO COMPARTMENTS -- AIR1600 Animal Environment in Cargo Compartments -- AIR1600A	The environmental factors of prime importance in the transport of animals in aircraft are air temperature, humidity and carbon dioxide concentration, and of course space (or volume) limitations. Secondary factors...
A GUIDE FOR THE SELECTION OF QUICK-DISCONNECT COUPLINGS FOR AEROSPACE FLUID SYSTEMS -- AIR1047 A GUIDE FOR THE SELECTION OF QUICK-DISCONNECT COUPLINGS FOR AEROSPACE FLUID SYSTEMS -- AIR1047A A GUIDE FOR THE SELECTION OF QUICK-DISCONNECT COUPLINGS FOR AEROSPACE FLUID SYSTEMS -- AIR1047B A GUIDE FOR THE SELECTION OF QUICK-DISCONNECT COUPLINGS FOR AEROSPACE FLUID SYSTEMS -- AIR1047C	The factors involved in the selection of a quick-disconnect are grouped into the following classifications for the purpose of discussion: (a) Functional considerations. (b) Weight considerations. (c) Environmental performance factors.
A Guide for the Selection of Quick-Disconnect Couplings for Aerospace Fluid Systems -- AIR1047D A Guide for the Selection of Quick-Disconnect Couplings for Aerospace Fluid Systems -- AIR1047E	The factors involved in the selection of a quick-disconnect are grouped into the following classifications for the purpose of discussion: a Functional considerations. b Weight considerations. c Environmental performance factors.
Thermodynamics of Incompressible and Compressible Fluid Flow -- AIR1168/1 Thermodynamics of Incompressible and Compressible Fluid Flow -- AIR1168/1A Thermodynamics of Incompressible and Compressible Fluid Flow -- AIR1168/1B	The fluid flow treated in this section is isothermal, subsonic, and incompressible. The effects of heat addition, work on the fluid, variation in sonic velocity, and changes in elevation are...
Bibliography - Lossy Filters -- AIR1500	The following bibliography on lossy filters for use on electrical and electronic systems was prepared by the Lossy Filter Subcommittee AE-4C.2 of the Society of Automotive Engineers. The bibliography is...
TRANSMISSION INTERLOCKS -- AIR1361 Transmission Interlocks -- AIR1361A	The following recommendations and suggestions are made for consideration for procurement of new equipment, or modification to existing equipment where practical. Excluded from this AIR is mobile ground equipment, such...
FLUID-SYSTEM-COMPONENT SPECIFICATION PREPARATION CRITERIA -- AIR1082B Fluid-System-Component Specification Preparation Criteria -- AIR1082C	The importance of adequate component procurement specifications to the success of a hardware development program cannot be overemphasized. Specifications which are too stringent can be as detrimental as specifications which...
Aircraft Engine Fuel Feed and Transfer Component Pressure Definitions -- AIR1749	The information in this document is limited to aircraft engine fuel feed, refueling, and transfer components (reference 2.1 ). It is assumed that isothermal, liquid fluid conditions exist, herein referred...
Aircraft Fuel System Pressure Definitions -- AIR1749A	The information in this document is limited to aircraft engine fuel feed, refueling, and transfer components (see 2.1 ). It is assumed that isothermal, liquid fluid conditions exist, herein referred...
PATTERNS OF O-RING FAILURES -- AIR1707 Patterns of O-Ring Failures -- AIR1707C Patterns of O-ring Failures -- AIR1707A Patterns of O-ring Failures -- AIR1707B	The information presented herein describes the commonly observed patterns of O-ring failure by means of both text and illustration. Possible causes and corrective actions are indicated for alleviating the problem.
Aircraft Nosewheel Steering/Centering Systems -- AIR1752A	The intent of this AIR is twofold: (1) to present descriptive summary of aircraft nosewheel steering and centering systems, and (2) to provide a discussion of problems encountered and "lessons...
BRAKE DYNAMICS -- AIR1064C	The landing gear is a complex multi-degree of freedom dynamic system and may encounter vibration problems induced by braking action. The vibratory modes can be induced by several frictional characteristics...
CUSHION TOW HITCHES TEST -- AIR1353 CUSHION TOW HITCHES TEST -- AIR1353A Cushion Tow Hitches Test -- AIR1353B Cushion Tow Hitches Test -- AIR1353C	The main purpose of this test was to determine the application advantages of cushion tow hitches in comparison to the commonly used rigid tow hitch type fitted on heavy aircraft...
Spacecraft Boost and Entry Heat Transfer -- AIR1168/11 Spacecraft Boost and Entry Heat Transfer -- AIR1168/11A	The prediction of vehicle temperatures during ascent through the earth's atmosphere requires an accurate knowledge of the aerodynamic heating rates occurring at the vehicle surface. Flight parameters required in heating...
Aerospace Pressurization System Design -- AIR1168/7 Aerospace Pressurization System Design -- AIR1168/7A	The pressurization system design considerations presented in this AIR deal with human physiological requirements, characteristics of pressurization air sources, methods of controlling cabin pressure, cabin leakage control, leakage calculation methods,...
Aerospace Ground Equipment Criteria for a Propellant Transfer Unit -- AIR1129	The primary purpose of a Propellant Transfer Unit (PTU) is to temperature-conditio n and weigh a specific amount of propellant, and transfer if to a vehicle propellant tank. A secondary...
Interface Protective Devices - Ground Equipment to Aircraft -- AIR1558A	The protective device hereinafter called a "fender" is intended to serve its purpose during normal aircraft servicing and prevent damage during docking contact rather than aggressive impact.
INTERFACE PROTECTIVE DEVICES - GROUND EQUIPMENT TO AIRCRAFT -- AIR1558	The protective device hereinafter called a "fender," is intended to serve its purpose during normal aircraft servicing and prevent damage during docking contact rather than agressive impact.
ELECTROMAGNETIC COMPATIBILITY ON GAS TURBINE ENGINES FOR AIRCRAFT PROPULSION -- AIR1423 Electromagnetic Compatibility on Gas Turbine Engines for Aircraft Propulsion -- AIR1423A	The purpose of this AIR is to acquaint the aerospace industry with problems in attaining electromagnetic compatibility on gas turbine engines, particularly as used in aircraft. It is also the...
Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays -- AIR1093A Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays -- AIR1093B	The purpose of this AIR is to provide recommendations for the minimum dimensions of characters and symbols used in aircraft instrument dials and panel displays as related to the conditions...
