Test Results: Sun-Foil Aircraft Reflecting and Insulating Sun Screens

LOCATION: Scottsdale, Arizona - Scottsdale Municipal Airport Ramp

Sun-Foil Aircraft Sunscreens

Product Test: SUN-FOIL Sun Screens

Purpose: To determine the ambient air and glare-shield temperatures of a parked aircraft with and without SUN-FOIL Sun Screens installed.

Test Parameters: A Piper Malibu remaining stationary for a period of five consecutive days was used for the test. Recording thermometers were placed in the aircraft; one was placed on the glare-shield, the other on the co-pilot's arm rest. Temperatures were read each day at 5:00pm with the aircraft remaining sealed for a period of twenty-four hours.

    Outside Temp Glare-Shield Panel Air Temp Inside Aircraft
Day 1: No Sun Screens 100° F 188° F 180° F 140° F
Day 2: Sun-Foil Sun Screens 102° F 120° F 114° F 117° F

Summary: Test results show SUN-FOIL Sun Screens effectively reduced cockpit glare-shield heat by 66° F, and air inside the aircraft by 23° F.