(650) 49-FLY-US

Cessna T-182T - N6166Q

Equipment: G1000/GFC700 WAAS & Synthetic Vision Technology (SVT)

Recent G1000 Upgrade:

Garmins G1000 Synthetic Vision Technology

Garmin’s SVT seamlessly blends information about the aircrafts position with topographic databases to create and display real-time 3D images. The information is presented on the G1000s large flight displays with XGA (1,024x768-pixel) resolution, superior sunlight readability and wide viewing angles. SVT presents the necessary information in ways that are easy to understand so pilots feel at ease interpreting the information.

SVT transforms the cockpit by accurately displaying synthetic terrain, flight hazards, flight path marker and highway-in-the-sky on the PFD so that the pilot maintains excellent airborne situational awareness even when flying in conditions of reduced visibility or darkness. This results in reduced pilot workload and safer flying.

Numerous SVT features increase safety of flight and help pilots fly with greater precision:

• Obstacles: Intuitively enlarges obstacle(s) as aircraft approaches; TAWS based colors are used when the required obstacle clearance is not met or in the case of potential obstacle impact
• Traffic: TCAS traffic symbology represented in 3D that changes size relative to range
• Flight Path Marker: Displays projected path of the aircraft
• Zero Pitch Line: Clearly distinguishes aircrafts altitude in relation to nearby terrain
• Gridlines: Drawn on the terrain surface and enhances distance perception
• Runways: Runway designations and thresholds are superimposed on terrain data; Unique runway highlighting and enhancements improves runway visibility from a distance
• Airport Signs: Depicts identifier of nearby airports

Weight and Balance

Replace sample weights with your actual weights, then click on the "Calculate" button to see the new takeoff C.G. Important: Pilots should always calculate the Weight and Balance on the ramp prior to takeoff using the latest data from the POH, and taking into account all circumstances including the difference between takeoff and landing fuel quantity and weight.