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SAE - SAE ARP6852 - METHODS AND PROCESSES FOR EVALUATION OF AERODYNAMIC EFFECTS OF SAE-QUALIFIED AIRCRAFT GROUND DEICING/ANTI-ICING FLUIDS Organization: SAE
Date: 2017-01-01
Description: Guidance and insight based upon those experiences are provided, including Similarity analyses Icing wind tunnel tests Flight tests Computational fluid dynamics and other numerical analyses This document also describes The history of evaluation of the aerodynamic effects of fluids The effects of fluids on aircraft aerodynamics The testing for aerodynamic acceptability of fluids for SAE and regulatory qualification performed in accordance with AS5900 Additionally, Appendices A to E present individual aircraft manufacturers’ histories and methodologies which substantially contributed to the improvement of knowledge and processes for the evaluation of fluid aerodynamic effects NOTE: This document is applicable for fluids that are “qualified” to (i.e., have passed) the tests and other standards prescribed in AMS1424 or AMS1428 and are properly used in accordance with ARP4737 NOTE: There are topics of potential interest not discussed in this document, such as re-hydrated gel residues (see 2.2) CAUTION: The results and conclusions of the various test programs described herein should not be assumed to be universally applicable CAUTION: All methodologies presented in this ARP were created or developed considering solely glycol-based fluids
SAE - SAE AHB-001 - SAE AIRCRAFT MAINTENANCE CHEMICALS AND MATERIALS AMS HANDBOOK Organization: SAE
SAE - SAE ARP6207 - QUALIFICATIONS REQUIRED FOR SAE TYPE I AIRCRAFT DEICING/ANTI-ICING FLUIDS Organization: SAE
Date: 2017-10-01
Description: This document describes: a. the preparatory steps to test experimental Type I fluids according to AMS1424; b. the recommendations for the preparation of samples for endurance time testing according to ARP5945; c. a short description of the recommended field spray test; d. the protocol to demonstrate that Type I fluid can be used with the Type I holdover time guidelines published by the FAA and Transport Canada, including endurance time data obtained from ARP5945; e. the protocol for inclusion of Type I fluids on the FAA and Transport Canada lists of fluids; f. the protocol for updating the FAA and Transport Canada lists of fluids; g. the role of the SAE G-12 Aircraft Deicing Fluids Committee; h. the role of the SAE G-12 Holdover Time Committee; and i. the process for the publication of Type I holdover time guidelines.
SAE - SAE ARP5945 - (R) ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE I AIRCRAFT DEICING/ANTI-ICING FLUIDS Organization: SAE
Date: 2017-10-01
Description: Examination of Endurance Time Data Periodically, the SAE G-12 Holdover Time Subcommittee examines endurance time test data of SAE Type I aircraft deicing/anti-icing fluids and validates, based on the endurance time data, if such fluids can be used in conjunction with generic Type I HOT guidelines.
SAE - SAE AMS1424 - FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1 Organization: SAE
Date: 2017-06-01
Description: Application The fluid is generally used heated either diluted with water, or as supplied, for the removal of deposits of frost, ice, and snow on exterior aircraft surfaces prior to take off. Consult aircraft manufacturer's maintenance manual and service letters to determine any restrictions relating to the use of deicing/anti-icing fluids for type and model of aircraft being treated.
SAE - SAE ARP5718 - QUALIFICATIONS REQUIRED FOR SAE TYPE II/III/IV AIRCRAFT DEICING/ANTI-ICING FLUID Organization: SAE
Date: 2017-12-01
Description: This document describes: a. the preparatory steps to test experimental Type II, III, and IV fluids according to AMS1428; b. the recommendations for the preparation of samples for endurance time testing according to ARP5485; c. a short description of wind tunnel testing; d. a short description of the recommended field spray test; e. the protocol to generate draft holdover time guidelines from endurance time data obtained from ARP5485; f. the protocol for inclusion of Type II, III, and IV fluids on the FAA and Transport Canada lists of fluids and the protocol for updating the lists of fluids; g. the role of the SAE G-12 Aircraft Deicing Fluids Committee; h. the role of the SAE G-12 Holdover Time Committee; and i. the process for the publication of Type II, III, and IV holdover time guidelines.
SAE - SAE ARP5485 - (R) ENDURANCE TIME TEST PROCEDURES FOR SAE TYPE II/III/IV AIRCRAFT DEICING/ANTI-ICING FLUIDS Organization: SAE
Date: 2017-10-01
Description: Purpose The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the sample selection and endurance time test procedures, for SAE Type II, III, and IV aircraft deicing/anti-icing fluids, required for the generation of endurance time data of acceptable quality for review by the SAE G-12 Holdover Time Subcommittee.
SAE - SAE AIR5354 - HISTORY OF THE SAE A-10 AIRCRAFT OXYGEN EQUIPMENT COMMITTEE Organization: SAE
Date: 2016-08-01
Description: The following is the history of SAE Committee A-10.
SAE - SAE AMS1428 - FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN (PSEUDOPLASTIC), SAE TYPES II, III, AND IV Organization: SAE
Date: 2017-03-01
Description: Consult ARP4737 for more information on the proper use or restrictions of SAE Type II, III, and IV aircraft deicing/anti-icing fluids. Precautions The lowest operational use temperature (LOUT) for a SAE Type II, III, and IV fluid shall be determined for the neat (undiluted) fluid or for each intended use dilution, and is the lowest temperature at which the fluid has been tested and certified as acceptable in accordance with the appropriate aerodynamic acceptance test (3.2.5) while still maintaining the 7 °C (13 °F) freezing point temperature buffer (see ARP4737).