WASHER, THERMAL COMPENSATING, METRIC SERIES -- AIR1754 Washer, Thermal Compensating, Metric Series -- AIR1754A Washer, Thermal Compensating, Metric Series -- AIR1754B	The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
Transfilling and Maintenance of Oxygen Cylinders -- AIR1059B	The purpose of this document is to list the best available information and guidelines for the qualification of personnel who are responsible for the filling of fixed or portable aircraft...
Torque Tightening Threaded Fasteners -- AIR1471A Torque Tightening Threaded Fasteners -- AIR1471B	The purpose of this SAE Aerospace Information Report (AIR) is to provide the aerospace propulsion industry with recommended assembly torque limits for commonly used aircraft propulsion system threaded fasteners when...
Aircraft Fuel Weight Penalty Due to Air Conditioning -- AIR1168/8 Aircraft Fuel Weight Penalty Due to Air Conditioning -- AIR1168/8A	The purpose of this section is to provide methods and a set of convenient working charts to estimate penalty values in terms of take-off fuel weight for any given airplane...
Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights -- AIR1106A	The scope of this Aerospace Information Report (AIR) is to discuss factors affecting visibility of aircraft navigation and anticollision lights, enabling those concerned with their use to have a better...
Bibliography of References Pertaining to The Effects of Oxygen on Ignition and Combustion of Materials -- AIR1169B Bibliography of References Pertaining to The Effects of Oxygen on Ignition and Combustion of Materials -- AIR1169C	The scope of this document is to provide a list of documents of types pertaining to the effects of oxygen on ignition and combustion of materials. Consolidating these references in...
Glossary of Technical and Physiological Terms Related to Aerospace Oxygen Systems -- AIR171D	The scope of this document is to provide a list of specialized terms with their meanings. The glossary will assist the use of other documents related to aircraft oxygen equipment...
GENERAL ENVIRONMENTAL REQUIREMENTS FOR DEEP SUBMERSIBLE VEHICLES AND SUBMARINES -- AIR1063	The scope of this HIR is to specify general oceanographic environments. Specific environmental requirements shall be specified in a detail specification. Specific requirements are in the state of constant flux...
Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights -- AIR1106B	The scope of this SAE Aerospace Information Report (AIR) is to discuss factors affecting visibility of aircraft navigation and anticollision lights, enabling those concerned with their use to have a...
SELECTING SLIPPER SEALS FOR HYDRAULIC-PNEUMATIC FLUID POWER APPLICATIONS -- AIR1244 SELECTING SLIPPER SEALS FOR HYDRAULIC-PNEUMATIC FLUID POWER APPLICATIONS -- AIR1244A	The SLIPPER SEAL is defined and the basic types in current use are described. Guide lines for selecting the type of Slipper Seal for a given design requirement are covered...
Ramp De-Icing -- AIR1335A	The specific purpose of this AIR is to provide general background information to better acquaint those who are involved with ramp de-icing of aircraft. Because the wide variance of atmospheric...
RECOMMENDED PRACTICE FOR MEASUREMENT OF STATIC MECHANICAL STIFFNESS PROPERTIES OF AIRCRAFT TIRES -- AIR1380A Recommended Practice for Measurement of Static Mechanical Stiffness Properties of Aircraft Tires -- AIR1380B	The static mechanical stiffness properties of aircraft tires are fundamental to any computation of wheel and landing gear shimmy characteristics, and are important guides in anti-skid system and aircraft wheel...
REPORT ON AIRCRAFT ENGINE CONTAINMENT -- AIR1537A	The study shall be directed to commercial aircraft service and include engine experience in both fixed wing aircraft and helicopters covering the time period from 1962 to the present.
CONVENIENT LOCATION OF OXYGEN MASKS FOR BOTH THE CREW AND PASSENGERS OF AIRCRAFT -- AIR1390 Convenient Location of Oxygen Masks for Both the Crew and Passengers of Aircraft -- AIR1390A Convenient Location of Oxygen Masks for Both the Crew and Passengers of Aircraft -- AIR1390B	There are four basic conditions requiring the dispensing of oxygen through oxygen masks to aircraft occupants in turbine powered aircraft during flight. The following conditions are derived from the Federal...
Cabling Guidelines for Electromagnetic Compatibility -- AIR1394A	These cable practice recommendations tend toward design guidance rather than standardization. EMC achievement tests can be standardized, but the means for achievement should not be constrained. The material can best...
Clamp Loads and Bending Stresses in Aircraft Tubing Installations -- AIR1593	This Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes, fittings and clamps caused by tube deflections encountered in misaligned installations.
GLOSSARY OF TECHNICAL AND PHYSIOLOGICAL TERMS RELATED TO AEROSPACE OXYGEN SYSTEMS -- AIR171C	This Aerospace Information Report (AIR) defines words, terms, and specialized language used in describing the function, design, and operation of aircraft oxygen systems.
FIRE TEST EQUIPMENT FOR FLEXIBLE HOSE AND TUBE ASSEMBLIES -- AIR1377 Fire Test Equipment for Flexible Hose and Tube Assemblies -- AIR1377A Fire Test Equipment for Flexible Hose and Tube Assemblies -- AIR1377B	This Aerospace Information Report (AIR) describes equivalent types of equipment that can perform fire tests in accordance with requirements of AS 1055.
Interface Protective Devices - Ground Equipment to Aircraft -- AIR1558B	This Aerospace Information Report (AIR) discusses damage to aircraft caused by ground equipment contact and suggests methods of protecting against that damage.
High and Extended Vibration Environment -- AIR1557A	This Aerospace Information Report (AIR) documents the vibration areas and vibration spectrum needed in determining electrical connector selection for typical jet aircraft. This AIR defines aircraft areas, the vibration spectrum...
FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS BY PLANAR RESONANT VIBRATION (FREE-FREE BEAM) -- AIR1529 Flexure Testing of Hydraulic Tubing Joints and Fittings by Planar Resonant Vibration (Free-Free Beam) -- AIR1529A Flexure Testing of Hydraulic Tubing Joints and Fittings by Planar Resonant Vibration (Free-Free Beam) -- AIR1529B	This Aerospace Information Report (AIR) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure...
INFORMATION ON ANTISKID SYSTEMS -- AIR1739	This Aerospace Information Report (AIR) has been prepared by a panel of the SAE A-5 Committee and is presented to document the design approaches and service experience from various applications...
ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS -- AIR1667	This Aerospace Information Report (AIR) identifies and summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection. Although various concepts...
AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS -- AIR1664	This Aerospace Information Report (AIR) includes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure and...
