This week, we’re pleased to feature guest posts from CFI and FAA DPE Jason Blair! We featured Jason’s excellent write up on flying the traffic pattern earlier this year. He writes his own blog at jasonblair.net.
Gliding is for gliders, right? Well, it’s not just for
…In today’s post, we are going to discuss the Airplane Flight Manual (AFM). The AFM is a document that is developed by your airplane’s manufacturer containing specific information in regards to operating instructions of the aircraft. These manuals are specific to an aircraft’s serial number and are approved by the
…The success of a flight depends largely on thorough preparation. In the course of your training, a pattern of regular preflight actions should be developed to ensure that this is the case. This includes planning a flight, and checking
…Monday’s post gave us an introduction into the world of gyroscopic flight instruments and as we learned these include the attitude indicator, turn coordinator, and heading indicator also referred to as the directional gyro. Each one of these gyroscopic flight instruments functions based off the principle of rigidity
…This week we’re looking again at flight instruments. More specifically, gyroscopic instruments. Take a look at what we’ve posted so far on flight instruments, including our CFI’s series on pitot-static systems. This post is excerpted from Bob Gardner’s The Complete Private Pilot.
The attitude indicator, the
…Let’s recap some of the important information we learned from Monday’s post on carburetor ice.
As air flows through a carburetor, it expands rapidly. At the same time, fuel entering the airstream is vaporized. Expansion of the air and vaporization of the fuel causes a sudden cooling
…Today we’re taking a look at carburetor ice with the Pilot’s Handbook of Aeronautical Knowledge.
As mentioned earlier, one disadvantage of the float-type carburetor is its icing tendency. Carburetor ice occurs due to the effect of fuel vaporization and the decrease in air pressure in
…As the angle of attack is increased (to increase lift), air will no longer flow smoothly over the upper wing surface but instead will become turbulent or “burble” near the trailing edge. A further increase in the angle of attack will cause the turbulent area to expand forward.
