"TEMPERATURE MEASUREMENT RANGE SHALL BE +212 DEG F TO +716 DEG F, SAMPLE CAPACITY SHALL BE 500ML MINIMUM, DIFFERENTIAL PRESSURE SHALL BE 0 TO 300 MMHG, POWER REQUIRED SHALL BE 115.0V, WEIGHT OF THE SYSTEM SHALL NOT EXCEED 200 LBS, FUEL LEAK AUTOMATIC SHUT-OFF MECHANISM SHALL BE INCLUDED, TESTER SHALL BE CAPABLE OF AUTOMATIC PERFORMANCE OF PREPROGRAMMED TESTS AND USER DEFINED TESTS, SHALL HAVE A 15 INCH MINIMUM DIAGONAL DISPLAY SCREEN OF CRT OR BETTER, TESTERS OPERATING SYSTEM SHALL BE COMPATIBLE WITH THE LATEST AIR FORCE STANDARD, TESTER SHALL PROVIDE A MEANS OF CONNECTING A STANDARD PRINTER VIA USB OR PARALLEL PORT, TESTER SHALL HAVE A STANDARD KEYBOARD FOR DATA INPUT"
FTLD
FUNCTIONAL DESCRIPTION
EVALUATES THE OXIDATION STABILITY OF AVIATION TURBINE FUELS