Aerospace Information Report for Continuous Flow Oxygen Hose Disconnect Fittings -- AIR1358B Aerospace Information Report for Continuous Flow Oxygen Hose Disconnect Fittings -- AIR1358C	This Aerospace Information Report (AIR) indicates those dimensions, deemed critical by the manufacturer to assure proper mating of disconnect hose fittings. The dimensions are critical, but not necessarily complete, in...
Ground Equipment Rebuild Program -- AIR1599A	This Aerospace Information Report (AIR) is intended to be concerned with fleet programs rather than programs for individual units. Technical and administrative considerations in developing an approach to a program...
Construction and Calibration of Parallel Plate Transmission Line for Electromagnetic Interference Susceptibility Testing -- AIR1209	This Aerospace Information Report (AIR) is intended to provide information relating to the construction, calibration, and usage of parallel plate transmission lines in electromagnetic compatibility susceptibility testing.
Four Wheel Drive Aircraft Tow Tractors - Factors for Design Consideration -- AIR1363A	This Aerospace Information Report (AIR) is presented in two parts. The first part is simply a summarization of design factors that must be considered in establishing vehicle specifications and design...
STANDARD WORDS FOR TEST PARAGRAPHS FOR TUBE FITTINGS AND TUBE ASSEMBLIES -- AIR1378 STANDARD WORDS FOR TEST PARAGRAPHS FOR TUBE FITTINGS AND TUBE ASSEMBLIES -- AIR1378A Standard Words for Test Paragraphs for Tube Fittings and Tube Assemblies -- AIR1378B Standard Words for Test Paragraphs for Tube Fittings and Tube Assemblies -- AIR1378C	This Aerospace Information Report (AIR) is written as a guide for the wording recommended for use, when applicable, in design and procurement specifications for tube fittings and tube assemblies, both...
EXHAUST EMISSION LIMITS FOR DIESEL ENGINES USED IN AIRCRAFT GROUND SUPPORT EQUIPMENT AT AIRPORT ENVIRONMENTS -- AIR1312	This Aerospace Information Report (AIR) outlines the conditions which diesel engines should meet when installed and used as prime movers for aircraft ground support equipment at commercial airports. All aircraft...
Control of Water Carryover from the Environmental Control System and Condensation on the Structure -- AIR1204A	This Aerospace Information Report (AIR) outlines the design considerations and criteria for the control of water carryover from the environmental control system (ECS) with respect to causes and indicated corrective...
OXYGEN SYSTEM AND COMPONENT CLEANING AND PACKAGING -- AIR1176A Oxygen System and Component Cleaning and Packaging -- AIR1176B	This Aerospace Information Report (AIR) specifies work area details, cleaning methods, test methods, and specifications for oxygen clean parts and packaging materials.
Handling and Installation Practice for Aerospace Hose Assemblies -- AIR1569A	This AIR can be used for the selection, care, handling, installation, and maintenance of hose assemblies for aerospace fluid systems. AIR797 lists characteristics of military and SAE hose, hose assemblies,...
HANDLING & INSTALLATION PRACTICE FOR AEROSPACE HOSE ASSEMBLIES -- AIR1569	This AIR can be used for the selection, care, handling, installation, and maintenance of hose assemblies for aerospace fluid systems.
POWER SOURCES FOR FLUIDIC CONTROLS -- AIR1245	This AIR concerns itself with the end use of Fluidic (or Flueric) control hardware on aerospace vehicle applications. The fluidic control hardware application is viewed as a system comprised of...
HIGH AND EXTENDED VIBRATION ENVIRONMENT -- AIR1557	This AIR defines aircraft vibration areas, the vibration spectrum for those areas and a coupling mechanism recommendation for circular electrical connectors.
ELECTRICAL CONNECTORS AND WIRING, COMPATIBILITY OF -- AIR1329A Electrical Connectors and Wiring, Compatibility of -- AIR1329B	This AIR defines the areas where incompatibility may exist between the selected wire and the electrical connector in which it is terminated and how to design for compatibility. Refer to...
ELECTRICAL CONNECTORS AND WIRING, COMPATIBILITY OF -- AIR1329	This AIR defines the areas where incompatibility may exist between the selected wire and the electrical connector in which it is terminated and how to design for compatibility.
DC Resistivity vs RF Impedance of EMI Gaskets -- AIR1404	This AIR discusses the DC resistivity property of EMI gaskets.
Emc Antennas and Antenna Factors: How to Use Them -- AIR1509	This AIR discusses the use and application of EMC antennas and antenna factors. The relationships between antenna gain, antenna factor, power density (W/m2), and field strength (V/m) are discussed. Some...
AIRCRAFT DAMAGE CAUSED BY GROUND SUPPORT EQUIPMENT -- AIR1589	This AIR examines only those incidents which were caused by ground support equipment used for aircraft handling and servicing and for line maintenance. It does not include damage that occurred...
AEROSPACE INFORMATION REPORT FOR CONTINUOUS FLOW OXYGEN HOSE DISCONNECT FITTINGS -- AIR1358 Aerospace Information Report for Continuous Flow Oxygen Hose Disconnect Fittings -- AIR1358A	This AIR indicates those dimensions, deemed critical by the manufacturer, which are required to be adhered to so that proper mating of the disconnect hose fitting with the correct disconnect...
Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids -- AIR1168/9 Thermophysical Properties of the Natural Environment, Gases, Liquids, and Solids -- AIR1168/9A	This AIR is arranged in the following four sections: 2A - Properties of the Natural Environment 2B - Properties of Gases 2C - Properties of Liquids 2D - Properties of...
THERMOPHYSICAL CHARACTERISTICS OF WORKING FLUIDS AND HEAT TRANSFER FLUIDS -- AIR1168/10 Thermophysical Characteristics of Working Fluids and Heat Transfer Fluids -- AIR1168/10A	This AIR is arranged in the following two sections: 2E - Thermodynamic Characteristics of Working Fluids, which contains thermodynamic diagrams for a number of working fluids currently in use and...
BAROMETRY FOR ALTIMETER CALIBRATION -- AIR1075	This AIR is concerned only with aspects directly relating to available accuracy. While well-designed photoelectric, inductive or capacitive readers and pressure regulators, and other accessories are highly desirable for convenience...
PERMISSIBLE DENT AND CHAFING DAMAGE OF AIRCRAFT HYDRAULIC TUBING -- AIR1388 SERVICE DAMAGE LIMITS FOR AIRCRAFT HYDRAULIC TUBING -- AIR1388A	This AIR is intended to assist in evaluating the serviceability of damaged hydraulic tubing lines. The performance requirements are outlined to which the defect samples were tested. Test methods and...
