Remove AGL Remove Knot Remove True Airspeed
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Instrument Flying (IFR) FAQs – top questions this week

Flight Training Central

AIM 5-3-3 ) Change in the average true airspeed (at cruising altitude) when it varies by 5 percent or 10 knots (whichever is greater) from that filed in the flight plan. ( IFR = Ceilings between 500’ and 999’ AGL and/or visibility between 1 and 3 miles. AIM 5-3-3 ) When an approach has been missed. (

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Mastering Short Field Landings (A Step-by-Step Guide)

Pilot Institute

In the Cessna 172S Pilot’s Operating Handbook (POH), the landing distance decreases by 10% for every 9 knots of headwind. For the Cessna 172, landing distance increases by 10% for every 2 knots of tailwind. Your aircraft will fly at a faster true airspeed at higher density altitudes.

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Invisible Trap Kills Glider Pilot – How To Avoid Microbursts

Chess In the Air

He only needed a glide ratio of 14:1 to reach the airfield to arrive at a typical pattern altitude of 1,000 ft AGL. At this point he still had an altitude of 8,275 ft MSL, i.e. 2,739 ft AGL. This is consistent with Rick’s report, which referenced 9 knots of wind. His altitude was 1339 AGL and his ground speed was 92 kts.

Pilot 52
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ADS-B UPDATE 2024– WHERE ARE WE NOW?

Universal Weather

or greater and/or max cruising true airspeed (TAS) greater than 250 knots (kts). Aircraft manufactured on or after 01-JAN-2020 and has an MTOW exceeding 12,566 lbs (5,700 kgs) or having a maximum cruising true airspeed (TAS) greater than 250 knots must have ADS-B (Out) 1090 MHz applicable to RTCA DO-260B.