OPTIONAL Class A TAWS, ADS-B Out software upgrade available at additional cost, P/N: 010-00878-05
|Dimensions:||6.25"W x 6.00"H x 11.25"D||Display Size:||4.46"W x 5.27"H|
|Display Resolution:||600 x 708 pixels||Display Type:||Color TFT LCD; sunlight readable|
|Weight:||7.7 lb||Voltage Range:||11-33|
|Built-in VHF Comm:||No||Transmit Power:||no (VHF comm not included)|
|Built-in VOR/LOC/GS:||No||Receiver:||15 channel; TSO-C146c|
|IFR or VFR:||IFR||Basemap:||Yes|
|US Terrain & Obstacle Database:||Yes||Nav Database:||Yes|
|Types of Jeppesen Data:||Full & Non-Precision approaches, DPs and STARs, Victor/Jet Airways, eCharts (w/Optional Enablement)||Nav Database Coverage Area:||Americas, International or Worldwide|
|Waypoints/ Favorites/ Locations:||1000||Flight Plans:||99 reversible; up to 100 waypoints each|
|Fly WAAS Approaches:||Yes||Moving Map:||Yes|
|Front-Loading Datacards:||Yes||XM WX Weather & Radio for US & Canada Compatible:||Yes|
|TIS Alerting Compatible:||Yes||Class B TAWs Alerting Compatible:||Yes|
|Additional:||Eligible for PilotPak Databases|
|Part Number||Audio Panel Description:|
|010-00819-50||Black receiver w/rack, backplate, conn kit, config module & product info kit|
|011-02281-00||Black receiver, 11-33 VDC|
Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact email@example.com
The serial number on all of our products is necessary for registration and warranty purposes. The system ID is an internal number which is required for database updates and downloads. These updates can be done on the Fly Garmin website. Each aviation database update is downloaded specific to the system ID of each GPS, therefore if the system ID is incorrect on our website, your aviation databases will not update correctly.
This error "0" is associated with the database program running on a computer that is not running a supported operating system. For the program to work correctly, the file must be downloaded on a computer running Windows XP or newer.
The glide path that is generated is based on the information that is used for the Localizer Performance with Vertical guidance (LPV) and Lateral Navigation / Vertical Navigation (LNAV/VNAV) procedures. It uses a specified decent angle that is centered at the MAWP (Missed Approach Waypoint) and at the TCH (Threshold Crossing Height). If this information is included in the electronic database for the approach, the 400W/500W series, G1000 with WAAS, and GTN 600/700 series will generate a glide slope.
This error message can result from a wide variety of issues. Below is a list of the most common:
An altimeter does not measure altitude on the GTN-725 device. The altimeter in the aircraft measures air pressure. The altimeter is calibrated to display a certain change in altitude based on a change in air pressure. For every inch of mercury pressure change, the altimeter displays a change of approx. 1000 ft. of altitude. The GPS does not use air pressure to determine altitude and is not subject to the pressure errors in determining altitude. Therefore, the GPS derived altitude is almost always more accurate than an altimeter. Since everyone uses a pressure-based system to determine altitude, it is integral to utilize a pressure sensitive altimeter to ensure required vertical separation.