GROUND EQUIPMENT REBUILD PROGRAM -- AIR1599	This AIR is intended to be concerned with fleet programs rather than programs for individual units. Technical and administrative considerations in developing an approach to a program will be suggested...
PRESTRESSING (AUTOFRETTAGING) OF HYDRAULIC TUBING LINES -- AIR1379 Prestressing (Autofrettaging) of Hydraulic Tubing Lines -- AIR1379A Prestressing (Autofrettaging) of Hydraulic Tubing Lines -- AIR1379B	This AIR is intended to describe and document a process presently in use for proof testing, which at the same time improves the fatigue life of 304 1/8 hard CRES...
AIRCRAFT ENVIRONMENTAL FACTORS FOR DESIGN CONSIDERATION -- AIR1309	This AIR is presented in two parts - the first part, to alert the engineer with respect to the environmental factors which he might have to consider - the second...
FAULT ISOLATION IN ENVIRONMENTAL CONTROL SYSTEMS OF COMMERCIAL TRANSPORTS -- AIR1266	This AIR outlines concepts for the design and use of fault isolation equipment that have general application. However, the specific concern applies only to use with Environmental Control Systems in...
Upper Frequency Measurement Boundary for Evaluation of Shielding Effectiveness in Cylindrical Systems -- AIR1700A	This AIR points out that above a frequency called the "transition frequency," variances associated with the shielding effectiveness measurements can become large. It includes the derivations to demonstrate this. This...
OXYGEN SYSTEM AND COMPONENT CLEANING AND PACKAGING -- AIR1176	This AIR specifies work area details, cleaning methods, test methods, and specifications for oxygen clean parts and packaging materials.
Torque Tightening Metric Screw Threaded Fasteners -- AIR1551A Torque Tightening Metric Screw Threaded Fasteners -- AIR1551B	This AIR supplies information on recommended assembly torque limits for tension type nuts and bolts of the materials and plating combinations given in Table 1 .
TORQUE TIGHTENING METRIC SCREW THREADED FASTENERS -- AIR1551	This AIR supplies information on recommended assembly torque limits for tension type nuts and bolts of the materials and plating combinations given in Table I .
Spectrum Analyzers for Electromagnetic Interference Measurements -- AIR1255	This AIR was prepared to inform the aerospace industry about the electromagnetic interference measurement capability of spectrum analyzers. The spectrum analyzers considered are of the wide dispersion type which are...
Electromagnetic Compatibility (EMC) System Design Checklist -- AIR1221 Electromagnetic Compatibility (EMC) System Design Checklist -- AIR1221A	This checklist is to be used by project personnel to assure that factors required for adequate system electromagnetic compatibility are considered and incorporated into a program. It provides a ready...
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines -- AIR1419B Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines -- AIR1419C	This document addresses many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability. It provides a review of the development of techniques used...
Minimum Safety Requirements for Special Purpose Airline Ground Support Equipment -- AIR1375C Minimum Safety Requirements for Special Purpose Airline Ground Support Equipment -- AIR1375D	This document applies to special purpose equipment which is used in the ground handling, servicing, and maintenance of transport aircraft. Fixed airport facilities and equipment covered under other sections of...
MINIMUM SAFETY REQUIREMENTS FOR SPECIAL PURPOSE AIRLINE GROUND SUPPORT EQUIPMENT -- AIR1375B	This document applies to special purpose equipment, excluding fixed facilities, which is used in the ground handling, servicing, and maintenance of aircraft. Equipment covered under other sections of the Federal...
VEHICLE ELECTRICAL SYSTEMS -- AIR1336	This document considers the following major areas: 1 Major components and their ratings 2 Selection criteria for optimum design balance for electrical systems 3 Effects of operating conditions and environment...
COOLING OF MODERN AIRBORNE ELECTRONIC EQUIPMENT -- AIR1277 Cooling of Modern Airborne Electronic Equipment -- AIR1277A	This document contains information on the cooling of modern airborne electronics, emphasizing the use of a heat exchange surface which separates coolant and component. It supplements the information contained in...
AIRCRAFT NOSE WHEEL STEERING/CENTERING SYSTEMS -- AIR1752	This document covers both military aircraft (land-based and ship-based) and commercial aircraft. It is intended that the document be continually updated as new aircraft and/or new "lessons learned" become available.
AIRCRAFT ANTICOLLISION LIGHT SYSTEMS USING FLASHTUBES -- AIR1276	This document covers red and white aircraft anti-collision lights using flashtubes as the light source.
AIRCRAFT FLASHTUBE ANTICOLLISION LIGHTING SYSTEMS -- AIR1276A Aircraft Flashtube Anticollision Lighting Systems -- AIR1276B	This document covers red and white anticollision lights using flashtubes as the light source.
Uncertainty of In-Flight Thrust Determination -- AIR1678A Uncertainty of In-Flight Thrust Determination -- AIR1678B	This document defines and illustrates the process for determination of uncertainty of turbofan and turbojet engine in-flight thrust and other measured in-flight performance parameters. The reasons for requiring this information,...
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL SYSTEMS -- AIR1616 Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems -- AIR1616A	This document defines design, performance, and test criteria for self-sealing breakaway valves.
Aircraft Engine and Accessory Drives and Flange Standards -- AIR1160C	This document defines features that require interface definitions between aircraft engines and accessory drives and flanges and summarizes various aerospace standard dimensional performance data.
The Advanced Environmental Control System (AECS) Computer Program for Steady State Analysis and Preliminary System Sizing -- AIR1706C	This document has been declared "CANCELLED" as of January 2010. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index.
Plain Bearing Selection for Landing Gear Applications -- AIR1594B Plain Bearing Selection for Landing Gear Applications -- AIR1594C Plain Bearing Selection for Landing Gear Applications -- AIR1594D	This document is intended to give advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications. Information included herein was derived from...
PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS -- AIR1594 Plain Bearing Selection for Landing Gear Applications -- AIR1594A	This document is intended to give advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications. Information is given on bearing installation...
Oxygen System Maintenance Guide -- AIR1392A	This document is intended to give general instructions and directions for personnel performing maintenance and modification work on Oxygen Systems.
AIRCRAFT FIRE PROTECTION FOR HELICOPTER GAS TURBINE POWERPLANT AND RELATED SYSTEMS INSTALLATIONS -- AIR1262	This document is reissued for application to helicopters. It is primarily intended to apply to the engine or engines, but it shall also apply to fire protection of lines, tanks,...
