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Standard

Measuring Aircraft Gas Turbine Engine Fine Fuel Filter Element Performance

2003-05-15

HISTORICAL

ARP1827A

This SAE Aerospace Recommended Practice (ARP) delineates two complementary filter element performance ratings: (1) dirt capacity, and (2) filtration efficiency, and corresponding test procedures. It is intended for non-cleanable (disposable), fine fuel filter elements used in aviation gas turbine engine systems.

Standard

MEASURING AIRCRAFT GAS TURBINE ENGINE FINE FUEL FILTER ELEMENT PERFORMANCE

1992-08-01

HISTORICAL

ARP1827

This ARP delineates two complementary filter element performance ratings and corresponding test procedures. It is intended for the noncleanable (disposable), fine fuel filter elements used in aviation gas turbine engine systems.

Standard

FUEL PUMP THERMAL SAFETY DESIGN

1978-11-01

HISTORICAL

ARP594C

These recommendations cover only those design factors which might cause the pump motor or pump housing to act as an autogenous or spark-ignition source for explosive fuel vapors within the airplane tank.

Standard

RECOMMENDED PRACTICES FOR GENERAL AVIATION FILTERS, RECIPROCATING ENGINE (PISTON TYPE) AIRCRAFT

1975-09-01

HISTORICAL

ARP1400

This recommended practice establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 50 - 100 psig.

Standard

AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER

1974-01-01

HISTORICAL

AIR1326

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 and the aircraft engine fuel system, and limitations in the usage of the V/L concept.

Standard

FUEL BOOSTER PUMP DESIGN PROVISIONS FOR AUTOGENOUS AND SPARK IGNITION PREVENTION AND CONTROL

1965-09-01

HISTORICAL

ARP594B

These recommendations cover only those design factors which might cause the pump motor or pump housing to act as an autogenous or spark-ignition source for explosive fuel vapors within the airplane tank.

Standard

AIRCRAFT FUEL PUMP CAVITATION ENDURANCE TEST

1957-11-15

HISTORICAL

ARP492

This procedure is intended to apply to any aircraft fuel pump which supplies liquid hydrocarbon fuel either directly to an aircraft engine or to another pump mounted on an aircraft engine, except that it is not intended to apply to a fuel pump mounted in a fuel tank.