Inhaltszusammenfassung zur Seite Nr. 1
N
B
KLN 90B GPS
Abbreviated Operation Manual
Rev. 1
ORS 20
Inhaltszusammenfassung zur Seite Nr. 2
N B KLN 90B GPS Abbreviated Operation Manual Rev. 1 ORS 20 IMPORTANT: Special installation procedures must be followed in order for the KLN 90B to be certified for IFR use. Consult the KLN 90B Flight Manual Supplement for the operating limitations of this unit. NOTE: Refer to the KLN 90B Pilot's Guide (006-08773-0000, Rev.1) for Database update information.
Inhaltszusammenfassung zur Seite Nr. 3
PREVIEW OF OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 1.0 TURN ON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 2.0 BASIC OPERATION OF PANEL CONTROLS . . . . . . . . . . . 6 2.1 Page Selection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 2.2 Entering Waypoint Identifiers . . . . . . . . . . . . . . . . . . . . . . . 8 2.3 The Duplicate Waypoint Page . . . . . . . . . . . . . . . . . . . . . . 9 3.0 INITIALI
Inhaltszusammenfassung zur Seite Nr. 4
12.3 Adding A Waypoint To A Flight Plan . . . . . . . . . . . . . . . . 41 12.4 Deleting A Waypoint From A Flight Plan . . . . . . . . . . . . 41 12.5 Deleting Flight Plans . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 12.6 Storing FPL 0 As A Numbered Flight Plan . . . . . . . . . . . 42 13.0 OPERATING FROM THE ACTIVE FLIGHT PLAN . . . . . . 43 13.1 General Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43 13.2 Turn Anticipation And Waypoint Alerting . . . . . .
Inhaltszusammenfassung zur Seite Nr. 5
PREVIEW OF OPERATION To give you an idea of how easy the KLN 90B is to operate, the following operational preview is presented. This operational preview assumes the KLN 90B has been properly installed, the unit was previously operational in the same general geographical location, and that no peripheral equip- ment interfaced with the KLN 90B (such as external HSIs, CDIs, autopi- lots, RMIs, fuel flow systems, moving map displays, etc.) is to be used at this time. If you are using this operatio
Inhaltszusammenfassung zur Seite Nr. 6
test page has been approved. Press the GPS CRS button to put the unit into the LEG mode. After the GPS CRS button indicates LEG, then the KLN 90B will continue the start-up process.) 3. A database page is now displayed showing the date the database expires or the date it expired. Press E to acknowledge the information displayed on this page. 4. A page displaying the letters PRESENT POS at the top will now be on the left side of the screen. In a couple of minutes or less, this page will display
Inhaltszusammenfassung zur Seite Nr. 7
IMPORTANT: This abbreviated operation manual does not include any information on how to use the KLN 90B for flying approaches or SID/STAR procedures. Refer to the KLN 90B Pilot’s Guide and the aircraft flight manual supplement for instructions on these procedures. 1.0 TURN ON • Push the Power/Brightness knob located in the upper right corner of unit to the “in” position. The unit is turned off by pulling this knob to the “out” position. • After a few seconds of warm up, the screen will show a T
Inhaltszusammenfassung zur Seite Nr. 8
The KLN 90B stores the correct time, date and last location of the aircraft in memory. If any of these parameters are not correct then the GPS receiver in the KLN 90B will automatically enter a mode in which it can determine this information. This usually will take less than 12 minutes, so the KLN 90B should be able to determine its position by the time you have taxied to the runway. However, if quicker time to lock onto satellites is required it is possible to shorten this time by giving the KL
Inhaltszusammenfassung zur Seite Nr. 9
updated on the Self Test page when power is first applied to the KLN 90B and on the Altitude page each time a new baro correction is made to the aircraft’s altimeter. The altimeter baro setting may be changed at a later time from inches to millibars (or vice versa) on the SET 7 page. The altimeter baro set field will not be a cursor field if the KLN 90B is inter- faced to certain air data/altimeter systems which update the baro set field when the aircraft’s altimeter baro setting is updated. T
Inhaltszusammenfassung zur Seite Nr. 10
2.0 BASIC OPERATION OF PANEL CONTROLS Top Left Segment Top Right Segment "Left Page" "Right Page" Lower Left Lower Middle Lower Right Segment Segment Segment 2.1 Page Selection The screen is normally divided into five segments defined by vertical and horizontal lines on the screen. The large top left segment is called the left page and the large top right segment is called the right page. The small lower left segment displays the name of the left page being displayed while the small lower ri
Inhaltszusammenfassung zur Seite Nr. 11
screen by first pressing the appropriate C button (left C for left page and right C for right page) to turn the cursor function on and bring the cursor on the screen. The appropriate concentric knobs are then used to enter the data. When a cursor is on the screen, the page name normally shown in the lower left and right segments is replaced with a CRSR annunciation in inverse video. Not all pages allow you to make data entry, and therefore pressing the C button while these pages are displayed