AIRCRAFT FIRE PROTECTION FOR RECIPROCATING AND GAS TURBINE ENGINE INSTALLATIONS -- AIR1076	This document is reissued for application to helicopters.
MANUFACTURERS' IDENTIFICATION OF AEROSPACE ELECTRICAL AND ELECTRONIC WIRING DEVICES AND ACCESSORIES -- AIR1351C	This document lists the symbols used by manufacturers of electrical and electronic wiring devices and accessories to identify their products that are within the scope of SAE Subcommittees AE-8C1 and...
DESIGNING FOR LONG LIFE WITH ELASTOMERS -- AIR1412 DESIGNING FOR LONG LIFE WITH ELASTOMERS -- AIR1412A Designing for Long Life With Elastomers -- AIR1412B Designing for Long Life with Elastomers -- AIR1412C Designing for Long Life with Elastomers -- AIR1412D Designing for Long Life with Elastomers -- AIR1412E	This document lists those guidelines recognized as being essential for consideration by the designer who is preparing to select an elastomer as part of an aerospace design.
Airline Tow Tractor - Baggage/Cargo Factors for Design Consideration -- AIR1316A Airline Tow Tractor - Baggage/Cargo Factors for Design Consideration -- AIR1316B	This document outlines the functional and design requirements for baggage/cargo tow tractors used for airline services.
Glossary of Technical and Physiological Terms Related to Aerospace Oxygen Systems -- AIR171E	This document presents a glossary of many of the terms that can be found in literature covering issues related to aviation oxygen systems and associated topics. Such a listing can...
Glossary of Technical and Physiological Terms Related to Aerospace Oxygen Systems -- AIR171F	This document presents a glossary of many terms found in literature related to aviation oxygen systems and associated topics. Such a listing can never be all inclusive, but the majority...
AUXILIARY POWER SYSTEM CONSIDERATIONS FOR ADVANCED MILITARY AIRCRAFT -- AIR1603	This document provides a brief description of the auxiliary power equipment that is available with enough description and pertinent comments to enable an engineer to make logical preliminary selection of...
Thesaurus for Fuel System Components -- AIR1615A Thesaurus for Fuel System Components -- AIR1615B	This document provides a summary of names commonly used throughout the industry for aircraft fuel system components. It is a thesaurus intended to aid those not familiar with the lexicon...
Oxygen Cylinder Quality, Serviceability, Maintenance Transfilling and Marking -- AIR1059C Oxygen Cylinder Quality, Serviceability, Maintenance Transfilling and Marking -- AIR1059D Oxygen Cylinder Quality, Serviceability, Maintenance Transfilling and Marking -- AIR1059E	This document provides guidance concerning the maintenance and serviceability of oxygen cylinders beginning with the quality of oxygen that is required, supplemental oxygen information, handling and cleaning procedures, transfilling and...
Oxygen Cylinder Quality, Serviceability, Maintenance Transfilling, and Marking -- AIR1059F	This document provides guidance concerning the maintenance and serviceability of oxygen cylinders beginning with the quality of oxygen that is required, supplemental oxygen information, handling and cleaning procedures, transfilling, and...
Liquid Propellant Gas Generation Systems -- AIR1343A Liquid Propellant Gas Generation Systems -- AIR1343B	This information report presents a preliminary discussion of liquid propellant gas generation (LPGG) systems. A LPGG system, as used herein, is defined as a system which stores a liquid propellant...
Transparent Area Washing Systems for Aircraft -- AIR1102A Transparent Area Washing Systems for Aircraft -- AIR1102B	This information report presents data and recommendations pertaining to the design and development of transparent area washing systems for aircraft.
FLEXURE FATIGUE STRENGTH OF TUBE FITTING JOINTS -- AIR1418	This information report presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S vs. number of cycles...
Limits and Fits - International Metric Tolerance System -- AIR1758	This information report provides guidance when the ISO International metric tolerance system for limits and fits per ISO/R286 or ANSI B4.2-1978 is applied on a standard, and also provides a...
Spacecraft Equipment Environmental Control -- AIR1168/13 Spacecraft Equipment Environmental Control -- AIR1168/13A	This part of the manual presents methods for arriving at a solution to the problem of spacecraft inflight equipment environmental control. The temperature aspect of this problem may be defined...
TIN PLATED SOLDERLESS TERMINAL LUGS AND SPLICES ON NICKEL COATED HIGH TEMPERATURE WIRE -- AIR1263 Tin Plated Solderless Terminal Lugs and Splices on Nickel Coated High Temperature Wire -- AIR1263A	This publication formally cautions against terminating nickel coated wire with tin plated insulated or uninsulated crimped solderless terminations.
MANUFACTURERS' IDENTIFICATION OF AEROSPACE ELECTRICAL AND ELECTRONIC WIRING DEVICES AND ACCESSORIES -- AIR1351B	This publication lists the symbols used by manufacturers of electrical and electronic wiring devices and accessories to identify their products that are within the scope of SAE Subcommittees AE-8C1 and...
MANUFACTURERS' IDENTIFICATION OF ELECTRICAL CONNECTOR CONTACTS, TERMINALS & SPLICES -- AIR1351A	This publication serves to define, through pictorial representation, those identification symbols, which are in current use by manufacturers of contacts for use in electrical connectors as well as terminals and...
ENVIRONMENTAL CONTROL SYSTEM CONTAMINATION -- AIR1539 Environmental Control System Contamination -- AIR1539A Environmental Control System Contamination -- AIR1539B	This publication will be limited to a discussion of liquid and particulate contaminants which enter the aircraft through the environmental control system (ECS). Gaseous contaminants such as ozone, fuel vapors,...
CONTROL OF WATER CARRYOVER FROM THE ENVIRONMENTAL CONTROL SYSTEM AND CONDENSATION ON THE STRUCTURE -- AIR1204	This publication will discuss water carryover from the environmental control system with respect to causes and indicated corrective or preventative action. In addition, condensation on structure will be reviewed with...
AIRCRAFT HUMIDIFICATION -- AIR1609	This report covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated...
HIGH VOLTAGE PULSE GENERATOR -- AIR1091	This report covers the use, electro-mechanical description, and accuracy of a pulse generator in the range of 5 to 30 kilovolts and zero to peak voltage time of less than...
