Flight Training Central
FEBRUARY 17, 2024
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. ( VFR = Ceilings greater than 3,000’ AGL and visibility greater than 5 miles MVFR = Ceilings between 1,000’ and 3,000’ AGL and/or visibility between 3 to 5 miles.
Air Facts
MAY 10, 2024
Particular attention to true airspeed vs. turn radius. At what AGL altitude will the aircraft be in a stable/configured condition? (No FAA parameters are no lower than 500’ AGL for stabilized criteria What specific runway lighting do we expect to see? No later than). What are the criteria for a Missed Approach Command?
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Chess In the Air
JUNE 24, 2022
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. At this point he was just NW of the runway at an altitude of 8000 ft MSL (2464 AGL). After all, a pattern entry altitude of approx.
Pilot Institute
MAY 4, 2024
Your aircraft will fly at a faster true airspeed at higher density altitudes. x V SO (or POH recommendation) by around 500 feet AGL. In this region of reversed command, use power to control altitude and pitch to control airspeed. Establish the target approach speed by around 500 feet AGL.
Universal Weather
APRIL 9, 2024
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.
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