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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 hazard include: a Reducing fueling rate into tank bays including use of multiple refueling inlet nozzles. b Reducing refuel plumbing flow velocities. c Introducing fuel into the tank at a low velocity near the bottom and directing it to impinge upon a grounded conducting surface. d Avoiding electrically isolated conductors in the fuel tank. e Using conductivity additives in the fuel.

This document defines design, performance, and test criteria for self-sealing breakaway valves.

This document defines design, performance, and test criteria for self-sealing breakaway valves for use in crash-resistant aircraft fuel systems.

This SAE Aerospace Information Report (AIR) presents a glossary of terns commonly utilized in the ground delivery of fuel to an aircraft and some terms relating to the aircraft being refueled.

This SAE Aerospace Information Report (AIR) is limited to the subject of aircraft fuel system plumbing systems and the questions concerning the requirements for electrical bonding of the various components of the system as related to Static Electric Charges, Electromagnectic Interference (EMI) and Lightning Strikes (Direct and Indirect Effects)

No scope available.

This SAE Aerospace Information Report (AIR) reviews performance testing parameters for noncleanable, often referred to as disposable, aircraft gas turbine engine lubricant filter elements.

This document defines design, performance, and test criteria for self-sealing breakaway valves.