Inhaltszusammenfassung zur Seite Nr. 12
The eight page types for the left side are the following: Page Annunciation Knob Annunciation Page Name Page Numbers TRI TRIP Trip Planning 0 - 6 MOD MODE Mode 1 - 2 FPL FPL Flight Plan 0 - 25 NAV NAV Navigation 1 - 5 CAL CALC Calculator 1 - 7 STA STAT Status 1 - 4 SET SETUP Setup 0 - 9 OTH OTHER Other 0 - 4 * * up to 10 with fuel management system and air data interfaces The ten page types for the right side are the following: Page Annunciation Knob Annunciation Page Name Page Numbers CTR CTR C
Inhaltszusammenfassung zur Seite Nr. 13
NOTE: If you are entering an airport identifier that is all letters (no num- bers), then it will begin with a “K” prefix in the Contiguous U.S., a “P” in Alaska, or a “C” in Canada. If there are numbers in the identifier, then a prefix is not used. For other areas of the world the airport identifier stored in the KLN 90B database is identical to how it is charted. Like all rules there are also exceptions to the guidelines given above. If the above rules do not work it is possible to scan throu
Inhaltszusammenfassung zur Seite Nr. 14
waypoints in the database having the identifier. Below the identifier is a list of the waypoint types (APT, VOR, NDB, INT, SUP) and the associated countries which use the identifier. To see an example of a Duplicate Waypoint page perform the following steps: • Press D. • Turn the left inner knob to select the letter D as a waypoint identifier. “D” is the full identifier of several waypoints in the KLN 90B database. Press E. The Duplicate Waypoint page will be displayed on the left side . At
Inhaltszusammenfassung zur Seite Nr. 15
the almanac data will become out of date only if the KLN 90B hasn’t been used for the previous six months or longer. Collecting new almanac data takes place automatically if the data is more than six months old. If the almanac data is out of date and needs to be collected, the KLN 90B will take a few minutes to acquire your present position (usually about six (6) minutes, but not more than 12 minutes). The Self Test and Database pages should be approved. 2. The aircraft must be located such t
Inhaltszusammenfassung zur Seite Nr. 16
• Press E to view the waypoint page on the right side. • Press E again to confirm the waypoint page. NOTE: As an alternative, you can also enter the approximate latitude and longitude of your present position directly on the SET 1 page instead of entering a waypoint identifier. • Use the left outer knob to position the cursor over CONFIRM?, if it is not there already. • Press E. NOTE: The groundspeed (KT) and heading ( °) fields are not used for actual initialization in an aircraft. However, if
Inhaltszusammenfassung zur Seite Nr. 17
If this condition isn’t occurring, then: 3. If there is any waypoint page (APT 1-8 page, VOR page, NDB page, INT page, SUP page, or ACT page) in view on the right side when D is pressed, then the Direct To page will contain the identifier for the way- point page being viewed on the right side. If neither of the conditions above are occurring, then: 4. When D is pressed, the waypoint identifier for the current active waypoint will be displayed. 5. If there is no active waypoint when D is pressed
Inhaltszusammenfassung zur Seite Nr. 18
4.2 Direct To - Procedure B • Select the desired waypoint type (APT, VOR, NDB, INT, or SUP) on the right page. • Select the desired waypoint identifier using the following method: a. Press the right C. The cursor will be over the first character in the waypoint identifier. b. Rotate the right inner knob to select the first character of the desired identifier. c. Turn the right outer knob one step clockwise to move the cursor to the second character and then use the right inner knob to select t
Inhaltszusammenfassung zur Seite Nr. 19
• Press D. The Direct To page is displayed on the left side and it con- tains the desired waypoint identifier. • Press E to approve the waypoint page displayed on the right side. The right side will display the NAV 1 page, and the left side will return to the page which was displayed prior to pressing D (unless the NAV 1 page was on the left side in which case the pages will revert to the state they were in prior to the direct to operation). The selected waypoint is now the active Direct To wa
Inhaltszusammenfassung zur Seite Nr. 20
5.0 THE NAVIGATION PAGES As you would expect, the NAV (navigation) pages contain information relating specifically to the KLN 90B’s navigation capabilities. The KLN 90B has five NAV pages. Unlike any other pages, these pages may be selected and viewed on both the left and right sides of the screen. The procedure for selecting specific pages, including the NAV pages, was described previously under “BASIC OPERATION OF PANEL CON- TROLS”. NAV pages 1,2,3, and 5 are briefly described here. The
