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API/EI 1585 - GUIDANCE IN THE CLEANING OF AVIATION FUEL HYDRANT SYSTEMS AT AIRPORTS - SECOND EDITION; NOW COPYRIGHTED BY EI Organization: API
Date: 2007-11-01
Description: Operational practices to maintain the system in a clean condition. The design of hydrant systems to aid cleaning. If the hydrant system is clean when placed in service and adequate filtration is given to the fuel entering it, the hydrant should remain clean in service.
IP - EI 1585 - GUIDANCE IN THE CLEANING OF AVIATION FUEL HYDRANT SYSTEMS AT AIRPORTS Organization: IP
MODUK - DEF STAN 02-319 - REQUIREMENTS FOR AVIATION FUEL SYSTEMS IN HM SURFACE SHIPS - ISSUE 3: 12/2009 Organization: MODUK
Date: 2009-12-11
Description: a) This Defence Standard (Def Stan) specifies the requirements for Aviation Fuel Systems in HM Surface Ships from the deck filling connections to the aircraft.
MODUK - DEF STAN 68-278 - CLEANING PROCEDURES & STANDARDS FOR NAVAL OXYGEN SYSTEM COMPONENTS Organization: MODUK
Date: 2016-09-09
Description: It is applicable to both Liquid and Gaseous Oxygen systems. This Standard does not apply to systems and components intended for aviation use; it does not provide guidance on material selection or design requirements for oxygen components/parts.
NPFC - MIL-PRF-29602 - CLEANING COMPOUNDS, PARTS WASHER AND SPRAY CABINET Organization: NPFC
Date: 2005-01-31
Description: The cleaning compound is intended for use in parts washers and spray cabinets for cleaning aviation weapons systems, and engine and support equipment components. The cleaning compound will remove oily contaminants which are present on disassembled components.
SAE/TP - 2006-01-2436 - QUIET, CLEAN, AND EFFICIENT, BUT HEAVY – CONCERNS FOR FUTURE FUEL CELL POWERED PERSONAL AIR VEHICLES Organization: SAE/TP
Date: 2006-08-29
Description: Author(s): Name: Eric Upton and Dimitri Mavris; Affiliation: Georgia Institute of Technology Meeting Details: Name: General Aviation Technology Conference and Exhibition Location: Wichita, Kansas Date: 08-29-2006 
API/EI 1550 - HANDBOOK ON EQUIPMENT USED FOR THE MAINTENANCE AND DELIVERY OF CLEAN AVIATION FUEL - FIRST EDITION; NOW COPYRIGHTED BY EI * TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: API
Date: 2007-10-01
Description: This publication provides information for: • Designers of aviation fuel handling systems (including aviation filter systems and other fuel cleanliness monitoring/control equipment).
ARMY - UFGS-33 08 53 - AVIATION FUEL DISTRIBUTION SYSTEM START-UP Organization: ARMY
Date: 2010-02-01
Description: NOTE: This guide specification covers the requirements for the flushing, cleaning and performance testing of new aircraft refueling systems constructed to the requirements of the DoD Type III/IV/V, and Cut'n Cover Hydrant Refueling System Standards.
NPFC - MIL-PRF-32348 - POWDER COATING, CAMOUFLAGE CHEMICAL AGENT RESISTANT SYSTEMS Organization: NPFC
Date: 2013-12-16
Description: Included are chemical agent resistant powder coatings for use as a finish coat and powder coatings meant for use as primers with chemical agent resistant camouflage finish coats on all military tactical equipment, which includes ground, aviation and related support assets. The materials are free of volatile organic compounds (VOCs), volatile organic hazardous air pollutants (VOHAPs) and inorganic hazardous air pollutants (HAPs), other than cobalt and non-hexavalent chromium.
NAVY - MIL-F-24666 - FILTER ELEMENT, SHIP FUEL SYSTEM PRE-FILTER, NON-CLEANABLE, HIGH EFFICIENCY Organization: NAVY
Date: 1986-08-19
Description: This specification covers high efficiency filter elements for use in navy distillate fuel, F-76 conforming to MIL-F-16884 or turbine fuel, aviation grade, JP-5 conforming to MIL-T-5624 (see 6.1).
ASTM F2799 - STANDARD PRACTICE FOR MAINTENANCE OF AIRCRAFT ELECTRICAL WIRING SYSTEMS Organization: ASTM
Date: 2014-05-01
Description: Definition—This practice defines acceptable practices and processes for the maintenance, preventative maintenance, and repair of electric systems in general aviation aircraft. This practice does not change or create any additional regulatory requirements nor does it authorize changes in or permit deviations from existing regulatory requirements.
SAE/TP - 2008-01-2235 - CFD ANALYSIS OF THE TIGERFISH RETRACTABLE FLOAT SYSTEM ON A DHC- TWIN OTTER Organization: SAE/TP
Date: 2008-08-19
Description: A DHC Twin Otter equipped with a the Tigerfish Aviation Retractable Float Pack was found to have only 17% more drag than the clean aircraft, as compared to 45% more drag for a fixed float equipped DHC Twin Otter.
ASTM F2639 - STANDARD PRACTICE FOR DESIGN, ALTERATION, AND CERTIFICATION OF AIRCRAFT ELECTRICAL WIRING SYSTEMS Organization: ASTM
Date: 2015-08-01
Description: Definition—This practice defines acceptable practices and processes for the design, alteration, and certification of electric systems and installations in general aviation aircraft. This practice does not change or create any additional regulatory requirements nor does it authorize changes in or permit deviations from existing regulatory requirements.
SAE ARP1827 - MEASURING AIRCRAFT GAS TURBINE ENGINE FINE FUEL FILTER ELEMENT PERFORMANCE Organization: SAE
Date: 2014-11-01
Description: It is intended for non-cleanable (disposable), fine fuel filter elements used in aviation gas turbine engine fuel systems.
SAE/TP - 2008-01-2236 - HIGH PERFORMANCE ROBOTICS FOR AEROSPACE PAINT FINISHING OPERATIONS Organization: SAE/TP
Date: 2008-08-19
Description: These developments include: new IRB5500 robots with increased work envelope and acceleration capability; highly efficient RB1000 paint atomizer family; CBS advanced paint saving cartridge technology; new robotic powder paint application (IC-3) and color change (PCC) equipment; DispensePac sealant and adhesive robotic dispensing systems including newest applications of sprayable masking materials; TrueView vision and force control systems supporting applications in work object location, robot guidance, part cleaning, sanding, polishing and masking.
SAE/TP - 2011-01-2594 - APPLICATION OF GENETIC ALGORITHM FOR PRELIMINARY TRAJECTORY OPTIMIZATION Organization: SAE/TP
Date: 2011-10-18
Description: The paper describes a preliminary study undertaken for the Systems for Green Operation Integrated Technology Demonstrator for the Clean Sky Project (FP7) [1] and uses a customized algorithm NSGAMO2 (a proposed variation of the Non-dominated Sorted Genetic Algorithm II [2]).
NPFC - MIL-DTL-22612 - DETECTOR, COMBINED CONTAMINATED FUEL Organization: NPFC
Date: 2015-01-29
Description: Due to the natural fluorescence of some diesel fuels, procedures for testing diesel fuels in these units may differ from aviation (kerosene) fuels.

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