SAE - SAE AS5901 - (R) WATER SPRAY AND HIGH HUMIDITY ENDURANCE TEST METHODS FOR SAE AMS1424 AND SAE AMS1428 AIRCRAFT DEICING/ANTI-ICING FLUIDS Organization: SAE
Date: 2014-06-01
Description: Minimum Requirements This document establishes the minimum requirements for an environmental test chamber, and test procedures to carry out anti-icing performance tests according to the current materials specification for aircraft deicing/anti-icing fluids. The primary purpose for such a test method is to determine the anti-icing endurance under controlled laboratory conditions of AMS1424 Type I and AMS1428 Type II, III, and IV fluids.
SAE - SAE AMS1428/1 - FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN (PSEUDOPLASTIC), SAE TYPES II, III, AND IV GLYCOL (CONVENTIONAL AND NON-CONVENTIONAL) BASED Organization: SAE
Date: 2017-02-01
Description: Foundation and Category Specifications The foundation specification establishes the requirements for all fluid, aircraft deicing/anti-icing, non-Newtonian (pseudoplastic), SAE Types II, III, and IV, and defines the terms Glycol (conventional and non-conventional) and Non- Glycol, and contains technical and other requirements that apply to both Glycol (conventional and non-conventional) and non-Glycol based fluids.
SAE - SAE AMS1428/2 - FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN (PSEUDOPLASTIC), SAE TYPES II, III, AND IV NON-GLYCOL BASED Organization: SAE
Date: 2017-02-01
Description: Foundation and Category Specifications The foundation specification establishes the requirements for all Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV and defines the terms Glycol (Conventional and Non-Conventional) and Non- Glycol and contains technical and other requirements that apply to both Glycol (Conventional and Non-Conventional) and Non-Glycol based fluids.
SAE - SAE AMS6479 - STEEL, BARS, FORGINGS, AND TUBING 1.45CR (0.93-1.05C) (SAE 52100) SPECIAL AIRCRAFT-QUALITY CLEANLINESS - UNS G52986 Organization: SAE
Date: 2015-10-01
Description: Form This specification covers a special aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
SAE - SAE AMS6528 - STEEL, BARS 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) SPECIAL AIRCRAFT QUALITY CLEANLINESS NORMALIZED - UNS G41300 Organization: SAE
Date: 2017-08-01
Description: Form This specification covers a special aircraft-quality, low-alloy steel in the form of bars. Application These bars have been used typically for parts required to meet stringent magnetic inspection criteria, having sections 0.50 inch (12.7 mm) and under in nominal thickness at time of heat treatment, and requiring a through-hardening steel capable of developing hardness as high as 35 HRC when properly hardened and tempered, and also for parts of greater thickness, but requiring proportionately lower hardness.
SAE - SAE AMS1424/1 - DEICING/ANTI-ICING FLUID, AIRCRAFT SAE TYPE I GLYCOL (CONVENTIONAL AND NON-CONVENTIONAL) BASED Organization: SAE
Date: 2016-04-01
Description: Form The foundation specification (AMS1424M) and the detail specificat...
SAE - SAE AMS1424/2 - DEICING/ANTI-ICING FLUID, AIRCRAFT SAE TYPE I NON-GLYCOL BASED Organization: SAE
Date: 2016-05-01
Description: Form The foundation specification (AMS1424M) and the detail specificat...
SAE - SAE AMS6529 - STEEL, BARS 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) SPECIAL AIRCRAFT-QUALITY CLEANLINESS NORMALIZED - UNS G41400 Organization: SAE
Date: 2017-05-01
SAE - SAE AMS6444 - STEEL, BARS, FORGINGS, AND TUBING 1.45CR (0.93 - 1.05C) (SAE 52100) PREMIUM AIRCRAFT-QUALITY, CONSUMABLE ELECTRODE VACUUM REMELTED - UNS G52986 Organization: SAE
Date: 2015-08-01
Description: Form This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
SAE - SAE AMS6409 - STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) SPECIAL AIRCRAFT QUALITY CLEANLINESS NORMALIZED AND TEMPERED - UNS G43406 Organization: SAE
Date: 2016-12-01
Description: Form This specification covers a low-alloy steel in the form of bars, ...
SAE - SAE AMS-T-9047 - TITANIUM AND TITANIUM ALLOY, BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY; S/S BY SAE AMS4921, AMS6900, AMS6901, AMS6910, AMS6940, AMS6931, AMS6930, AMS6932, AMS6936, AMS6935, AMS6905, AMS6907, AMS6906, AMS6915,AMS6920,AMSD6921,AMS6926 Organization: SAE
Date: 2006-05-01
Description: This specification covers aircraft quality, commercially pure titanium and alpha, alpha-beta and beta titanium alloy rolled or forged bar and reforging stock products. S/S by: SAE AMS4921, AMS6900, AMS6901, AMS6910, AMS6940, AMS6931, AMS6930, AMS6932, AMS6936, AMS6935, AMS6905, AMS6907, AMS6906, AMS6915,AMS6920,AMSD6921,AMS6926

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