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T/S/D Computer with Density Altitude Performance [DAA-304]

$18.95

Quickly determines takeoff and climb performance and all Time / Speed / Distance problems.

The Denalt computer was developed by the Federal Aviation Administration to replace the Koch Chart for computing altitude-temperature effects on airplane performance. The APR Denalt computer is adapted to airplanes equipped with either fixed or variable pitch propellers.

The Denalt Performance Computer enables a pilot to quickly and easily determine how density altitude erodes takeoff and climb performance. These rapid calculations apply to aircraft with either fixed-pitch or constant-speed propellers.

As far as APR’s popular Time/Speed/Distance computer is concerned, it obviously is the mainstay of navigation and capable of calculating a wide variety of popular problems.

APR's unique combination computer is available in either PVC plastic or lifetime anodized aluminum. Both are manufactured in the United States with high-visibility graphics. User-friendly instructions are included with both.

IMPORTANT: Always consult your pilot’s operating handbook as this computer does not supplement or replace the manufacturer’s performance data. Not applicable to turbocharged aircraft.

Anodized aluminum discs, 3 ¾” dia. Plastic cursor 4 ¾”.

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