RECOMMENDATIONS FOR SELECTION AND USE OF TORQUE WRENCHES FOR AEROSPACE PROPULSION SYSTEMS APPLICATIONS -- AIR1268	This report covers torque indicating and limiting devices, also referred to as torque wrenches or torque handles, accessories used to obtain predetermined torque values on nuts, bolts, plumbing, related fasteners...
COMMON TERMINATION METHOD, ELECTRICAL WIRING SYSTEM, APPLICATION OF -- AIR1402 Common Termination Method, Electrical Wiring System, Application Of -- AIR1402A	This report defines the guidelines for a COMMON TERMINATION METHOD for aerospace vehicle electrical wiring systems and shows how designers can select a minimum number of different parts, among preferred...
AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY -- AIR1489A Aerospace Landing Gear Systems Terminology -- AIR1489B Aerospace Landing Gear Systems Terminology -- AIR1489C	This report has been compiled by the Landing Gear Systems Terminology panel of SAE Committee A-5 (Aerospace Landing Gear Systems). It represents an effort to gather together those terms commonly...
IGNITION EXCITER OUTPUT VOLTAGE PULSE MEASUREMENT USING A PRESSURIZED BALL GAP -- AIR1090	This report includes a procedure for typical pulse voltage measurement using the pressurized ball gap, calibration procedure, and a description of the pressurized ball gap.
CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES -- AIR1184A	This report is intended to identify the necessary analytical tools to enable making value judgments for minimizing the various errors typically encountered in capacitance systems. Thus, in addition to identification...
Capacitive Fuel Gauging System Accuracies -- AIR1184B	This report is intended to identify the various errors typically encountered in capacitance fuel quantity measurement systems. In addition to identification of error sources, it describes the basic factors which...
Aerospace Fuel System Specifications and Standards -- AIR1408B	This report lists documents that aid and govern the design of aircraft and missile fuel systems. The report lists the military and industry specifications and standards and the most notable...
Aerospace Fuel System Specifications and Standards -- AIR1408A	This report lists documents that aid and govern the design of gas turbine powered aircraft and missile fuel systems. The report lists the military and industry specifications and standards and...
AEROSPACE FUEL SYSTEM SPECIFICATIONS AND STANDARDS -- AIR1408	This report lists military and industry specifications and standards which are commonly used in aerospace gas turbine fuel systems. It is intended as a supplement to specifications MIL-F-3863, MIL-F-17874 and...
Index of Starting System Specifications and Standards -- AIR1174B	This report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Listings are provided as follows: Section 2 . Topic Listing...
INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS -- AIR1174A	This report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Only those hardware standards which have been specifically designed for...
INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS -- AIR1174	This report lists military and industry specifications and standards which are used in aerospace engine starting systems. Only those hardware standards which have been specifically designed for engine starting systems...
PHYSICAL PROPERTIES OF HYDRAULIC FLUIDS -- AIR1362	This report presents data on hydraulic fluids which are of interest to detail designers of hydraulic systems and components for military flight vehicles. The data pertain to fluids conforming to...
Clamp Material, Injection Molded -- AIR1397A Clamp Material, Injection Molded -- AIR1397B	This report presents the material properties and test requirements for an injection molded thermoplastic compound utilized for fabrication of AS1396 clamp block assembly.
Regulatory Requirements Covering the Use of Breathing Oxygen in Aircraft -- AIR1389A	This report presents, paraphrased in tabular format, an overview of the Federal Aviation Regulations (FAR) and the Joint Aviation Regulations (JAR) for aircraft oxygen systems. It is intended as a...
FAR - Regulatory Requirements Covering the Use of Breathing Oxygen in Aircraft -- AIR1389B FAR - Regulatory Requirements Covering the Use of Breathing Oxygen in Aircraft -- AIR1389C	This report presents, paraphrased in tabular format, an overview of the Federal Aviation Regulations (FAR) for aircraft oxygen systems. It is intended as a ready reference for those considering the...
AGE CONTROL OF AGE SENSITIVE ELASTOMERIC MATERIALS -- AIR1364	This report summarizes data and background relative to age control of specific classes of those nitrile type synthetic elastomers used in sealing devices which are resistant to petroleum base hydraulic...
FLUID PROPERTIES -- AIR1116 Fluid Properties -- AIR1116A Fluid Properties -- AIR1116B Fluid Properties -- AIR1116C	This report summarizes data relative to liquid fluids and their properties which are of interest to Aerospace Fluid Power technologists.
HYDRAULIC SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT -- AIR1083A	This report supplies data on various survivability design approaches and techniques to provide a broad frame of reference for future fluid power designers. Before the designer embarks on the overall...
Inlet Total-Pressure Distortion Considerations for Gas-Turbine Engines -- AIR1419D	This SAE Aerospace Information Report (AIR) addresses many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability. It provides a review of the...
VEHICLE ELECTRICAL SYSTEMS -- AIR1336A	This SAE Aerospace Information Report (AIR) considers the following major areas: 1 Major components and their ratings 2 Selection criteria for optimum design balance for electrical systems 3 Effects of...
Ground Support Equipment Electrical Systems -- AIR1336B Ground Support Equipment Electrical Systems -- AIR1336C	This SAE Aerospace Information Report (AIR) considers the following major areas: 1 major components and their ratings; 2 selection criteria for optimum design balance for electrical systems; 3 effects of...
Cooling of Military Avionic Equipment -- AIR1277B	This SAE Aerospace Information Report (AIR) contains information on the thermal design requirements of airborne avionic systems used in military airborne applications. Methods are explored which are commonly used to...
Clamp Loads and Bending Stresses in Aircraft Tubing Installations -- AIR1593A	This SAE Aerospace Information Report (AIR) contains information relative to stresses and loads developed in tubes caused by tube deflections encountered in misaligned installations. Users are advised that when calculating...
Aircraft Humidification -- AIR1609A Aircraft Humidification -- AIR1609B	This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin...
Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351D Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351E Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351F Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351G Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351H	This SAE Aerospace Information Report (AIR) covers the general requirements for and the listing of manufacturers identification that appear on electrical/electroni c wiring devices and accessories as required by individual...
Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351J Manufacturers' Identification of Aerospace Electrical and Electronic Wiring Devices and Accessories -- AIR1351K	This SAE Aerospace Information Report (AIR) covers the general requirements for, and the listing of, manufacturers' identification markings, names, symbols or trademarks, and CAGE codes that appear on electrical and...
Electrical Connectors and Wiring, Compatibility of -- AIR1329C	This SAE Aerospace Information Report (AIR) defines the areas where incompatibility may exist between the selected wire and the electrical connector in which it is terminated and how to design...
