User manual GARMIN G1000: KING AIR C90 PILOT'S GUIDE REV. A, SEP, 2007

[. . . ] Hawker Beechcraft C90A/GT Copyright © 2007 Garmin Ltd. This manual reflects the operation of System Software version 0636. 00 or later for the Hawker Beechctaft C90A/GT. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc. , 1200 East 151st Street, Olathe, Kansas 66062, U. S. A. [. . . ] 2) Turn the small FMS Knob to enter the fuel on board. 3) Press the ENT Key to confirm the entry. When the aircraft is in the air and a destination waypoint has been entered, the fuel calculations can be completed. · Estimated landing weight = zero fuel weight + estimated landing fuel weight. · Estimated landing fuel weight = fuel on board weight - (fuel flow x ETE) · Excess fuel weight = estimated landing fuel weight - fuel reserves weight If the aircraft is on the ground or a destination waypoint has not been entered, the following fields display invalid values consisting of six dashes: · Estimated landing weight · Estimated landing fuel weight · Excess fuel weight 5-112 Garmin G1000 Pilot's Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A FLIGHT MANAGEMENT WEIGHT CAUTION AND WARNING CONDITIONS If the zero fuel weight is greater than the maximum allowable zero fuel weight, then the zero fuel weight is displayed in amber. If the aircraft weight is greater than the maximum allowable takeoff weight, then the aircraft weight is displayed in amber. If the estimated landing weight is greater than the maximum allowable landing weight, then the estimated landing weight is displayed in amber. If the estimated landing fuel weight is positive, but less than or equal to the fuel reserves weight, the following values are displayed in amber: · Estimated fuel at landing weight · Excess fuel weight If the estimated landing fuel weight is zero or negative, then the following values are displayed in red: · Estimated fuel at landing weight · Excess fuel weight 190-00663-00 Rev. A Garmin G1000 Pilot's Guide for the Hawker Beechcraft C90A/GT 5-113 FLIGHT MANAGEMENT 5. 10 RAIM PREDICTION RAIM (Receiver Autonomous Integrity Monitoring) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (4. 0 nm for oceanic, 2. 0 nm for enroute, 1. 0 nm for terminal, and 0. 3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. Because of the tighter protection limit on approaches, there may be times when RAIM is not available. RAIM prediction must be initiated manually if there is concern over WAAS coverage at the destination or some other reason that compromises navigation precision. If RAIM is not predicted to be available for the final approach course, the approach does not become active. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. RAIM PREDICTION Box - Prediction Waypoint - Arrival Time - Arrival Date - RAIM Status RAIM Softkey (displays RAIM PREDICTION) SBAS Softkey (displays SBAS Selection) Figure 5-98 RAIM Prediction Predicting RAIM availability at a selected waypoint: 1) Select the AUX-GPS Status Page. The RAIM Prediction `WAYPOINT' field is highlighted. 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, or airway waypoints). 5-114 Garmin G1000 Pilot's Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A FLIGHT MANAGEMENT 4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of waypoints and press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. [. . . ] The first waypoint in the missed approach procedure becomes the active waypoint when the SUSP Softkey is selected after crossing the MAP. All published missed approach procedures must be followed, as indicated on the approach plate. To execute the missed approach procedure prior to the MAP (not recommended), select the Active Flight Plan Page and use the ACT LEG Softkey to activate the missed approach portion of the procedure. AFTER A MISSED APPROACH, HOW CAN THE SAME APPROACH BE RE-SELECTED?HOW CAN A NEW APPROACH BE ACTIVATED? NOTE: Do not attempt to reactivate the current approach prior to crossing the missed approach point (MAP). [. . . ]