TM 1-1510-225-10 3D-66 plan.      A   different   groundspeed   may   be   entered   by using  the  left  outer  knob  to  position  the  cursor  over each digit of the groundspeed and using the left inner knob to select each individual digit. If  data  is  entered  for  FF  and  RES, as described for the TRI 1 page, the fuel required for the trip is now displayed.  Fuel flow and reserve fuel entries made on the TRI 5 page also input this same data on the TRI 1 and the TRI 3 pages. 4.   Turn    off    the    cursor    function    and    then select the TR I 6 page.  The minimum ESA and    a    listing    of    areas    of    special    use airspace  of  special  use  airspace  won’t  fit on  one  page,  there  will  be  multiple  TRI  6 pages indicated by TRI+6.  Refer to Figure 3D-95. TRI+6 FP 7 ESA 13800FT LUBBOCK CL C A-637 ALRT Figure 3D-95.  TRI 6 Page 3D-26.  THE CALCULATOR PAGES. The  are  seven  calculator  pages  which  may  be used   to   calculate   a   variety   of   information   such   as pressure  altitude  and  density  altitude,  true  airspeed, winds aloft, VNAV angle, and time zone conversions.   The calculator pages rely on manual inputs of air data parameters even if  the  KLN  90B  is  interfaced  with  air data sensors. a.   The Calculator 1 Page.    The  CAL  1  page  is used    to    determine    pressure    altitude    and    density altitude. 1.   Display the CAL 1 page on the left side. 2.   Press the left  CRSR button to turn on the left cursor function. 3.   Enter  the  altitude  indicated  on  the  aircraft altimeter (IND) to the nearest hundred feet by  using  the  left  outer  knob  to  move  the cursor to the desired position and the left inner knob to select each digit. 4.   Use the left outer knob to move the cursor to the  first BARO position, and then enter the  current  altimeter  setting  by  using  the left  inner  and  outer  knobs.    The  pressure altitude (PRS) is now displayed. 5.   Use the left outer knob to move the cursor to  the  first  TEMP  position,  and  then  enter the   outside   air   temperature    (in    C)  by using the left inner and outer knobs.  The first digit of the temperature is either zero if   the   temperature   is   above   zero   or   a minus (–) if the temperature is below zero.   For    maximum    accuracy,    the    static    air temperature   should   be   entered.    This  is the   temperature   of   the   air   without   the effect of heating due to movement through the air.  The density altitude (DEN) is now displayed as illustrated in Figure 3D-96. 6.   Press the left  CRSR button to turn off the left cursor function. CAL 1   ALTITUDE IND:04000FT BARO:29.84” PRS  4100FT TEMP: 034^o C DEN  7100FT Figure 3D-96.  CAL 1 page NOTE If the AETMS is installed and interfaced to the   KLN   90B,   the   OTH   10   page   displays pressure  altitude  and  density  altitude  for the present conditions.  b.  The Calculator 2 Page.   The  CAL  2  page  is used to determine TAS. 1.   Select the CAL 2 page on the left side. 2.   Press the left  CRSR button to turn on the cursor function. 3.   Enter  the  aircraft’s  calibrated  airspeed  by using  the  left  inner  and  outer  knobs.    If