Identification and Coding of Fluid and Electrical Piping System Functions -- AIR1273B	This SAE Aerospace Information Report (AIR) establishes a positive identification of the functions and, if applicable, the hazards and direction of flow of pipe, hose, tube, or electrical conduit lines.
Standard Impulse Machine Equipment and Operation -- AIR1228	This SAE Aerospace Information Report (AIR) establishes the part numbers and/or description of the critical components and operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies,...
Standard Impulse Machine Equipment and Operation -- AIR1228A	This SAE Aerospace Information Report (AIR) establishes the specifications and descriptions of the critical components and operational guidelines for the standard hydraulic impulse machine for testing hydraulic hose assemblies, tubing,...
Information on Antiskid Systems -- AIR1739A Information on Antiskid Systems -- AIR1739B	This SAE Aerospace Information Report (AIR) has been prepared by a panel of the SAE A-5A Committee and is presented to document the design approaches and service experience from various...
Rotor Blade Electrothermal Ice Protection Design Considerations -- AIR1667A	This SAE Aerospace Information Report (AIR) identifies and summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection systems. Although...
Environmental Control System Contamination -- AIR1539C	This SAE Aerospace Information Report (AIR) includes a discussion of liquid and particulate contaminants which enter the aircraft through the environmental control system (ECS). Gaseous contaminants such as ozone, fuel...
Aircraft Flexible Tanks General Design and Installation Recommendations -- AIR1664A	This SAE Aerospace Information Report (AIR) includes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure...
Methods of Achieving Electromagnetic Compatibility of Gas Turbine Engine Accessories, for Self-Propelled Vehicles -- AIR1425A Methods of Achieving Electromagnetic Compatibility of Gas Turbine Engine Accessories, for Self-Propelled Vehicles -- AIR1425B	This SAE Aerospace Information Report (AIR) is a description of methods to be employed to achieve Electromagnetic Compatibility (EMC) of gas turbine engine accessories. Its primary objectives are to aid...
Hose Assembly Identification Practices -- AIR1698A Hose Assembly Identification Practices -- AIR1698B	This SAE Aerospace Information Report (AIR) is applicable to hose assemblies for which identification marking is not otherwise specified in procurement or performance standard or drawing.
BAROMETRY FOR ALTIMETER CALIBRATION -- AIR1075A Barometry for Altimeter Calibration -- AIR1075B	This SAE Aerospace Information Report (AIR) is concerned only with aspects directly relating to available accuracy. While well-designed photoelectric, inductive or capacitive readers and pressure regulators, and other accessories are...
Service Damage Limits for Aircraft Hydraulic Tubing -- AIR1388B	This SAE Aerospace Information Report (AIR) is intended to assist in evaluating the serviceability of damaged hydraulic tubing lines. The performance requirements are outlined to which the defect samples were...
EVALUATION OF HELICOPTER TURBINE ENGINE LINEAR VIBRATION ENVIRONMENT -- AIR1289A	This SAE Aerospace Information Report (AIR) outlines a recommended procedure for evaluation of the vibration environment to which the gas turbine engine powerplant is subjected in the helicopter installation. This...
Fault Isolation in Environmental Control Systems of Commercial Transports -- AIR1266A Fault Isolation in Environmental Control Systems of Commercial Transports -- AIR1266B	This SAE Aerospace Information Report (AIR) outlines concepts for the design and use of fault isolation equipment that have general application. The specific focus is on fault isolation of environmental...
Aircraft Accessory Drag Torque During Engine Starts -- AIR1087B	This SAE Aerospace Information Report (AIR) presents a discussion of drag torques of engine accessories operating at cold temperature. Various conditions of temperature, speed, and acceleration rates are reviewed showing...
Power Sources for Fluidic Controls -- AIR1245A Power Sources for Fluidic Controls -- AIR1245B	This SAE Aerospace Information Report (AIR) presents a review of the types and general characteristics of power sources that may be used to provide the power for gaseous or liquid...
Aerospace Hydraulic Fluids Physical Properties -- AIR1362A Aerospace Hydraulic Fluids Physical Properties -- AIR1362B	This SAE Aerospace Information Report (AIR) presents data on hydraulic fluids which are of interest to detail designers of hydraulic systems and components for aerospace flight vehicles. The data pertain...
Aerospace Hydraulic Fluids Physical Properties -- AIR1362C Aerospace Hydraulic Fluids Physical Properties -- AIR1362D	This SAE Aerospace Information Report (AIR) presents data on hydraulic fluids which are of interest to detail designers of hydraulic systems and components for aerospace flight vehicles. The data pertains...
Flexure Fatigue Strength of Tube Fitting Joints -- AIR1418A Flexure Fatigue Strength of Tube Fitting Joints -- AIR1418B	This SAE Aerospace Information Report (AIR) presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S versus...
Gas Energy Limited Starting Systems -- AIR1467B	This SAE Aerospace Information Report (AIR) presents information on gas energy limited propulsion engine starting systems employed in commercial and military applications and remote industrial sites. The types of systems...
Safety Criteria for Pneumatic Starting Systems -- AIR1639A	This SAE Aerospace Information Report (AIR) presents safety criteria for pneumatic type engine starting system design and component hardware. Included are safety criteria in design of both starter control valves...
Minimization of Electrostatic Hazards in Aircraft Fuel Systems -- AIR1662A	This SAE Aerospace Information Report (AIR) provides background information, technical data and related technical references for minimization of electrostatic hazards in aircraft fuel systems. Techniques used to minimize the electrostatic...
Minimization of Electrostatic Hazards in Aircraft Fuel Systems -- AIR1662B	This SAE Aerospace Information Report (AIR) provides background information, technical data, and related technical references for minimization of electrostatic hazards in aircraft fuel systems.
Aerospace, Slipper Seals, Selection for Fluid Power Applications -- AIR1244B	This SAE Aerospace Information Report (AIR) provides basic information on the use of slipper seal sealing devices when used as piston (OD) and rod (ID) seals in aerospace fluid power...
Handbook of Hydraulic Metric Calculations -- AIR1657C	This SAE Aerospace Information Report (AIR) provides details of how to perform hydraulic system calculations using equations that incorporate the metric International System of Units (SI).
Anti Blow-By Design Practice for Cap Seals -- AIR1243B Anti Blow-By Design Practice for Cap Seals -- AIR1243C Anti Blow-By Design Practice for Cap Seals -- AIR1243D	This SAE Aerospace Information Report (AIR) provides information on anti blow-by design practice for cap seals. Suggestions for piston cap seal sidewall notch design and other anti blow-by design details...
