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<br />TABLE 2.1.1 Instrumentation Onboard \4yoming King Air (N2UW) <br /> <br />Para;"etcr <br /> <br />rleasured <br /> <br />Ins t r u r:18 n t <br /> <br />type <br /> <br />nanufacturer and <br />nodel number <br /> <br />R.Jnge <br /> <br />Time <br />Const<Jnt <br /> <br />Accuracy <br /> <br />Useable <br />Reso 1 ut ion'" <br /> <br />le:~pe:-ature <br /> <br />0.1 C <br /> <br />Ten~pe ra tu r2. <br /> <br />De,,1 Point <br /> <br />Heading <br /> <br />-l="' <br /> <br />Altitude <br /> <br />Indicated <br />Airspeed <br /> <br />Rate of <br />Climb <br /> <br />Position - <br />Azimuth <br /> <br />Position <br />Distance <br /> <br />Ve rt i ca 1 <br />Acceleration <br /> <br />Platinum <br />Resistance <br /> <br />P 1 a t i num <br />Resistance <br />Reverse Flm.J <br /> <br />Peltier cooled <br />mirror <br /> <br />~jagnetie <br /> <br />Total <br />Pressure <br /> <br />Differential <br />Pressure <br /> <br />Diffel-ential <br />Altitude <br /> <br />VOR <br /> <br />onE <br /> <br />Vert. Stab. <br />Accelerometer <br /> <br />Rosemount Engr. Co. <br />SlOB a;:rpl ifier <br />J'lode I 102 Probe <br /> <br />NCAR Probe <br />J-1inco, Inc. <br />EI er'ent <br /> <br />Cambridge System, Inc. <br />Hodel 137C3 <br /> <br />King Radio Corp. <br />KPl 553 & Sperry <br />C14-43 <br /> <br />Rosemount Engr. Co. <br />Model 1201FAIBIA <br /> <br />Rosemoun t Eng r. Co. <br />J-jodel 831 CPX <br /> <br />Rosemount Engr. Co. <br />Mode] 1241-A-4BCDE <br /> <br />King Radio Corp. <br />KNR 615 <br /> <br />King Radio Corp <br />KDI.1 705A <br /> <br />Humphrey <br />Model SA-09-0502-1 <br /> <br />+50"C <br /> <br />3 see <br /> <br />+0.50C <br /> <br />+0.5"C <br /> <br />0.1 C <br /> <br />+500C <br /> <br />0.5 see <br /> <br />+500C 3OC/sec +0.5OC>OoC 0.3C <br /> (s Im.J rate) +1.OoC<OcC <br />0-3600 1 sec +10 0.10 <br /> <br />- - <br /> <br />----- <br /> <br />- -- <br /> <br />- <br /> <br />- -.. <br /> <br />- - <br /> <br />- -- <br /> <br />0-15 psia <br />(0-]034 mb) <br /> <br />15 ms <br /> <br />0-1.6"Hg <br />(0-54 mb) <br /> <br />25 ms <br /> <br />O.25?& <br /> <br />0.004 psia <br />(0.3 mb) <br /> <br />3xlO-3. <br />( O. 1 mb ) <br /> <br />+6000 <br />T+30.5 m/s) <br /> <br />50 ms <br /> <br />jl,djustable f.or <br />zero & span <br /> <br />1% to 15,0001 <br />2% to 25,0001 <br />5% to 30,0001 <br /> <br />~ 50 fpm <br />(0.25 m/s) <br /> <br />0-3600 <br /> <br />1 see <br /> <br />1.50 <br /> <br />0.2 n mi <br /> <br />0.1 n mi <br /> <br />0-200 n mj <br /> <br />] see <br /> <br />0.002 9 <br /> <br />(-) <br /> <br />+0-2 9 <br /> <br />10 ]JS <br /> <br />*Values quoted are estimates of overall useable resolution which can be expected for actual flight conditions. <br />In several cases, indicated by (-), \-Je have insufficient experience to estimate the useable resolution. Theoretical <br />resolutions are one part in 4095 for all the above parameters. <br />