♦ THE STC IS DESIGNED TO INSTALL ONE OR UP TO EIGHT INDICATOR AT A TIME
♦ AN OPTIONAL 485 DATA BUS PMA WIRE HARNESS IS AVAILABLE TO ALLOW
DOWNLOADING OF MAINTENANCE DATA FROM ALL EIGHT ENGINE INDICATORS
♦ A BUILT IN CLOCK PROVIDES A DATE STAMP WHEN AN EVENT OCCURS
♦ THE COST PER INDICATOR IS GREATLY REDUCE OVER EXISTING INDICATORS
♦ THE INSTALLATION IS A PLUG AND PLAY - NO CHANGE IN AIRCRAFT WIRING
♦ BRIGHT LED DIGITAL DISPLAY AND BACK LIGHTING PROVIDE VERY HIGH MTBF
♦ IN SERVICE PROVEN MTBF - 35,000 HOURS
♦ THREE YEAR WARRANTY - READABILITY IS GREATLY IMPROVED
♦ DIGITAL DESIGN - MICROPROCESSOR CONTROLLED
♦ FAA TSO (TECHNICAL STANDARD ORDER) APPROVED
♦ ACCURACY +0.5% OF THE INPUT SIGNAL - OVER TIME & TEMPERATURE RANGE
♦ POINTER RESOLUTION (007 OF AN INCH AT TIP) - TRUE ANALOG MOVEMENT
♦ POWER REQUIREMENTS PER INDICATOR - 28 VDC - 160 mA MAX INDICATOR
OPERATES CORRECTLY AT 10 TO 40VDC
♦ THE INDICATORS DO NOT REQUIRE CALIBRATION
♦ POSITIVE FAILURE INDICATION OF SIGNAL AND/OR POWER
♦ AVALABLE NIGHT VISION (GREEN A, B OR WHITE)