Molded Rigid Plastic Parts -- AIR1269B Molded Rigid Plastic Parts -- AIR1269C	This SAE Aerospace Information Report (AIR) provides recommendations for the best practices to be followed in the molding of rigid thermoplastic and thermosetting molding compounds. The molding processes covered in...
Airborne Hydraulic and Control System Survivability for Military Aircraft -- AIR1083C	This SAE Aerospace Information Report (AIR) provides the hydraulic and flight-control system designer with the various design options and techniques that are currently available to enhance the survivability of military...
AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT -- AIR1083B	This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge...
Performance Testing of Lubricant Filter Elements Utilized in Aircraft Power and Propulsion Lubrication Systems -- AIR1666C	This SAE Aerospace Information Report (AIR) reviews performance testing parameters for non-cleanable (often referred to as disposable) filter elements utilized in aircraft power and propulsion lubrication systems, including gas turbine...
Performance Testing of Lubricant Filter Elements Utilized in Aircraft Power and Propulsion Lubrication Systems -- AIR1666A Performance Testing of Lubricant Filter Elements Utilized in Aircraft Power and Propulsion Lubrication Systems -- AIR1666B	This SAE Aerospace Information Report (AIR) reviews performance testing parameters for non-cleanable, often referred to as disposable, filter elements utilized in aircraft power and propulsion lubrication systems, including gas turbine...
PERFORMANCE TESTING OF GAS TURBINE LUBE OIL FILTER ELEMENTS -- AIR1666	This SAE Aerospace Information Report (AIR) reviews performance testing parameters for noncleanable, often referred to as disposable, aircraft gas turbine engine lubricant filter elements.
Age Control of Age Sensitive Elastomeric Materials -- AIR1364A Age Control of Age Sensitive Elastomeric Materials -- AIR1364B Age Control of Age Sensitive Elastomeric Materials -- AIR1364C	This SAE Aerospace Information Report (AIR) summarizes data and background relative to age control of specific classes of those nitrile type synthetic elastomers used in sealing devices which are resistant...
Materials for Fluid Systems Components and Their International Equivalents -- AIR1564A	This SAE Aerospace Information Report (AIR) summarizes the materials referenced in specifications for components used in USA fluid systems and, where available, the equivalent materials of France, Germany, United Kingdom,...
Identification and Coding of Fluid and Electrical Piping System Functions -- AIR1273A	This SAE Aerospace Information Report establishes a positive identification of the functions and, if applicable, the hazards and direction of flow of pipe, hose, tube, or electrical conduit lines.
STARTER SYSTEM OPTIMIZATION START ANALYSIS, TURBINE ENGINE - ELECTRIC, BATTERY POWER -- AIR1602	This SAE Aerospace Information Report includes procedures for the analysis of a gas turbine engine start. It utilizes a standard form for the essential starting characteristics of the gas turbine...
Cross Reference for Materials for Fluid Systems Components Including Military and Federal Specifications and Their International Equivalents -- AIR1564B Cross Reference for Materials for Fluid Systems Components, Including Military and Federal Specifications and Their International Equivalents -- AIR1564C	This SAE Aerospace Report (AIR) provides a cross reference for SAE material standards to other similar standards. The SAE Committee G-3 invites comments and recommendations for the addition of materials...
Aerothermodynamic Systems Engineering and Design -- AIR1168/3 SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design -- AIR1168/3A	This section presents methods and examples of computing the steady-state heating and cooling loads of aircraft compartments. In a steady-state process the flows of heat throughout the system are stabilized...
Ice, Rain, Fog, and Frost Protection -- AIR1168/4 SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection -- AIR1168/4A SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection -- AIR1168/4B SAE Aerospace Applied Thermodynamics Manual Ice, Rain, Fog, and Frost Protection -- AIR1168/4C	This section presents the basic equations for computing ice protection requirements for nontransparent and transparent surfaces and for fog and frost protection of windshields. Simplified graphical presentations suitable for preliminary...
Aircraft Fuel Weight Penalty Due to Air Conditioning -- AIR1168/6A Characteristics of Equipment Components, Equipment Cooling System Design, and Temperature Control System Design -- AIR1168/6	This section relates the engineering fundamentals and thermophysical property material of the previous sections to the airborne equipment for which thermodynamic considerations apply. For each generic classification of equipment, information...
ENVIRONMENTAL CRITERIA AND TESTS FOR AEROSPACE GROUND EQUIPMENT IN SUPPORT OF SPACE SYSTEMS -- AIR1167	This specification establishes environmental criteria for designing Aerospace Ground Equipment (AGE) in support of space systems. The test levels in this specification have been elevated to compensate for absence of...
RECOMMENDED PART NUMBERING GUIDELINES FOR FLUID SYSTEM COMPONENTS INCH SYSTEM OF MEASUREMENTS -- AIR1590	THIS STANDARD CONSIDERS THE PART NUMBERING SYSTEM FOR HOSE ASSEMBLIES, FITTINGS, AND CLAMPS. OTHER COMPONENT TYPES COULD BE ADDED LATER.
Ramp De-Icing -- AIR1335B	This Technical Report has been declared "CANCELLED" as of June 2018 and has been superseded by AS6285, AS6286, and AS6332. By this action, this document will remain listed in the...
Flight Compartment Glare -- AIR1151A	To bring to the attention of the aircraft designer and user the problems that can result from the fight crew experiencing glare. To improve visibility conditions for the flight crew...
Designing with Elastomers for Use at Low Temperatures, Near or Below Glass Transition -- AIR1387C Designing with Elastomers for use at Low Temperatures, Near or Below Glass Transition -- AIR1387D	To ensure success in design of elastomeric parts for use at low temperature, the design engineer must understand the peculiar properties of rubber materials at these temperatures. There are no...
TORQUE TIGHTENING THREADED FASTENERS -- AIR1471	To supply information on recommended assembly torque limits for tension type nuts and bolts of the following materials and plating combinations given in Table I .
A Primer of Aircraft Multiplexing -- AIR1207	Today's sophisticated aircraft are required to effectively perform a variety of missions. With the advent of micro-miniaturizatio n in electronics and advanced digital computers, a new generation of avionics equipment...
Verification of Landing Gear Design Strength -- AIR1494A Verification of Landing Gear Design Strength -- AIR1494B	Verification of landing gear design strength is accomplished by dynamic and static test programs. This is essentially a verification of the analytical procedures used to design the gear. An industry...

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