1、b -,- - -_L &* MS33b3b REV B bb m 7777732 0007437 5 W . . c ACCELERATION AIR8PEED ALTlTUDE ANGLEOFATTACK DISTANCE (NAVIGATION) ENGWE SPEED FUEL FLOW FUEL QUANTlTY HEADING hlA“OLD PRESS OXYGEN (QUANTlTYI PRESSURES (SYSTEMS) UNITS OP MEASUREMENT PROPELLER/ROTOR SPEED - TEMPERATURE - THRWT - TORQUE - V
2、ERTICAL SPEED - UNi OF GRAYITY (g) (1) mm (II) MACH NWER FEET DEGREES OR UNITB PROPORTIONAL TO DEGREES NAUTICAL -ES (i) RECIPRQCATING ENGINES - R.P.M. (Il) TURBO-JET ENFS - PERCENT R. P. M. POUNDS PER ROUR POUNDG DEGREES (COMPASS) INCHES OF MERCURY LITRES POUNDS PER SQUARE INCH R.P.M. DEGREES CEISIU
3、S (CENTIGRADE) POUNDS 0 PouNDF FEET PER MINWE NOTES: 1. THE ABOVE UNITS SHALL BE USED POR THE DISPLAY OP WPORMATION ON AIRCRAFT AND ENGINE INSTRUhENTS AND AIS0 SHALL BE USED AS STANDARDS FOR EQUIPMENT WHICfi SENSES OR COMPWES THE SAME INFORMATION FOR DISPLAY. * 1. THE STANDMID DOES NOT PROHIBIT THE
4、USE OF INSTRUMENTS DISPLAYING INFORMATION IN GENERAL TERMS SUCH AS -PER CENT, FULL, HALF, EMPTY- OR m “TIME TO GO. 3. 4. INTERNATIONAL TIlLE MILITARY ST ANDAID AVY-AS INTEREST THER COST ASCC-lOlZ WAF-11 STANAG- HEMUREMENT, UNITS OF, POR AIRCRAW INSTRUMENTS MS33636 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
